TW593064B

TW593064B - A seating system and a passenger accommodation unit for a vehicle

Info

Publication number: TW593064B
Application number: TW092101637A
Authority: TW
Inventors: David Ferry; Adam Bernard Wells; Luke Miles; Andrew Leslie Lawler; David Edward Starkey
Original assignee: Virgin Atlantic Airways Ltd
Priority date: 2002-08-09
Filing date: 2003-01-24
Publication date: 2004-06-21
Also published as: TW200402382A

Abstract

A passenger seat assembly for a vehicle, particularly an aircraft, which is adapted to provide self-contained, individual seating and sleeping accommodation for a passenger said seat assembly comprising: supporting structure (42) for supporting said assembly off the floor of a vehicle; one or more movable passenger-bearing, structural components (71, 72); and means for connecting said movable, structural components to said structure such that said components can be selectively moved between a seat configuration, in which a plurality of passenger-bearing surfaces on said one or more structural, movable components (71, 71) or said supporting structure form a seat for the passenger, and a bed configuration, in which a plurality of said bearing surfaces (47, 48, 67, 74, 76) are disposed substantially coplanarly and substantially contiguously to form a bed for the passenger; characterised in that at least one of said movable components (72) is double-sided, comprising first and second opposite sides, one of said sides having a first seat surface (73) that forms part of the seat in said seat configuration, and the other side having a second bed surface (74) that forms part of said bed in said bed configuration.

Description

593064 玖、發明說明 (發明說明應敘明：發明所屬之技術領域、先前技術、内容、實施方式及圖式簡單說明） I：發明戶斤屬之技術領域3 發明領域本發明係有關於一種用於乘客载具，尤指飛機，的新 5 穎座位系統。本發明同時係有關於一種載具用乘客容納單元’該容納單元係適用以提供個別的、自備的座位及睡眠的乘客設施。本發明之容納單元係可使用在任一乘客載具，包括公車、巴士、渡輪以及火車車廂，但其係特別地適於使用在飛機上。本發明同時包括對載具用，尤指飛機， 10 乘客座位或是與其相關的改良。 C先前技術3 發明背景 15 20 一種傳統式飛機用之乘客座位其係包括一背靠以及一座位底盤其係藉由一適當的支撐結構受支撐而離開載具之地板，該支撐結構係固定在地板上的一對座位執道上。當使用座位之乘客透視觀視時，座位係形成一抽象的座位縱軸，並且於飛機之機身内的客艙中複數之該等座位係用以成列地配置，每一列係橫向地延伸橫過客艙，一個接著一個之後，每—餘之抽㈣絲歡體上係與機身之縱軸對正’以致母—座位係面向前。通常，於飛行期間，座位之月#月^夠自-直立的位置後仰至使用座位乘客感到舒適的一後仰位置。-些先前技術的乘客座位，特別針對飛機之商務餘及頭等驗内所用的座位，其中相鄰列之座位門的間距係較經濟餘中之座位為大，同包含有-腿靠（Ieg.咖） 7 593064 玖、發明說明 /、係以叙接至座位底盤的前方’並能夠在一下或儲藏位置，其中腿靠係自座位底盤懸垂而下大體上係垂直地朝向地板’以及-升高或展開的位置，其中腿靠自座位底盤向前伸展用以承受乘客離開地面之腿部，之間移動。因此，傳 •先式爪枝乘客座位藉由將背靠後仰並在有配裝腿靠的狀況下將腿靠升高’而使乘客能夠獲得相當的舒適度。儘官上述傳統的飛機乘客座位西己£，大體上對於持續三至四小時之短程運輸而言係符合要求的，但對於乘客: 型地希望能夠睡眠的較長飛行而言係無法符合要求。即使 1〇在上述的後仰位置，使用座位的乘客依然保持-般的坐姿。多數的乘客覺得當坐著時根本難以有舒適的睡眠。近年來疋期地搭乘長程航班的乘客人數顯著地增加，因而在業界傾向於所設計的乘客座位能夠讓乘客在飛行期間採用進一f的後仰位置以有助於睡眠。這對進行商務旅程的乘客而口係特別重要，因其在抵達目的地係需感覺精神恢復並且機敏的。 20 業界已揭露針對增加飛機乘客座位能夠後仰之程度的、可月b ι±其’、不過包含伸展背靠所能向後地後仰的程度並且將腿靠升高。使用該技術，當背靠後仰且腿靠升高時伸展至極限其係能夠形成—大體上為平坦的床，每次伸展至該-狀況時其大體上係配置成與座位底盤彼此為共平面的。該-系統的—缺點在於，鄰接列座位之間的間距大體上必需增加用以容納乘客的最大高度。儘管此狀況有時係發生在飛機之頭諸區域，但是對於商雜大體上係不缓 8 593064 玖、發明說明从白、°再者，儘管能夠形成_大體上水平地配置的平坦表面仁疋4表面仍不理想，因為在座位上的發泡材或其他的墊塞-般係經造型使用作為—座位，然而針對床而言，係需要具有—大體上為平坦的表面。 10 15 在德國專利GB23助4A中揭露一種用於飛機頭等搶的座位單元，其係包括一辅助座位係配置面向一主要座位丄輔助座位具有_座位部分係配置與主要座位之一腿靠配合，在主要座位之背靠係後仰至一水平的位置時，用以構成連々、平坦的供睡覺用之表面。座位單元界定一抽象勺座位縱轴，並且複數之該座位單元係相關於每—座位之縱軸以、縱向偏矛多的關係、，可並列地配置在客驗中，每一座位單元的方向係與飛機機身之縱軸成一銳角，俾便在每一座位單元之前方或後方形成一大體上為三角形或梯形的空間（根據座位單元係相對於客艙面向外抑或是面向内而定）。该空間係用w容納工作檯面（c〇unter_t〇p)至一相鄰座位單元之側，並可任擇地係為一食櫥或是其他的儲存空間。德國專利GB2326824 A的優點在於，在一連同主要座位之背靠、座位部分及腿靠的平坦睡眠表面中結合一附加、辅助的座位，其能夠形成一長的睡眠表面，該表面能夠提供身高高於6呎（1.83公尺）的乘客舒適的服務。然而，德國專利GB2326824 A之座位單元與上述的傳統式系統相較就客艙空間而言提供甚至較高的間接費用，此外，仍具有之缺點在於，座墊主要係設計作為座位使用而非作為床舖。德國專利GB2326824 A之座位的一缺點在於，佔用了客搶 9 20 593064 玖、發明說明中極大的地板面積，鑑於其之整體長度，德國專利 GB2326824 A之座位單元完全地不適合用在飛機的商務艙。世界專利WO 00/21831 A2號中揭露一種座位單元，其主要係使用在飛機客艙的商務艙部份，能夠將座位單元轉換成一床位。世界專利W0 00/21831 A2號之座位單元包括一對相對面向的座位，每一座位包含一供乘座者身體所用之座位空間，以及一供乘座者放置腿部的一伸展空間。所配置之座位讓一抽象的分隔軸之每一側邊將一座位空間伸展超越該軸進入另一座位的伸展空間。當安裝在飛機客艙 10中8可，其中之一座位大體上係面向前，而其他的座位大體上係面向後。世界專利W〇〇〇/21831 A2號之座位單元的每一座位包含一主要的座位，其大體上係與上述德國專利 GB2326824 A之主要的座位相同但不具有_腿靠，以及一 15 20 辅助單元係與主要座位之#方„。每—座位因而包括一主要座位，其具有一可後仰的背靠及座位底盤，以及一辅助單兀係包含一升高墊其係使用作為一擱腳部分 rest)。主要座位係可後仰，以致當背靠後仰時，座位底盤向前移動而與輔助單元接觸，用以於其間構成—連續表: ，將該表面使用作為-乘客所用的睡眠表面。與德國專利 GB2326824 A相較，世界專利w〇〇〇/2i83i A2號之座位單元因而具有在長距離飛行期間提供乘客一大體上水平的睡 :表面的優點。然而，世界專利w〇〇〇/2183i Μ號之座位早兀就於一典型的商務艙中可用的空間而言係為浪費的，並且當裝配為床舖時其之缺點在於，每一座位無法讓身材 10 玖、發明說明高大的乘客得到舒適的服務。與上述先前技術之座位相較 ’世界專利W0 00/2183 1 A2號之座位單元的每一座位同時具有其之座位坐墊並非特別針對使用作為睡眠表面而設計，其輪廓裝配主要係針對座位表面的用途的缺點。於飛機頭等艙中所使用之乘客座位的另一特性係為寬大的座位寬度。與世界專利WO 00/21831 A2號之座位單元相關的進一步缺點在於為了在商務艙中容納最大的總人數，所以將座位寬度減小，讓多數的乘客覺得不舒適。儘管世界專利WO 00/21831 A2號之座位單元，針對飛行過程中的乘客提供大體上平坦的睡眠表面係為公認優秀的優點，但是其之整體尺寸讓身高及/或體重高於平均值的乘客覺付座位稍嫌狹窄。再者，隱私隔板係配置在相鄰的座位單元之間，再加上於商務艙受限的空間甲配置的座位單元總數’導致客艙整體上具有稍嫌擁擠的景象。法國專利987559 A號中揭露一種大眾運輸載具，諸如電動車、公車以及相似車輛，所用的座位裝置，其係包括成列的座位，每一座位包括一支撐結構用於支撐離開載具地板的座位、一座位底盤以及一背靠。在二相鄰列座位之間形成-走道。與走道相鄰的其中之一座位的座位底盤，其係可在與走道鄰接的三座位支撐結構之間，以—颠倒的方向移開並吊起，用以在走道中構成一附加的座位。一座位之背靠因而能夠向前地搖動進入先前由座位底盤所佔用之空間’用以提供該-座位一個替換的座位底盤。一座位之背靠於是具有前及後表面，其二者係可使用作為部分的 593064 坎、發明說明座位。整列的座位係可任擇地能夠支撐一床墊用以構成一坐臥兩用的座位。然而，法國專利987559 a號之裝置並不適合使用在客機上，因為客機走道必需隨時保持暢通無阻 ’再者，複數之相鄰的座位係用以針對一單一的坐臥兩用 5的座位提供支撐。因此法國專利987559 A號之裝置並不能夠對每一座位提供一坐臥兩用的座位。曰本專利JP 5-13838 A號中揭露一種諸如巴士及火車之載具用座位系統，其係包含複數之座位。每一座位包含一座位底盤以及一背靠能夠在一直立位置與一後仰位置之 1〇間搖動，並且座位係配置在客艙中，相關於客搶之中心線成角度並面向外，用以在每一座位與客艙之一壁之間形成-大體上為三角形的空間。該空間容納一箱+，其係包含一供相鄰座位所用的擱腳部分。 15 20 法國專利647809錢中揭露_種臥舖車用的座位系統，其中複數之座位係配置與臥舖車之縱軸成_肖度，並係面向内用以在每一座位之背後形成一大體上為三角形:;空間，係用以容納一供相鄰座位所用的小桌子。發明概要因此本丧明之-目的係提供客機之商務驗用改良的客搶。特別地，本發明之一目的係提供該客搶，其係結合一具有最大長度’並且較佳地同時具有最大寬度之平坦的睡眠表面。本發明之-目的係提供一種改良的载具用乘客容納單 12 玖、發明說明兀，特別係針對飛機，該容納單元係用以提供乘客用之自備、個別的座位與睡眠客搶，特別係用在飛機之商務舱，其中相鄰列座位之間的間距，典型地係位在50_60吋（127 至1.52公尺）的範圍内。本發明之另一目的係提供一種乘客容納單元，其係可轉換成-具有最大長度的床舖’用以容納身材高大的乘客，特別是那些身高高於6呎的乘客〇·83公尺）。本發明之另-目的係提供一種具有—座位表面的载且用乘客容納單元，其係特別地使用作為一座位表面與—床 10舖表面，並係特別地使用作為一床舖表面。 15 20 本發明之一不同的目的係所提供之乘客容納單元能夠轉換成$舖並且當裝配為一座位時能夠對提昇或對第1 客艙的氣氛有所貢獻，當裝配為一床舖時能夠對提昇或對第-、不同的客艙氣氛有所貢獻。因此，本發明之另—目的係提供-種載具客艙用座位系統，其包含複數之能夠: 換成床舖的乘客容納單元，當所有或是大部分的單元係裝配為座位時，其係能夠帶給客搶—種特別的第_整體視覺外觀並且’當所有或是大部分的單元係裝配為床舖時，其係此夠帶給客艙一種第二整體外觀或氣氛。本發明之另一目的係提供一種乘客載具，特別是飛機，用座位系統，其係能夠最有效地利用乘讀㈣空間。 /本發明之另-目的係提供_種乘客載具之__曰用座位系統，其具有一大體上為不擁擠的外觀。本發明之進一步目的由以下的發明及本發明的特定具 13 593064 玖、發明說明體實施例之說明，對熟知此技藝之人士而言係為顯而易見的0 10 15 ，用乘客容納單元，其係用以提供乘客用之自備、個別的座位與睡眠舖位，該容納單元包含：支撐結構用於支撐該離開載具之地板的總成；一或更多的可移動乘客支承、結構性元件；以及用於將該可移動、結構性元件連接至該結構的構件，以致該元件係可選擇地在一座位形式，其中位在該一或更多之結構性、可移動元件上複數之乘客支承表面或是該支撐結構用以構成一乘客用座位，以及一床舖形式，其中複數之該支承表面係大體上共平面且連續地配置 ’用以構成-乘客用的床舖之間移動；其之特徵在於至少 —該可移動元件係為雙側的，包含第_與第二相對之側邊 ,該其中之—側邊具有_第_座位表面係在該座位形式中構成部分之座位，以及另—側邊具有一第二床舖表面係在 "亥床舖形式中構成該部分之床舖。 ★雙側、可移動、結構性元件可包含一内部、承重之具有第—及第二相對表面的膜片，以及第一與第二外坐塾層 20 =用以藉由分別地位在第—與第二表面上之該膜片加以支 2因此’該雙側的可移動元件之該一側邊，例如，可承發泡填塞層其之輪廓表面係按適當形狀製作，使用作為一座位元件，並且該另一 ^W透係可承载具有一大體上為旦表面的一發泡填塞層、_ 使用作為部分之床舖。該雙側 17私動之元件的該第一側邊 !你了具有一第一外觀，其係 14 593064 玖、發明說明有助於或是提昇-適於座位環境的整體客搶外觀。例如，該第-表面可具有-皮質或是仿皮質的座位外罩。該第二表面可具有一視覺外觀係有助於或是提昇-適於睡眠環境的整體客艙氣氛。因此，該第二表面係可裝上織物或是其 5他材料其之外觀通常與寢具材料結合的墊子。車乂佳地，该雙側疋件係為一背靠元件。該背靠元件係可與支撐結構連接，以致其係可選擇地在一第一大體上為直立位置與一第二傾斜位置之間樞轉，第一大體上為直立位置其中第一表面係配置用以構成部分之座位，以及第二 1〇傾斜位置其中該第二表面係配置用以構成部分之床舖。較佳地，月罪7G件之第二床舖表面，於第二傾斜位置中大體上係為水平的。於一些具體實施例中，一或更多的該乘客支承表面係可形成一座位底盤。該背靠元件係可與結構連接以致，於 15第一傾斜位置，背靠元件係覆蓋座位底盤。因此，根據本發明，該座位底盤可具有一專用的座位表面，其係按適當形狀製作並裝上墊子特別地係使用作為一座位。於床舖的幵7式中，座位底盤於第二傾斜位置係可藉由背靠元件整體或是部分地加以隱藏，以致座位底盤之座位外觀係由背靠 2〇所隱藏。於一些具體實施例中，該座位底盤可包括一或更多的該可移動元件，其係與該支撐結構連接用以在一上展開位置與一下儲藏位置之間具有一垂直元件的一方向上移動，以及座位底盤移動構件係配置當背靠元件係由直立位置移 15 593064 玖、發明說明動至傾斜位置時，用於將座位底盤從上展開位置移動至下儲藏位置。因此，於該第二傾斜位置，背靠元件係可佔用通吊'係由位在上展開位置的座位底盤所佔用之空間，在床舖形式中，座位底盤係可移至其之下儲藏位置。本發明之 5此特性容許座位總成之床舖表面能夠配置在離载具地板的一相對低高度的位置，使乘客易於攀登上床舖並且易於自床舖下床。於本發明之較佳的具體實施例中，一或更多的該乘客支承表面係包含一床舖延伸表面’在該座位形式中，該床舖延伸表面係配置或可展開而將座位向前或向後配置。該月罪元件可與結構連接，以致在該傾斜位置中該第二床舖表面與該床舖延伸表面構成一大體上連續的表面。該床舖 (伸表面係可配置或可展開而將座位底盤元件向前配置以致’在座位形式中’該床舖延伸表面係可使用作為_搁腳 b部分。該容納單元因而不具有一連接至座位底盤並可自座位底盤展開的腿靠元件。因此’本發明之容納單元可在與座位底盤之前方隔開的—位置處，包括-分__表面。於一些具體實施例中，一或更多之該乘客支承表面可包括-位在該背靠元件後方的背面延伸表面，並且該背靠 μ元件係可與結構連接，以致在該傾斜位置中，該第二床舖表面與該延伸表面大體上係為共平面的。於一些具體實施例中，於該傾斜位置中，該背靠元件係可與該背面延伸表面之前方隔開，並且配置一可移動充填元件’其係與該結構連接以致可在一儲藏位置與—展開 16 593064 玖、發明說明位置之間移動，當該充填元件展開時，該充填元件包括一 “支’充填表面’其係在該背靠元件與該背面延伸表面 k伸以致4背面延伸表面、充填表面以及第二床舖表面構成一大體上馮連、$的表面，並可配置構件當背靠元件自直立位置移動至傾斜位置時，用於將充填元件由該儲 =置移動至„亥展開位置。該充填元件可植轉地安裝在背件的後S位在背面延伸表面中間以致在儲藏位置中 ’充填元件係可與水平面成_以，並且—旦展開，係可 ίο _至展開位置。因此，於床舖形式中，可藉由一背面延申表面充填表面與一擱腳表面以及背靠元件的第二表面而構成床舖。本發明之床舖的總長至少為78叶〇.98公尺），並且於一些具體實施例中’長度係、可超過85忖(2.16公尺）。 15 較佳地，該背靠元件係與結構連接用於在一直立位置與-完全後仰位置之間選擇性地移動，其中背靠元件係相對於直立位置向後地搖動。於—些具體實施例中，一或更夕之4可移動70件係可包含_座位底盤，其係與支撐結構連接以致其係可在-第—與_第二位置之間相對於支樓結構枢轉，並且配置構件當背靠元件係自直立位置向後地枢 20 轉至完全後仰位置時，用於將座位底盤從第—位置漸進地樞轉至第二位置。出人意外地發現本發明之複數的乘客容納單元係可配置在飛機客艙中的商務艙部分，而不致㈣地減少座位數目。每-座位係界定-抽象的縱軸，相對於正常使用座位 17 593064 玖、發明說明的方式前後地延伸。頃發現假若每一乘客容納單元的配置方式係將其之抽象軸與飛機之縱軸成一對（⑶以如句角，角度範圍係在35至55度間，則在一飛機客驗中係可容納最大數目的本發明之乘客容納單元。 5 因此，根據本發明之另一觀點，提供一種乘客載具用，尤指飛機，座位系統其係包括複數之座位單元，每一座位單元界定-抽象的座位縱軸，並包括一支標結構係用以將座位單元附裝至載具地板，成型構件或是經配置用於形成包含一座位底盤與一背靠的一座位的構件；特徵在於該 10座位單几係配置用以構成一行（column)界定一抽象的縱行軸，該行中該座位單元係以縱向偏移的關係，在與抽象的行軸成一銳角下並列地配置，從而形成每一座位之背面空間，每一座位單元進一步土也包括成形構件或是經配置用於形成一大體上為平坦的床舖，床舖之主要部分係配置在座 15位位置的前方，床舖向後延伸進入該空間中用以伸展該平坦的床舖。較佳地該每一座位之背後空間大體上係為三角形或是梯形。該銳角典型地係位在30-60度的範圍中，較佳地係為 2〇 4〇-50度，例如，4〇度、μ度或5〇度。通常，該座位單元係安裝在該載具的一客艙中，該客艙係界定一抽象的客艙縱軸。該抽象的行軸大體上係可與該客艙軸平行，或是成一對銳角。因此，於一飛機客艙中，本發明之座位單元係可以“人字形（herringbone)，，的配置方式加以配置。 18 593064 玫、發明說明 ▲該座位單元可配置與載具之一側壁相鄰並且面向内。較㈣，该客艙包括二對置側壁，以及一行之座位單元係連績地配置或是接近地與每一側壁相鄰以致每一座位面向客艙内冑位在座位之背靠後方的一延伸表面與側壁相鄰 5地配置。座位因而可使其之背部至載具壁板，給予客驗一整體不擁擠的外觀。々客艙工間谷§午’則可將_或更多的附加行之座位單元朝向客驗之中心配置。假若在任一已知的客搶中能夠容納二中央行之座位，因而該等行之座位較佳地大體上係背 10 靠背地配置。每一座位單元較佳地進而包括一搁腳部分係配置在座 2前方。關腳部分因而能夠由座位❹者所使用，在飛行過程中處在-升高位置用以支撐他或她的腳，及/或在另一乘客探訪該座位使用者時能夠坐於其上。倘若配置該 15 -搁聊部分’則發現乘客不需將座位單元與—可移動腿靠結合作為部分之座位成型構件。於些具體貫施例中，每一 ^ /fr ® ^ -r ^ ^ 可庄诅早兀可進一步地包括前方。一第一隱私隔板，其係配置在該擱腳部分的 20 该座位成型構件以及該床舖成型構件係可包括一或更多的可移動乘客支承元件’其係具選擇性地配置用以，於座位形式下，至少構成部分的乘客用座位，或是，在床輔形式下，用以至少構成部分之該平坦的床舖，並且在床销形式下平坦的床位，係有利地配置在大體上與在座位形式下座位底盤相同之高度。 19 593064 玖、發明說明車乂佳地’母-座位單元在該位於座位背後的空間中包括一第―’較㈣麵固定的，《客支撐元件，當在床舖形式下“己該可移動元件時，該第一乘客支撑元件大體上係配置與該—或更多的可移動元件共平面，並係用以構成該部分的平坦床舖。該第-乘客支撐㈣大體上係可為三角形或是梯形。應察知的是，當座位單元係配置為床舖形式t帛乘客支撑TL件係、僅由_乘客使用，因此係可配置座位單元以致第-乘客支撐元件延伸進人由凹入之客艙 10 側壁所形成的一橫向凹部中，用以將客艙中空間的利用發揮至最大程度。 15 有利地，每一座位單元進一步地包括-第二乘客支撐元件’較佳地係固定至座位之_側邊，該第二乘客支撑元件大體上係配置與該第—乘客支#元件共平面，並係當在該床舖形式下裝配可移動元件時，用以構成該部分的:坦床舖’從而橫向地伸展該平坦的床舖。該第二乘客支撐元件大體上係可為三角形或是梯形。一座位單元之該第一固定元件大體上係配置與一相鄰座位單元之第二固定元件連續’並且該第一與第二元件係可藉由一第二隱私隔板而相互分開。第-與第二元件大體上係、佔用了座位後方的所有空間。因而本發明提供一座位系統，其係特別地適用在客機之一商務艙。本發明之座位系統提供具有背靠、座位底盤以及可任擇的搁腳部分的個別座位單元，於飛行期間用以容許乘客將其之腿部擱在一升高的位置。每一座位單元係 20 20 593064 玖、發明說明配置自備構件用於形成一大體上平坦的床舖，並藉由配置該平坦的床舖在座位後方向後地伸展，進入一由座位單元之配置所形成的一空間中，而能夠充分地利用客艙中空間。出人意外地，頃發現根據本發明能夠在客機之商務艙中 5提供長度上達7呎（2·13公尺）的平坦床舖，大體上不致犧牲乘客總人數。再者，專利申請人已發現可配置本發明之座位單元，用以帶給客艙一大體上不擁擠的外觀。該支撐結構係可由熟知此技藝之人士所熟知的任一適合、符合飛航標準、重量輕之材料所製成，並係可配備適 ίο σ的固疋構件，用於將座位單元固定至位在飛機客艙中的座位軌道。較佳地，支撐結構包括一護腋片（pile价）或底座（plinth)係用以附裝至該座位執道。根據本^ a月之另一觀點，提供一乘客載具用座位模組，該座位模組包含一座位部分、一搁腳部分、一單一的支 b撐、、、。構用於支擇該座位部分及該離開載具地板的搁腳部分以及附裝構件用於將該支撐結構附裝至位在載具之地板中的一對座位軌道；其之特徵在於該附裝構件包含二隔開的口疋邛刀用於將支撐結構在二隔開點處固定至該對軌道中的其中之一軌道’以及一單一的第三固定部分用於將支撐、"構固疋至另一軌道’從而在座位模組與座位執道之間提占式固定，該配置致使複數之該座位模組係可附裝至一對座位軌道，一個接著一個，從而構成複數之座位單兀母一座位單元包含一模組之座位部分，以及另一相鄰模組的擱腳部分。 21 593064 玖、發明說明已發現的是，根據本發明在一單一的座位支撐結構與一對座位執道之間使用一 3點式固定方式，容許該對之二座位軌道形成較大的撓曲度，如果在機身受到過度的應力時’例如’諸如如果發生緊急或是毀機落地（crash 5 landlng)狀況，彼此相對地移動，於是降低了結構在該等狀況下在一或更多的固定點處自座位軌道脫離的可能性。根據本發明之另一觀點，提供一種乘客載具，尤指飛機’用乘客座位總成，該總成係用以提供乘客用座位及睡眠設施，該總成包括： 0 —支撐結構，其係用以支撐離開载具地板的總成；複數之座位70件，其係包括一座位底盤元件以及一背罪元件4#元件包含第一與第二相對側邊，該其中之一側邊具有一第一座位表面，而另一側邊具有一大體上平坦的第二床舖表面； 15 20 或更多的輔助容納元件，其係與該支撐結構連接或疋構成為。卩刀之忒支撐結構，並係可配置或是可展開地與，亥座位並列配置’該或每一輔助容納元件具有一輔助的、大體上為平坦的乘客支承表面；以及其係用以將座位元件連接至支撐結一座位移動機構構’該座位移動機構包括—座位轉換子機構，其係用以容制座位TL件移動’以致座位元件能夠具選擇性地在一用以提供乘客用座位的座位形式，與用以提供乘客用床舖的床舖形式之間移動，該座位轉換子機構係用以控制背罪几件的移動，以致該背靠元件係可由—第—直立位置， 22 593064 玖、發明說明其中背靠元件的該第-座位表面與該座位底盤元件配合用於構成座位，樞轉至-第二傾斜位置，其中第二床舖表面大體上係配置與一或憂客的兮絲& + _ 乂灵夕的，亥辅助乘客支承表面共平面或是連續，用以構成床舖。 5 目此’根據本發明，提供—種乘客座位總成，其係具有複數之可移動座位元件，係用以構成一座位。座位總成同時能夠轉換成一床舖形式，其中背靠元件及一或更多的輔助7L件構成-乘客用睡眠表面。本發明之特徵在於，背靠元件具有第一表面係特別地用以使用作為一座位表面， 10以及第二相對表面係特別地用以使用作為一睡眠表面。較佳地，該座位移動機構係用以控制該座位底盤元件及省方罪元件彼此相關地移動。該座位轉換子機構係可用以控制該背靠元件的移動，以致當背靠元件係自第一位置移動至第二位置時，該背靠元件係向前地搖動覆蓋座位底 15盤元件，並且位在第二傾斜位置的該背靠元件係疊置覆蓋座位底盤元件。有利地，因此在床舖形式中，座位底盤元件與背靠元件之第一座位表面皆未構成部分之床舖表面，因而可以特別適於座位使用的材料為座位裝上墊子。同樣地，在座位形式中，並不使用背靠之第二床舖表面以構成 20部分之座位，因此該床舖表面係可以特別適於使用作為床舖的方式裝上墊子。再者，在座位形式及床舖形式中，分別使用為座位元件裝上墊子的材料彼此間係可上不同的顏色’及/或具不同的紋理，及/或不同的圖案，當本發明之所有或大部分之該等乘客總成係裝配成該其中之一方式日寺 23 593064 玖、發明說明，俾便在飛機客艙中產生_第—氣氛或_，，情境，，，而當所有或大部分之該等乘客總成係裝配成該另一方式時，產生第二不同的氣氛或一”情境，，。背靠元件之該一表面可承載 -具有輪廓相符之第—表面的發泡塾塞層，其係用以構成月Λ或疋刀之座位背靠，而另一表面可承載一具有一大體上平坦的第二表面的發泡墊塞層，其係用以構成部分之床舖。该座位轉換子機構係可用以控制座位底盤元件之移動 ’以致當背靠元件係自第_直立位置移動至第二傾斜位置 10時，該座位底盤元件係受引動相對於支撐結構向下地移動。因此，座位總成之床舖表面係可配置在離載具地板一相對低高度的位置，對乘客而言係易於攀登上床舖及下床。較佳地，配置適合的馬達裝置用於自動地在直立與傾斜位置之間移動背靠元件，以及配置可由使用者操作的控 15 制裝置用於控制馬達裝置之作動。忒座位移動機構較佳地進而包括一座位後仰子機構，其係用以容許該座位具選擇性地自一直立位置後仰至一完全後仰的位置，該座位後仰機構係用以控制背靠元件的移動，以致當座位係自直立位置後仰至完全後仰的位置，該 20背靠元件向後地自第一直立位置搖動至一第s完全後仰的位置。該座位後仰子機構係可有利地進而用以控制該座位底盤元件之移動，以致當背靠元件係自第一直立位置向後地搖動至第三完全後仰的位置時，導致該座位底盤元件向後傾斜。因此，於完全後仰的位置中，背靠元件與座位底 24 593064 玖、發明說明盤元件係可分別地疋向用以提供使用座位總成之乘客一符合人類工程學舒適的就座位置。背靠元件之後仰動作與座位底盤元件之傾斜動作係可在該可由使用者操作的控制裝置之控制下機動化。 5 較佳地，一或更多之該輔助容納元件係配置或可展開地配置在座位的别方或是後方。於一些具體實施例中，一或更多之該輔助容納元件係可包括一搁腳部分，係配置或可展開地配置在該座位的前方，並且於該第二位置中，背罪凡件之第二床舖表面大體上係配置與該擱腳部分共平面 10 並連續。 -或更多之該輔助元件係可包含_固定的背面延伸表面，配置在座位的後方。於一些具體實施例中，該座位總成可進-步地包括-可移動充填元件，以及該座位轉換子機構係可用以容許該充填元件在一下、儲藏位置與—升高 15、可展開位置之間移動，其中該充填元件在該第二傾斜位置延伸大體上與該背靠元件之該第二表面共平面並連續，以及該背部延伸表面，從而構成一大體上平坦、伸展的床舖表面。該座位轉換子機構係可進一步用以控制該充填元 2。2的移動，以致當背靠元件係由該第-直立位置移動至該傾斜位置時，該充填元件係受引動由該儲藏位置移動 f該展開位置。該充填元件係、可樞轉地與背靠元件之下端部連接_’以致當背靠元件係由第一位置移動至第二位置時充填70件係丨動由儲齡置移動至展開位置。該座位轉換子機構係可包含一座位支撐袭置，其係拖 25 593064 玖、發明說明轉地與支撐結構連接，用於在一第一座位位置與第二床舖位置之間搖動。該背靠元件係可安裝在支撐裝置上，以致背靠元件係可藉由將支撐裝置由該第一位置搖動至該第二位置，而能夠自第一直立位置樞轉至第二傾斜位置，以及 5可提供可鬆開的固定裝置用於具選擇性地將支撐裝置固定在第一及第二位置。於一些具體實施例中，該座位支撐裝置係可包含二相對的搖動板。該搖動板係可藉由一或更多的扭力管互連。該座位底盤元件係可樞轉地安裝在支撐裝置上，該佈置以致當支«置係由第一位置搖動至第二位置時，座位底盤元件係受引動由一上展開位置向下地移動至一下儲藏位置，並且背靠元件係受引動向前地搖動覆蓋座位底盤元件，以致在第二傾斜位置，背靠元件係覆蓋座位底盤元件。座位底盤元件相對於背靠^件係可包括—前端部以及一 15後端部，並且座位底盤元件係可在該後端部處或是朝向該後端部樞接至支撐裝置。方便地，該座位移動機構進一步地包括一座位底盤支 «置，用於支撐座位底盤元件的前端部。該座位底盤支撐裝置係可包含-滑道，其係配置在座位底盤元件的下方 π、-腳構件具有二相對端部，該其中之—端部係可拇接至座位底盤元件的前端部’而另—端部係可滑動地於該滑道中嗜合，以及-拖戈支柱係將腳構件的另_端部連接至支撐裝置，該配置以致當支撑襄置係自第一位置搖動至第二位置時，移動拖良支柱用以引動或是容許腳構件之該另一 26 玖、發明說明 W在滑道中滑動，該滑道所具之外形以致當支撐装置從第-位置移動至第二位置時，腳構件係向下移動，從而致使或容許座位底盤元件之前端部漸進地向下移動。該腳構件係可在該-料處轉至錄底m 端部處係樞接至該滑道。於—此且…"由在3亥另一些具體貫施例中，座位底盤几件之前端耗可藉由二„件切，每—㈣件係滑動地與和座位之—個別橫向側並列的—個別滑道中喷合。 10 較佳地，座位移動機構進一步地包括一座位㈣子機構’當該支撑裝置係配置在第一座位位置中時，其係用以容許該座位元件具選擇性地在一直立位置與_完全後仰位置之間移動。該座位後仰子機構包括一曲線的執道，其係附裝至支撐裳置歧構成在支撐裝置中，並具有二相對之執道端部 1 以及稷數之間隔開的軌道從動件係附裝至該背靠元件， 15該執道從動件係用以沿著軌道口齒合並滑動，裝配執道以致 f執道從動件沿著軌道從—端部滑動至另_端部，引動背靠元件漸進向後地從第一直立位置搖動至一第三完全後仰置"亥座位後仰子機構可進一步地包括一可具選擇性操 20作的雙向傳動裝置，其係用於平移地將該背靠元件相對於支標裳置而移動，該配置致使該傳動裝置作動將轨道從動件〜著曲線軌道滑動，從而致使背靠元件漸進地在該第一與第三位置之間搖動。有利地，該傳動裝置可包括一線性致動器係於背靠元人亥支樓扁置之間連接。例如，諸如一線性螺桿（linear 27 593064 玖、發明說明 rew)或疋滾珠螺桿（ball screw)的一線性致動器，其係可在第與第二位置之間的任一中間位置處停止，從而容許月罪7L件在第一與第三位置之間連續地後仰，並可在任一所需的中間位置處停止。 5 於一些具體實施例中，該線性致動器可包括一線性螺桿或是滾珠螺桿固定地牢固至支撐裝置、一螺桿嚙合裝置樞接至背靠元件以及一藉由該支撐裝置所承載的可具選擇性麵作的雙向馬達，用於轉動地傳動該線性或是滾珠螺桿。該座位底盤元件相對於背靠元件可具有一前端部以及一 10後端部，並且該線性致動器可樞轉地於支撐裝置與座位元件之間連接，該線性致動器係於該後端部處或是朝向該後端部處附裝至座位底盤元件，用於相對於支撐結構漸進地向下傳動該座位底盤元件，從當背靠元件係位在該第一直立位置時的一第一上位置至當背靠元件係位在該第三完全後仰位置B守的一第二下位置，並且該座位移動機構可進而 I括座位底盤支撐裝置，用於當座位底盤元件之後端部係又傳動向下時，支撐座位底盤元件之前端部，從而致使座位底盤在背靠元件向後搖動時漸進地向後傾斜。因此，於直立位置，背靠元件係大體上可為直立的方向，並且座 2〇位底盤凡件大體上係可水平地配置。於完全後仰的位置，月Λ元件係相對於直立位置向後搖動，並且座位底盤元件係相對於直立位置向後傾斜用以構成一舒適的倚靠座位位置。較佳地，曲線執道之外形、線性致動器之長度與位置、介於線性致動器與背靠元件及座位底盤元件之間樞軸的 28 593064 坎、發明說明位置、以及座位底盤支撐裝置的形式，致使當座位係自直立位置漸進地後仰至完全後仰位置時，其係移動經過一系列的預定、符合人類工程學舒適的座位位置。於該預定位置的中間位置，曲線軌道之外形等係可由内插法所決定。 5於一些具體實施例中，為了容許背靠元件及座位底盤元件採用前述符合人類工程學舒適的位置，線性致動器可經由一無效運動裝置（lost motion device)與背靠元件連接，容 σ午在座位底盤元件及背靠元件之間小程度地相對橫移。該座位轉換子機構可包含一可具選擇性操作的雙向致 10動器，用於將該支撐裝置固定在該第一座位位置與該第二床舖位置之間。該致動器可包括一四桿雙搖動連桿組 (four-bar double-rocker linkage)，該連桿組包括一搖桿與連接裔連桿係在該支撐裝置與該搖桿中間連接，以及可具選擇性操作的雙向旋轉式傳動裝置，用於作動該搖桿，該 15配置致使搖桿作動導致該支撐裝置在該第一與第二位置之間搖動。該旋轉式傳動裝置可包括一馬達、一蝸輪（w〇rm gear)以及一蝸輪（w〇rm wheel)，其中蜗輪（w〇rm wkd)係固疋地牢固至搖桿。一蝸輪（w〇rm gear)/蝸輪（w〇rm wheel) 裝置係為一不可逆（non_reversible)裝置，因此有利地，例 20如，在體重過重的乘客猛烈地坐入座位之狀況下，對支撐裝置所造成之過度的力量並未經由蝸輪（w〇rm gear)/蜗輪 (worm wheel)裝置傳達至馬達。再者，旋轉式傳動裝置係固定在第一與第二位置。然而’為了在需要時容許將支撐裝置手動地在該第一 29 593064 玖、發明說明與第二位置之間搖動，例如，在飛機客餘中該馬達或是電力故障狀況下’蜗輪（WGnn gear)可自堝輪（贈m她叫脫離。該致動器係可附裝至座位總成之支樓結構，位在該座 5位几件下方。6亥支撐裝置係可包括二間隔開的侧構件，其係分別地配置在背靠元件之相對側邊上。該連接器連桿係可與侧構件連接，位在支樓裝置與該支撐結構之間的植轴點下方。因此，本發明提供一種載具用，尤指飛機，乘客座位 10總成，其中一背靠元件係安裝在一支撐結構上，以致為了乘客的舒適性由一直立位置向後地後仰至-後仰位置，並能夠向前地樞接至一大體上水平的傾斜位置覆蓋一座位底盤元件的頂部。座位底盤元件以及背靠元件之一第一表面 ’其係裝上好使其適於作為_座位。然而，背靠元件之 15第二反向表面係使用作為一床舖表面。座位可包括一，而較佳為二，固定或可展開的辅助延伸表面位在座位之後方及/或前方’並且背靠元件係樞接至支撐結構，以致在樞接至第二傾斜位置時，其係與其中之一的延伸表面接觸，用以與其構成一大體上為連續的表面。可配置一可移動充 20填兀件，用以充填在背靠元件與另一延伸表面之間所提供之空間。本發明之座位總成因而能夠由一座位轉換成一床舖，其甚至能夠容納身材高大的乘客。有利地，本發明之座位總成係可相對於飛機客艙之縱抽成-35度與55度之間的角度，較佳為4〇至5〇度，以致位 30 593064 玖、發明說明在背靠元件後方的一延伸表面係延伸進入由一典型凹入的飛機客艙内壁所形成的一凹部中。儘管與凹入客艙壁並列的客艙區域並不適合，並且淨空高度（headroom)不足，用以容納位在直立位置的背靠元件，但其係可根據本發明用 5以容納背部延伸表面，在床舖形式中，係構成部分的床舖表面。延伸表面、充填元件以及背靠元件的第二表面，較佳地係裝上以發泡墊塞或是任何特別適於使用作為床舖的等效材料所製成的墊子。因此，本發明之座位總成的床舖表面係可具有一大體上平坦的表面，在展開時大體上係為 10 水平的。可進一步地察知的是，當該座位總成係配置為座位形式時，將背靠元件直立，位在座位後方的背部延伸表面大體上係受隱藏並形成一有用的儲藏空間。方便地，該儲藏空間係可用以儲藏僅在座位總成轉換成床舖形式時所需之 15寝具材料。例如，由位在背靠元件後方的背部延伸表面所形成的儲藏空f曰1,係可用以儲藏一羽絨被（duvet)及/或— 毯子與-或更多的枕頭。有利地，該等寢具材料在座位總成處在座位形式時係受隱藏，帶給客艙_整體整齊的外觀。當將座位總成轉換成床舖形式時，背#元件係向前搖動覆蓋座位底盤元件之頂部，用以露出背部延伸表面，並容許輕易地取用儲藏在背部延伸表面上的寢具材料，其係: 夠手動地在床舖表面上展開。 ’' 根據本發明之另一觀點，描报括士蜆點挺供一種特別係在，例如機’之載具上使用的後仰座位總成’其係包括一固定的支 31 593064 玖、發明說明樓4刀’用以支撐載具之地板總成、一可後仰的座位部分，其係包含一座位底盤以及一背靠'以及座位連接裝置係用以將该座位部分與該支撐部分連接，該連接裝置包括一座位後仰機構係用以容許並控制該座位部分在一第一直立位置與第一完全後仰位置之間的移動，以及可具選擇性 ’、乍之雙向馬達裝置，係用以在該第一與第二位置傳動該座位部分；其中該座位後仰機構包括一不可逆線性致動器於該馬達裝置與該座位部分之間連接。 4不可逆線性致動器係可包括一引導螺桿傳動裝置或 1〇是一滾珠螺桿傳動裝置，或是任何其他等效、不可逆的裝置。在第一直立位置與第二完全後仰位置之間，使用該一不可逆致動器用於傳動座位部分，所具有的優點在於，施力在座位刀白勺過度強烈或是突發的力i並未傳達至馬達 15 從而p牛低對馬達造成損害的風險，並因而延長其之壽命例士 $ Μ重過重的乘客驟然地坐人他或她的座位部分:因而對座位部分造成一突發、強烈的力量，該強烈的力量並未經由不可逆線性致動器傳達至馬達裝置。線性致動器可包括-線性螺桿或滾珠螺桿，附裝至該 20 支撐部分與該座位部分之其中之一部分（或是一部分連接），以及-螺㈣合裝置係附裝至該座位部分與該支撐部分之其中的另-部分（或是-部分連接）。於一些具體實施例中，線性致動器可與座位底盤連接，用於沿著相對於支樓部分，介於-第一位置與—第二位置之間的一預定線性路徑，傳動該座位底盤。 32 593064 玖、發明說明該座位底盤相對於背靠可具有一前端部及一後端部，以及線性致動器係可在該後端部處或是朝向該後端部轉至座位底盤，並係可配置用於在其由第一位置移動至第二位置時向下地傳動座位底盤之後端部。該座位後仰機構可 5進-步i也包括-支撑裝f，當座位底盤之後端部向下傳動時，用於支撐座位底盤之前端部，從而當背靠向後搖動時 ’致使座位底盤向後傾斜。線性致動裔係可交替地或是附加地與背靠連接，用於在一第一直立位置與一第二後仰位置之間平移地傳動背靠 10 。該座位後仰機構可進一步地包括一引導裝置，當背靠係由第一直立位置移動至第二完全後仰位置時，用於相對於支撐部分漸進向後地搖動該背靠。該引導裝置係可包括一曲線執道，其係附裝至支撐部分或是一部分與支撐部分連接，以及複數之隔開的執道從動件，其係附裝至背靠，該 15軌道從動件係用以沿著該執道嚙合並滑動。有利地，線性致動器係可樞接至座位底盤，並可經由一無效運動裝置樞接至背靠，用以容許在座位底盤與背靠之間相對的樞轉與平移的移動，為了容許在背靠與座位底盤之間移動的自由度，而使該等座位元件能夠採用複數之 20相對、預定的、符合人類工程學之舒適的位置。於本發明之另一觀點中，提供一種具有一可後仰背靠的座位，該座位包括一固定的支撐部分，其係用以支撐該離開地板的座位、一座位部分包括一可後仰的背靠以及座位連接構件，其係用以將該座位部分與該支撐部分連接， 33 593064 玫、發明說明 5 10 15 錢接構件包括背靠後仰機構，其係用以容許並控制背靠在』一第一直立位置與一第二完全後仰位置之間的移動；其々中該背靠包括一具有一上端部的第一下背靠構件，以及— j上月罪構件’其係豐置在該背靠構件上，並係在上端部處或是朝向上端部而樞接，俾便於其間傳動平移移動，並且其中該背靠後仰機構包括附裳至支撑部分或是一部分與該支撐部分連接的第一與第二伸長引導執道，該第一軌道具有二相對的軌道端部、複數之第一隔開的執道喃合從動構件丨係附裳至第一背靠構件並用以於該第一軌道令，合並滑動’以及一第二軌道喃合從動構件，其係附裝至弟-背靠構件或是-部分與該背靠構件連接，並用以於該第二軌道中唾合並滑動’該第-軌道係為曲線的，以致當第一軌道喃合從動構件沿著第—執道從—端部滑動至另一端部時，致使背靠構件在第一直立位置與第二完全後仰位置之間相對於支樓部分漸進地搖動，以及該第二軌道的外形致使當該第二軌道喃合從動構件係受影響沿著該第二軌道滑動時，致使第二背靠構件相關於第一背靠構件漸進地搖動。 20 〃此有利i也i與下背靠構件在直立與完全後仰位置中係可具有不同的相對配置。再者，上與下背靠構件之相對配置在直立與凡全後仰位置之間係可連續地調整。較佳地，於第一直立位置，μ沏土上人下者罪構件彼此大體上係為共平面地配置，用以構成-大體上平坦的背靠表面。於第二完全後仰位置，上ik下北土 " ，、下月罪構件係可為一對鈍角，以致下 34 593064 玖、發明說明月罪構件係以較上背靠構件為大的角度自直立位置傾斜。因此下背讀件係可構成_腰椎支撐部分供制座位乘客所用。 /玄背靠後仰機構係可包括具有成-對純角之二臂的一 5搖才干，該搖桿係在該二臂中間的一位置處拖接至第一背靠構件，該其中之一臂承載該第二軌道端合從動構件，以及具有二相對端部的一連桿，該其中之一端部係樞接至純 · 桿的另-臂，而另一端部係固定地牢固至第二背靠構件； # 該配置致使當第二從動構件係受影響沿著該第二軌道滑動 10 ’搖桿係受影響相關於其之峰搖動至第一背靠構件，從而致使該連桿相關於其之樞轴樞轉至搖桿的另一臂，從而致使第二背靠構件相關於其之樞軸枢接至第一背靠構件。忒背菲後仰機構可進一步地包括用於限制搖桿及/或連桿的移動的構件。 15 5亥座位連接構件可進一步地包括一可具選擇性操作的雙向線14致動器，其係在支撐部分或是與支撐部分連接的 · 一部分與該背靠之間連接，用於相對於該支撐部分平移地移動該背靠，該配置致使當背靠受引動而相對支撐部分平移地移動時，位在第一背靠構件上的第一從動構件係受引 20動而沿著第一軌道漸進地滑動，從而致使背靠在第一直立位置與第二完全後仰位置之間漸進地搖動。。亥座位部为大體上包括一座位底盤。該線性致動器可與座位底盤連接，用於將該座位底盤沿著一預定的線性路徑由第一位置與第二位置之間移動。該線性致動器可樞接 35 593064 玖、發明說明至座位底盤。有利地，線性致動器可樞轉地藉由-無效運動裝置而與背靠結合。以下係僅參考本發明之具體實施例的伴隨圖式經由實例所作的說明。 5 圖式簡單說明圖式中：第1圖係為-飛機機身的一前部分的截面、概略平面圖’顯示本發明之一種包含複數之個別的座位單元的座位系統。 1〇帛1A圖係為第1圖之部分的放大視圖，顯示三相鄰的座位單元。第0係為第1A圖之二相鄰的座位單元的等角視圖。 ;第2圖中，其中之一座位單元係顯示為直立座位形式，另-所示為後仰座位形式，以及第三者係顯示為一床舖形 15式。第2 A圖係顯示於第2圖中所示類型的個別座位單元的一支撐結構的一部分，其中將可移動座位元件移開。第3圖係為本發明之一種載具用第一乘客座位總成的概略側視圖，係顯示一直立的座位形式。〇第4圖係為第3圖之第一乘客座位總成的另一概略的側視圖，係顯示一完全後仰的座位形式。、第5圖係為第3及4圖之第一座位總成的另一概略的側視圖，係顯示一床舖形式。第6圖係顯示第3至5圖處在直立座位形式之第—座位 36 593064 玖、發明說明總成的部分的一等角視圖，其中將坐墊移除。土第6A圖係為構成部分之第6圖的第_座位總成的一背罪元件的一側視圖。第6B圖係為第从圖之背靠元件的_#角視圖。 5 第7圖係為在第6圖中所示之部分的第-座位總成之另 -等角視圖’其中座位總成係處在完全後仰的座位形式。第8圖係為第6及7圖之部分的第—座位總成的另_等角視圖，其中座位總成係處在床舖形式。第9圖係為第3至8圖之部分的第—座位總成的—座位 10移動機構的一等角視圖’其十所示為床舖形式。第10圖係為第9圖之部分的座位移動機構的一側視圖 ’其中所示為座位形式。第U圖係為第9及1〇圖之部分的座位移動機構的另一側視圖，其中所示為床舖形式。 5帛12圖係為第9至11圖之部分的座位移動機構的-放大的等角視圖。第13圖係為第3至8圖之第—座位總成的部分之座位後仰子機構的一等角視圖。 20 第Η圖係為第3至8圖之第一座位總成的部分之座位轉換子機構的-等角視圖’其中所示為床舖形式。第15圖係為第14圖之部分的座位轉換子機構的另一等角視圖，其中所示為-座位形式將一蜗桿（w_sc叫自 -對應的蜗輪(_m gear)中移開，用以容許在座位與床舖形式之間手動地移動座位轉換子機構。 37 593064 玖、發明說明第16圖係為第14及15圖之部分的座位轉換子機構之- 放大、截面側視圖。第17圖係為本發明之另一座位系統的一截面、概略平面圖。 5 帛18圖係為本發明之—乘客容納單元的-等角視圖，其中所示係為一座位形式。第19圖係為第18圖之一乘客容納單元的—等角視圖，其中所示係為一床舖形式。第20A-20C圖係顯示第18及19圖之乘客容納單元在床 10舖形式與座位形式之間互相轉換的概略側視圖。第21A圖係為第18及19圖之乘客容納單元的一概略、等角視圖，顯示一乘客使用處在座位形式下的座位。第21B圖係為第18及19圖之乘客容納單元的一概略、等角視圖，顯示一乘客使用處在床舖形式下的座位。 15 第22圖係為本發明之另一容納單元的一等角視圖，其中所示為一座位形式。第23圖係為第22圖之乘客容納單元的一等角視圖，其中所示為一床舖形式。第24A圖係為第22及23圖之乘客容納單元的一概略、 20等角視圖，顯示一乘客使用處在座位形式下的座位。第24B圖係為第22及23圖之乘客容納單元的一概略、等角視圖，顯示一乘客使用處在床舖形式下的座位。第25圖係為第22及23圖之乘客容納單元的一變化形式的等角視圖，其中係包含一滑動座位底盤。 38 593064 玖、發明說明第26A_26C圖係概略地顯示滑動座位底盤之不同位置的側視圖。第27圖係為第22及23圖之乘客容納單元的另一變化形式的等角視圖。 5 第28圖係為一飛機機身之一前部分的上及下甲板的概略、截面平面圖，顯示本發明之另一座位系統應用在一波音747-400⑧型飛機之上與主甲板。第29A圖係為本發明之一第二乘客座位總成的一概略側視圖，其中所示的座位總成係處在進餐位置。第29B圖係為弟29A圖之第二乘客座位總成的一概略側視圖，其中所示係處在一中間後仰位置。第29C圖係為第29A及29B圖之第二乘客座位總成的一概略側視圖，其中所示係處在一完全後仰位置。第30A圖係為第29A至29C圖之第二乘客座位總成的一 15 概略側視圖，其中所示係處在另一中間轉換位置。第30B圖係為第29A至29C圖以及第30A圖之座位總成的一概略側視圖，其中所示係處在床舖形式。第31圖係為包括本發明之複數的乘客總成的另一座位系統的一概略平面圖。 20 第32圖係為包括本發明之複數的乘客座位總成的另一座位系統的一概略平面圖。第33A圖係為本發明之第三乘客座位的一概略側視圖 ’其中所示之座位總成係處在一座位形式。第33B圖係為第33 A圖之第三座位總成的一概略側視 39 593064 玖、發明說明圖，其中所示係處在一中間位置。第33C圖係為第33A及33B圖之第三總成的_概略正視圖，其中所示係處在一床舖形式。 L實施方式；3 5 較佳實施例之詳細說明一客機大體上包括具有一前端部與一後端部的一中空、心軸狀（spindle-shaped)機身。於伴隨圖式之第i圖中所示的一實例，一典型的飛機機身1〇之一前端部部分12其係配置朝向前端部11。該機身10於前端部與後端部之間，係 10藉由在第1圖中鏈點線A-A所示界定一飛機縱軸，並且機身 10係朝向前端部11推拔，用以構成一鼻部分15。機身10容納飛機之多種性能與設施，包括一或更多的乘客客艙20、21。配置在一特定飛機上乘客客艙2〇、以之數目與尺寸，係視在機身中供乘客客艙所適用之空間以及 15對於乘客客艙所需形式而定。本發明並未限定使用在任一特疋形狀、尺寸或是客艙數目上。然而，於第丨圖中，僅係為一實例，如圖中所示二客艙2〇、21係位在機身的前部分12中，一第一客艙2〇係位在飛機之鼻部分15内，以及一第二客艙21係配置在第一客艙20後方，一公用區域22係配 20置在二客艙20、21之間。如第！圖中所示，該公用區域22 可包括一廚房23以及一或更多的乘客盥洗室24。如第1圖中所示，一飛機客艙20、21大體上係由機身 1〇之内部表面的二相對表面部分26、28所形成。實際上， ^相對表面部分26、28構成客艙20、21之相對側壁。於機 40 593064 玖、發明說明身内各舶20、21同時包括一地板或甲板3〇，其係由適當的基礎結構（未顯示）所支撐，以及一天花板（同時未顯示）位在地板3 〇上方於相對側壁之間延伸。該相對側壁2 6、2 8通 ΐ 乂複數之預製、合成被板加以襯倚使客艙内部具有引人 5 /主目的外觀，並在客艙20、21與飛機外部之間提供絕熱作用。嵌進於地板30中的機身之基礎結構，其包括為熟知此技藝之人士所廣為熟知類型之複數對座位執道32、34，如第1圖中虛線所示。每一成對的執道大體上係為線性的， 1〇並且包括一對大體上平行的軌道，其係用於將複數之座位或是其他的裝置固定地牢固至飛機之基礎結構。大體上，一飛機客艙20、21包括二外對之座位執道32，每一軌道係配置與二對置客艙側壁26、28的其中之一個別的側壁相鄰。如空間容許，一客艙20、21同時可包括一或更多的中央 15對座位執道34，其係配置在外對座位執道32的中間。如第 1圖中所示，第一客艙20包括一單一中央對之座位軌道34 ’同時第二客艙21包括二並列的中央對之座位軌道34。典型地，一中央對之座位執道34大體上係平行於飛機縱軸 Α而延伸。在一飛機客艙21係配置朝向機身1〇之一中央部 20分，而離開飛機之前端部與後端部處，例如，諸如第i圖中的苐一客舶21 ’客知21之相對側壁2 6、2 8大體上係平行於飛機縱軸A-A而延伸，並且外對之座位軌道32係依循側壁26、28之直線，因而同時大體上係平行於飛機縱軸A-A 而延伸。然而，朝向飛機之鼻部分15，該相對側壁26、28 41 593064 玖、發明說明係為拱形的並朝向前端部11收斂。因此，於該等狀況下，外對之座位執道32係相關於飛機縱軸A-A成一對銳角。每一客艙20、21容納複數之座位單元40。如第1圖中所示，位於每一客艙20、21中，座位單元40係配置用以構 5 成為複數行29之座位單元，如以下所詳述。每一行29係固定地牢固至個別對之座位軌道32、34，並且大體上與其平行地延伸’並界定一如第1圖中線B-B所示之抽象的行軸。如第1圖中所示，第一客艙20包括二行29之座位單元40，該每一行29係固定地牢固至該外對之座位執道32的其中之 10 一個別的執道。當位在第一客艙20中該外對之座位軌道29 係相關於飛機之縱軸A-A而傾斜，於第一客艙中每一行29 之座位單元40的抽象行軸B-B，同時係與飛機之縱軸a-A 成一對銳角。第二客艙21包括二外行29之座位單元4〇,以及一互相並列的中央行2 9之座位單元4 〇。每一外行2 9係附 15裝至該外對之座位執道32的一個別執道，並且每一中央行 29係附裝至該中央對座位執道34的一個別軌道。如以上所述，该中央對座位執道34大體上係平行於飛機縱軸A_A而延伸，因此每一中央行29之座位單元40大體上同時係平行於飛機縱軸A-A而延伸。於第二客艙21中，每一外對之座 20位軌道32大體上同時係平行於飛機縱軸A-A而延伸，因此第二客艙21之每一外行29大體上係平行於飛機軸a_a而延伸。第1A及2圖係顯示構成部分之第丨圖之其中的一行的三相鄰座位單元40。每一座位單元4〇包括支撐結構42用於將 42 593064 玖、發明說明座位皁兀附裝至地板30。該支撐結構42係可以熟知此技藝之人士所熟知的任何適合方式製成，但較佳地包括一承重的、航太等級的鋼質次框架（未顯示），係以一或更多之按形狀適當製作的合成嵌板加以包覆。每一座位單元4〇具有 5 一前端部51、一後端部52以及二相對侧邊53、54。與後端部52並列的支撐結構42,其係包括一座位外殼43，如第2A 圖中所示，其大體上形成一立方體的凹部44。對於該凹部 44之後方，支撐結構42形成一第一、大體上平坦且一般係為二角形的表面47，當座位單元4〇係安裝在一客艙2〇、21 10中時，其係大體上平行於客艙20、21之地板30延伸，但稍有傾斜，如以下的詳細說明。與座位單元4〇之一第一側邊 53並列的支撐結構42，其係形成大體上平坦且一般係為三角形的表面48，其大體上係與第一表面47共平面，並且於一些具體實施例中，如第2及2A圖中所示，其大體上係與 15第一表面47連續。該每一第一及第二表面47、48係足夠堅固’用以支撐一乘客的至少部分重量。該第二表面48具有一第一凹入橫向邊緣45，其係由座位外殼43之一前端部向外並向後地延伸至位在外殼43之前端部與座位單元4〇之後端部52之中間點46。該第一及第二表面47、48形成一大體 20 上為線性的第二橫向邊緣49，其係自該點46向後並向内延伸至座位單元的後端部52。該第一與第二表面47、48因而延伸至後方及立方體凹部44的其中之一側邊，並形成該凹部44的上部分。該第一及第二表面47、48係藉由支撐結構 42支稽在離客艙2〇、21之地板30的一預定高度處。 43 593064 玖、發明說明位在座位單元40之第二側邊54處，座位外殼43包括一直立的拱形隔板60,其係具有一凸面的後部分㈣座位單元40之後端部52延伸至立方體凹部仰―後端部，以及一大體上線性則部分6 2其係在凹部4 4的前與後端部之間延伸。該後凸面部分61如第1A圖中所示於平面圖中具有一曲度 ’其係與第二表面48之第一凹入橫向邊緣45的曲度一致。該隔板60大體上係延伸高於第一及第二表面fa，並使用作為ί、使用座位單元40之乘客的隱私隔板，環繞著座位單元40之後端部52與第二側邊54。 1〇 #座位單元4G之前端部51並列的支撐結構42，其係包括一軟塾凳（ottoman)由地板3〇向上延伸，並具有一大體上平坦的上表面66。該上表面66係用以承載一坐墊67，其之厚度致使所配置的坐塾67大體上係與第-及第二表面47、 /、平面"亥软墊无65係足夠堅固用以支擇一乘客的重量 15 ’广致如有需要，坐墊67係可使用作為一輔助座位。該支撐…構42進一步地包括一相對小、辅助的隱私隔板68，環繞著座位單元40之前端部51。邊立方體凹部44接受複數之可移動乘客支承元件，其係藉由-將於以下詳加說明的座位移動機構，與支樓結構 2〇連接。該可移動乘客支承元件包括一座位底盤71與一背靠 72座位移動機構容許乘客支承元件具選擇性地裝配，用以提供一乘客用座位，如第2圖中所示之中央與右手邊的座位單元40，或疋一床舖如第2圖中所示之左手邊的座位單兀40。於座位形式中，可移動乘客支承元件”、72係可 44 593064 玖、發明說明具選擇性地在如第2圖之右手邊的座位單元4〇所示一直立或用餐位置，以及如第2圖之中央座位單元4〇所示的一後仰或是倚靠位置之間移動。該可移動乘客支承元件71、72係經由座位移動機構附 5波至支樓結構42以致，在座位形式中，座位底盤7丨係容納在外殼43之立方體凹部44内，並且背靠72係自凹部44向上延伸至座位底盤71的後方，並在座位單元4〇之第一與第二側邊53、54之間橫向地延伸。因此，如一使用座位單元的乘客所感知，座位單元40界定一抽象的座位縱軸，其係 1〇在座位單元40之前與後端部51、52之間延伸，並係如第1A 圖中的虛線C-C所示。於完全直立的位置中，座位底盤71大體上係配置與外 λ又43之第與第一表面47、48相同高度處，並係與軟塾覺 65之後方隔開，以致坐墊67提供使用座位單元扣之一乘客 15所用的擱腳部分。於後仰的位置中，背靠72係相對於其在直立位置中的位置後仰，並且座位底盤71係稍微向後傾斜，用以提供一符合人類工程學之舒適的倚靠座位位置。再者，於倚靠位置，軟墊凳65之坐墊67係作為一乘客用擱腳部分。 ί〇該背靠72包括一前表面73與一後表面74。於直立及後仰位置，背靠之前表面73係與座位底盤71配合，用以構成乘客用座位。於床舖形式中，如第2圖之左手邊的座位單兀所不，背靠係相對於座位單元向前地搖動，並且部分地谷納在立方體凹部44中，以致背靠72之後表面74大體上係 45 玖、發明說明與第一與第二表面47、48共平面，並且與軟墊凳65之坐墊 67共平面。在床舖形式中，背靠72之後表面74大體上同時係與第二表面48及坐墊67為連續的。座位移動機構包括一可移動充填元件76，如第ία圖中所示，當座位係由座位形式轉換至床舖形式時，其係由一儲藏位置移動至一展開位置。於床舖形式中，充填元件76係配置在中間位置，並且大體上係與背靠72之後表面74以及該第一表面47共平面並為連續的。於床舖形式中，座位單元4〇因此提供一乘客用延伸床舖表面，床舖表面藉由第一表面47而在座位後方延伸，藉由第二表面48由座位之橫向延伸，並藉由軟墊凳65 之坐墊67而在座位前方延伸。相關於苐1及1A圖，位於每一行29中的座位單元40係附裝至個別對的座位軌道32、34 ,以致每一座位單元4〇之抽象的座位縱軸c_c係與抽象的行縱軸b-b成一對銳角， 15 、並且座位單元40係於縱向彼此間偏移地並列配置，以致每一座位單元40在每一座位71、72之後方形成一大體上為三角形或疋梯形的空間36。該座位單元4〇係配置在行29中，以致座位單元40之隱私隔板60的凸面部分61，大體上係連續緊靠在另一相鄰座位單元4〇之第一凹面橫向邊緣上。〇如第1A圖中清楚可見，每一座位單元40之座位71、72之後方的空間36，因而係由一座位的第一表面47以及另一相鄰座位的第二表面48所佔用，該一與另一座位單元4〇之第一及第二表面47、48係分別地藉由一座位單元4〇之隱私隔板 60而互相隔開。因而使用位在每一座位71、後方的空間 46 593064 玖、發明說明 36，用以在床舖形式中將座位71、72向後延伸進入該空間 36中，而延伸由座位單元40所提供之床舖表面、7 4、7 6的長度。於一行29中的座位單元40所成之銳角，係視所需的客 5搶配置而相對於抽象的行軸B-B而定向。然而，典型地，每一座位單元40之抽象的座位軸c_c與行軸B_B所對之銳角係位在30度至60度的範圍中，而較佳係為4〇度至5〇度，如第1圖中所示，例如約為40度。座位單元4〇的方向係可相關於客艙20、21而面向内或向外。於第i圖之第一客艙 10 20中，能夠見到的是，每一外行29係配置與相對側壁26、 28之其中個別的一側壁相鄰，並且於每一行29中的座位單凡40係面向内。於每一行29中座位單元4〇的第二橫向邊緣 49大體上係共平面的，用以構成一伸長行外邊緣，其係延伸與客艙20之側壁26、28並列。由於在第一客艙2〇中側壁 15 26、28的曲度，所以在外行邊緣與每一侧壁26、28具有一 J間隙2 7 ’並且通常係使用由熟知此技藝之人士所熟知類型的適合充填嵌板填塞該間隙27。於第二客艙21中，每一外行29之座位單元40相對於客搶21同時係面向内並面向前。由第1圖中可見，當第二客 2〇艙21之側壁26、28與第一客艙20之側壁26、28相較大體上彎曲較小’座位單元4〇的第二邊緣49與在第一客艙2〇中的位置相較’係配置得更為接近側壁26、28，因而在座位單兀的外行邊緣與相對客艙側壁26、28之間不具或是大體上不具間隙。第二客艙21之二中央行29的座位單元40同時係 47 593064 玖、發明說明向則，但相關於客艘21其之方向係面向外。該二中央行 29係背靠背地配置，以致於一尹央行29中每一座位單元的第二線性單元49，大體上係與位在另一中央行29的另一座位單元40的一對應之第二線性邊緣料為連續的。然而， 5與第一客艙20之行29相較，第二客艙21之行29的座位單元 40，其係配置以致在每一座位71、72之後方，座位單元係形成一大體上三角形或是梯形的空間36，其係由一座位單凡4〇之第一表面47與另-相鄰座位單元4〇之第二表面48 所佔用。 1〇冑私隔板係配置在二中央行29之間，該隔板可包括一可移動部分構件，其係位在二中央行29中每一對之對應座位40的中間，該定位構件係可具選擇性地在一展開位置人儲藏及收回立置之間自㉟地移動，於展開位置中該定位構件有效地在成對之二座位4〇之間構成一隱私屏障，而 ;儲藏及收回位置中將該定位構件移除，以致使用二對應座位的乘客在床舖形式抑或是座位形式中，於其之間並未具有任何邊界。員杂現本务明之座位系統容許處在床舖形式下的每一座位單元4〇，提供一乘客用床舖表面，其之長度至少為80 寸（2’032 a尺）’於每—行29中介於相鄰座位單元扣之間的間距係為50至60忖⑽至⑸公尺）。於一些狀況下，能夠乂 w亥严曰1距提供在床舖形式下整體之床舖尺寸係超過Μ 吋（2.16公尺）。應察知的是，夫3又口田本杂明之一座位單元4〇的可移動乘客 48 593064 玖、發明說明支承元件71、72，如第2圖中所示，係配置成一用餐或是倚靠的座位形式，座位71、72之後方的空間36係由直立或是後仰的背靠72所隱藏。因此，當座位單元4〇係使用作為一座位時，空間3 6提供一有用的儲藏空間，特別地係能夠 5用以儲藏寢具材料，諸如枕頭、毯子、羽絨被以及相似物。邊荨寢具材料能夠儲藏位在座位71、7 2之後方的空間3 6 内’以致寢具材料係由座位71、72之後方的第一表面47所支撐。當一乘客希望睡覺時，可移動乘客支承元件7丨、72 、76係能夠具選擇性地移動至如第2圖中所示的床舖形式 1〇，因此將座位71、72之後方空間36暴露，容許易於拿取儲藏於其中的寢具。利用位在床舖形式的可移動座位元件71 、72、76，由座位單元40所提供之伸展的床舖表面係可由乘客或是空服員手動地舖放寢具材料，用以提供一乘客用元全地完成的床舖。 15 於座位形式中，使用座位單元的一第一乘客能夠坐在由座位底盤71以及背靠72所構成的座位上，以及希望見到第一乘客的一第二乘客能夠坐在由軟墊凳65所提供的輔助座位上。如第1A圖中所示，座位單元4〇之第二表面“承載一鉸 2〇接的臂靠75，其係鉸接至支撐結構42用於在如第^圖中所示的一儲藏位置與一展開位置（未顯示）之間，於第二表面 48的平面中搖動，於儲藏位置中臂靠乃大體上係平行於第二線性邊緣49而延伸，而於展開位置中臂靠乃在與由座位底盤71以及背靠7 2所構成的座位並列的立方體凹部* *之前 49 玖、發明說明與後端部之間，大體上係平行於抽象的座位軸C-C延伸， f此使用座位的—乘客可將他或她的其中之—手臂摘在臂 *75上°可㈣地’臂靠75可儲藏在構成於該平面48中的 -凹部（未顯示）内，並可提供構件用於在一儲藏位置與— 1位置之間垂直地平移臂靠’於儲藏位置_該臂靠係容 2在該凹部中’與該頂部表面48齊平，於展開位置中該臂靠自凹部突出用以提供-臂靠供座位使用者使用。此可交 j方式所具之優點在於，於儲藏位置，在由頂部表面Μ所提供之可用表面區域上不致碰撞臂靠。另一固定式臂靠（ 1〇未顯示）係可由隔板60所支承。口此本發明之座位系統包括複數之自備的座位單元 40，該每一單元提供乘客用個別的座位與睡眠舖位。於每仃29中，可見到的是，一座位單元4〇之第二側邊54的隔板60與另一相鄰座位單元4〇之隔板6〇係配置與一座位單元 15 4〇的第一側邊53並列，形成一部分封閉、私人空間，供使用該一座位單元40的乘客所用。本發明之每一座位單元4〇包括一座位外殼43以及一軟墊先65 ’该軟墊凳65係與座位外殼43之前方隔開。然而，如上所述本發明之座位單元4〇係可便利地藉由將一座位單 20兀40之座位外殼43與另一相鄰的座位單元4〇的軟墊凳65一體成型而製成。因此，形成一座位單元4〇之座位外殼43的支撐結構42係可與形成另一相鄰的座位單元4〇的軟墊凳65 的支撐結構42—體成型。因此，本發明之座位系統，如第 1A圖中所示，係可由複數之座位模組8〇所組成，每一模組 50 593064 玖、發明說明 8〇包括座位外殼43與一座位單元4〇之可移動座位元件71、 72、76，以及另一相鄰座位單元4〇之軟墊凳65。藉由將複數之該座位模組80附裝至位在一客艙2〇、21中的一對座位執道32、34，能夠組裝複數之座位單元4〇，每一座位單元 5 4〇包括一模組的座位外殼43與另一相鄰模組80的軟墊凳65 〇母座位模組8 0，如第1及1 a圖中所示，於三點位置處附裝至一對座位執道32、34。特別地，每一座位模組8〇係於二隔開點38處附裝至該對座位軌道32、34其中之一座 10位執道，並於一單一點39處附裝至該對座位執道32、34的另一座位執道。每一座位模組8〇，其係可直接地附裝至該對座位軌道32、34或，可交替地，每一模組8〇之支撐結構 42可包括一基座或護腋片（未顯示），該基座或護腋片係附裝至座位執道32、34。於任一狀況下，支撐結構42或是基 15座或護腋片係利用為熟知此技藝之人士所熟知的腳固定裝置附裝至座位執道32、34。使用三點式固定方式38、39用於將一座位模組80附裝至一對座位軌道32、34，已發現係為有利的，超越一傳統式四點固定方式。特別地，頃發現二點式固定方式容許在一對座位軌道32、34之該二座位軌 2〇道之間有較大的撓曲度，因而容許在緊急降落狀況下該二座位執道彼此相對地移動或撓曲，或是墜落時降低座位模組80自座位執道32、34脫離的風險降低。每一座位單元40之形式，以及根據本發明在一客艙中對於座位單兀40之配置，係容許每一座位單元4〇之使用者 51 玖、發明說明易於從走道進入座位單元40,反之亦然。於第3至5圖中所示係為本發明之一第一乘客座位總成弟宋客座位總成能夠適用於構成一上述相關於第1 、、2及2A圖說明的座位系統之座位單元4〇。然而，熟 5知此技藝之人士應察知的是，本發明之座位系統並未限定弟至5圖之座位總成。上述之座位系統大體上能夠包括任座位單凡40，其係界定一抽象的座位縱軸c_c，並包括一支撐結構42用於支撐離開一載具之地板3〇的座位單元成型構件71、72或是可裝配用於形成一座位，其係包 1〇括一座位底盤71以及一背靠72與構件48、67、74、76，形成或是裝配用於形成一大體上平坦的床舖，該床舖的主要部分係配置在座位的前方位置，床舖係在座位後方向後延伸用於伸展為平坦的床舖。於第3至5圖中，第一乘客座位總成與第丨、1A、2及 15 2A圖之座位單兀4〇相一致之元件，係以相同之代表符號於之刖加數字” Γ’加以標示。本發明之第一乘客座位總成14〇具有一前端部151、一後端部152以及二相對側邊153、154。座位總成14〇包括一支#、、Ό構142，用於固定地將座位總成丨4〇牢固至嵌進在一 20載具之地板130中的座位軌道，並用於支樓離開則反的座位總成140。為熟知此技藝之人士所熟知之類型的任一適合的腳固定裝置，係可用以將支撐結構142牢固至一對座位執道。儘管第3至5圖之第一乘客座位總成14〇係特別地適用在飛機客機上，但其同時能夠適用在其他形式的乘 52 593064 玖、發明說明客載具，例如，諸如火車、長途公車以及水上載具（water-borne craft)，包括客船以及渡輪與氣墊船。該支撐結構142包括一座位外殼143，其大體上係配置朝向總成140之後端部152，以及一軟墊凳165其大體上係 5 配置朝向總成140之前端部151。該座位外殼143係形成一大體上直線的或是立方體凹部144，其係於其之上端部2〇1 及前端部202處敞開，並在其之後端部203處藉由一大體上垂直延伸的後壁204，以及在每一側邊藉由二隔開的相對、大體上垂直延伸的側壁205、206加以閉合。於第3至5圖 10中，僅見到其中之一側壁205。對於凹部144之後方，座位外殼143形成一大體上平坦的第一上表面147，以及凹部 144之一中間側邊和總成之一側邊153，外殼143進一步地形成一大體上平坦的第二上表面，其大體上係為與第一表面147共平面的，並且大體上同時係為連續的。該第一與 15第二上表面147、I48係足夠堅固用以支撐使用座位總成 140之乘客的部分重量。該軟墊凳165係與座位外殼143之前方隔開，並具有一大體上平坦的上表面166其係承載一座墊167，該座墊的一平坦上表面169大體上係與座位外殼143之第一與第二上表 20面147、I48共平面。該軟墊凳單元165同時係足夠堅固，用以支撐乘客的重量並能夠使用作為一辅助座位。凹部144之該每一侧壁205、2〇6承載一旋轉軸承以〕。該旋轉轴承222係互相對正，用以形成一橫軸其係橫向延伸穿過該凹部m大體上平行於地板表面13〇,但稍有傾斜 53 593064 玖、發明說明，如以下所詳述。該旋轉軸承222係配置高於地板表面130 ’其之高度大約在地板表面130與第一和第二上表面147、 148之間的中間位置。該旋轉軸承222同時係大體上在凹部 144中向後配置，朝向後壁204。該每一旋轉軸承222接受 5 如第6至8圖中所示之一座位移動機構220的一個別的、橫向延伸的耳軸221，其中為了清楚起見，將支撐結構丨42省略。每一耳軸221大體上係於中心附裝至一個別的、大體上為雙凸透鏡狀的搖動板223的一大體上平坦、面向外表 10面226上。每一搖動板223具有一大體上為線性的第一邊緣 224，以及一相對的拱形第二邊緣225。第9至丨丨圖係為搖動板223的詳細圖式。每一搖動板具有一上端部228與一下端部229，並且二搖動板223係藉由一大體上為圓筒狀、橫向延伸的具有二相對端部231、232之第一扭力管23〇扣接 15在一起。扭力管230之每一端部231、232係與和下端部229 並列的一個別搖動板223之一内表面227連接。第一扭力管 230因而用於聯合該二搖動板223，其係形成一凹部235位在其之個別相對内表面227的中間。該聯合的搖動板223因而能夠相關於與旋轉軸承222連接的耳軸221，而相對於座 20 位外殼143搖動。母搖動板223之棋形邊緣225係朝向其之下端部229 經由一適合的銷接合（pin j〇int)而樞接至一連桿Μ1的一端部242。連桿241的另一端部243係樞接一搖臂％的一端部 2 4 士第14及15圖中所示，搖臂245的另一端部2私係固 54 593064 玖、發明說明定牛固地與一第一可轉動扭力管25〇之個別的端部251、 252並列。於一端部251處，第二扭力管25〇係轉動地支撐在中空蝸輪外殼260中。於另一端部252處，第二扭力管 250係轉動地安裝在由凹部144之第二側壁2〇6所支撐的一 5 軸承2 5 3中。該蝸輪外殼260具有一大體上平坦的底部表面％〗，並形成一大體上為圓筒狀的内腔室262，其係容納第二扭力管250之一端部251所用之軸承253。該第二扭力管25〇之一端部251係同軸固定地牢固至容納在該腔室262内的一蝸輪 1〇 271。外殼260具有一上壁263其係如代表符號264所示係部分地切除用以露出蜗輪271之輪齒。該外殼26〇於該凹部 H4之後方處，與後壁2〇4並列，位在第二上表面148下方，係固定地牢固至位在第一側壁2〇5中的一凹部（未顯示）内的第一座位總成140之支撐結構142。 15 該外殼260之上壁263係構成有一大體上向上延伸的凸耳265，以及一大體上為圓筒狀的螞桿外殼273係鉸接至該凸耳265，用於如第14圖中所示的一嚙合位置，與第15圖中所示的一脫離位置之間移動。該蜗桿外殼273係按適當形狀製作，以致在嚙合位置中，外殼273係與蝸輪外殼26〇 20之上壁263嚙合。如第15圖中所示，蝸桿外殼273係如代表符號274所示般切除，用以容許蝸輪271之輪齒延伸進入蝸才干外设273之内部。如弟16圖中所示，蜗桿外殼273容納一媧桿270，其係可轉動地安裝在二相對推力軸承272之間。該蝸桿270係可轉動地經由一同軸的心軸275，與具有一馬 55 593064 玖、發明說明達外殼281的電氣馬達280結合，其係固定地牢固至蝸桿外殼273。如第16圖中所示，馬達外殼281係經由二連桿282 、283與蝸輪外殼260連接，構成一”中斷鏈結（break-link)” 裝置。該其中一連桿282係在一端部284處樞接至馬達外殼 5 281，並於另一端部285處與另一連桿283之第一端部樞接。該另一連桿283之一第二端部286係樞接至蝸輪外殼260 。該一連桿282大體上係大於另一連桿283，並且於嚙合位置中，三樞轉點284、285、286係為共平面的，以致介於另一連桿283之第二端部與蝸輪外殼260之間的樞轉點，係 10 配置在介於二連桿282、285之間的一連桿282之樞轉點284 至馬達外殼281與樞轉點285的中間位置，以致可防止蜗桿外殼273不致與蝸輪外殼260脫離。該一連桿282如第16圖中所示係可具選擇性地順時針轉動，致使另一連桿283同時順時針轉動，”破壞”三樞轉點284、285、286之對正。 15 蝸桿273因而能夠自蝸輪脫離，容許搖臂245相關於由該第二扭力管250所形成之軸自由地轉動，連桿282、283係用以限制蝸桿外殼273能夠自蝸輪外殼260脫離的程度。可交替地，取代中斷鏈結（break-link)裝置，蝸桿外殼273能夠藉由，例如一可移開螺栓，可鬆開地牢固至蝸輪外殼260 20 〇如第9圖中所示，每一搖動板223之内表面227係建構有一伸長、大體上為線性的凹部301，其之橫截面大體上為線性的，並大體上平行於該第一邊緣從與搖動板223之下端部229並列的一下端部302，延伸至位在搖動板223之 56 593064 玖、發明說明 4上與下端部228、229的一中間點處的一上端部303。如第3至5圖中所示，該伸長的凹部301容納一線性螺桿3〇4，如第〗3圖中所示其具有上及下端部305、306。於一些具體只施例中’滾珠螺桿或是任何其他適合的、不可逆線性致 5動器裝置係可用以取代該二線性螺桿。於其之上端部305 處，每一線性螺桿304係可轉動地安裝在一軸承3〇7中，其係於凹部301之上端部303處固定地牢固至搖動板223。每一線性螺桿304之下端部3〇6係容納在一齒輪外殼31〇中，其係固定地牢固至個別搖動板223之内表面227。（於第13 10圖中，省略其中之一齒輪外殼3 10，用以顯露出位在線性螺才干304之下端部3〇6處的細節）。該下端部3〇6係由一位在齒輪外殼310中的一轉動軸承3〇8所支撐，並係可轉動地經由一斜齒輪3 11與一轉動的傳動軸312之一個別的端部313 3 14結合。於一端部3 14處，傳動軸3 12係經由一對互相 15嚙合的小齒輪315、316與一步進馬達3 18連接，其係安裝至齒輪外殼310以致馬達318之作動致使軸312作動，並因而轉動線性螺桿304。每一線性螺桿304承載一螺帽32〇，其係包括一按適當形狀製作的主體321。該主體321大體上其之橫截面係為τ 2〇形狀，並包括一大體上直線的滑件部分322，其係按適當形狀製作，用以在構成於個別搖動板223之内表面227中的線性凹部301内’構成一緊密但是自由滑動的配合。該滑件部分322將線性螺桿3〇4容納於其中，並包含内部構造（未顯示），用於與螺桿3〇4嚙合。該主體321進一步地包括 57 593064 玖、發明說明一對相對的翼部分324，該每一部分具有一大體上平坦的外表面325，二翼部分324之外表面325相互之間大體上係為共平面的。主體321具有一大體上平坦的内表面326。將 /月件部分322肷入在個別的搖動板223之線性凹部301中， 5翼部分324之外表面325係緊密地與搖動板223之内表面227 相鄰。相關於第6圖，該每一螺帽320係經由一水平自由接頭 329與構成部分之座位底盤元件171的一結構膜片330的一個別橫向側邊緣331、332連接，其係配置在凹部235中， 10位在二相對搖動板223中間。該膜片330可包括一重量輕、模塑合成敢板或一多孔銘質薄片。該座位底盤元件171具有一後端部333以及一前端部334，該水平自由接頭329係配裝至膜片330朝向該後端部333，用以容許座位底盤元件 171的前端部334相對於後端部333向上或向下地傾斜，相 15對於搖動板223係較少移動。該座位底盤元件171包括適合的坐墊與墊襯物，其係由膜片330所支撐，用以提供使用座位總成140的乘客一舒適的座位表面。（為了清楚起見，在第6至8圖中將坐墊與墊襯物省略）。與前端部334並列的膜片330，其係樞接至一懸垂桿 342之一上端部341連接。桿342之另一端部係樞接至一滑件345連接，該滑件係可滑動地固持在一伸長的、大體上為線性的滑道350中，其係固定地牢固至位在該凹部144 内座位外殼143之該側壁205、206的其中個別之一側壁。如第3圖中清楚可見，每一滑道35〇其之方向係相對於地板 58 5193064 玖、發明說明表面130成一角度，以致滑道350在一上端部351與一下端部352之間’於凹部144中向前及向上地延伸。該桿342之另一端部343同時係樞接至一拖曳支柱355之一下端部354 連接，該拖曳支柱355的一上端部356係樞樞接至與搖動板 5 223之下端部229並列的個別搖動板223之第一線性邊緣224 〇相關於第9圖，每一搖動板223之内表面227係同時構成一伸長的梹形軌道360，其係在一與板223之上端部228 並列的上端部361與一和板223之下端部229並列的下端部 10 362之間，和第二拱形邊緣225並列地延伸。於線性凹部 301與拱形執道360的中間位置，每一搖動板223之内表面 227係同時構成一短的線性狹縫365，其係從與執道36〇之上端部361並列的一上端部366，延伸至和線性凹部3〇1之上端部303並列的一下端部367。如第3圖中清楚可見，線 15性狹縫365係相關於板223之線性邊緣224成一角度，以致當狹縫向下地由上端部366延伸至下端部367時，其係從線性邊緣224朝向拱形執道360向板内延伸。同時可以見到的是，拱形軌道360與線性狹縫365係從其之個別的上端部 361、366朝向其之個別的下端部362、367互相叉開。 20 位在每一搖動板223上的拱形軌道360接受可滑動的二隔開摩擦塊件371，如第6AA6B圖中所示，其係固定地牢固至一下背罪几件374之一個別的下側構件373的外表面 372。该下背靠兀件374，連同_於以下詳述的一上背靠元件構成-背Λ το件172。每-下側構件373大體上係為匕形 59 593064 玖、發明說明 ίο ^’具有~上端部375與-下端部376以及-大體上為線性々後邊緣377。於該下端部376處，每一下側構件373包括 ’、有向刖大出之鼻部分379的一擴大的腳部分378。每一下側構件373具有—大體上為線性的前邊緣381，其係相對於後邊緣377成—些微角度，在該上端部375與該擴大的腳部分378之間延伸。如第6A及6B圖中所示，位在每一下側的/、中之一摩擦塊件371係於側構件373之下端部376處安農至該外表面372，與後邊緣377約成45度的角度。該另-摩檫塊件371係在該上與下端部375、376中間勺”占處女裝至與該後邊緣377並列的該外表面372上。 4另一摩擦塊件371同時係與後邊緣377成一對角，但該角度係小於由一摩擦塊件371與後邊緣377所成之對角。 15 於該二下侧構件373的中間位置，下背靠元件374包括一大體上平坦的膜片385，其係與該前與後邊緣”？、381 一者之内。卩隔開，用以分別地構成後方與前方下凹部％6 及387。同樣地，座位膜片385可包括於飛機座位製造業界所廣為熟知類型的一模塑合成嵌板或是一多孔金屬薄片。每一側構件373之外表面372進一步地構成有一大體上為直線形狀的腔室39〇，其具有一周圍側壁391。該腔室 390係以一蓋板38〇所覆蓋（為了清楚起見，係於第6八及6]3 圖中省略），其係固定地牢固至側構件373之外表面372。該腔室390容納一大體上為三角形的搖桿392，其係具有一上翼件393以及一下翼件395。搖桿392大體上係於其之鈍角頂點396處中央地樞接至側構件373。於下翼件395的盡 60 20 玖、發明說明頭係配置一朝向外的插銷397，並且於上翼件393的盡頭係配置一凸耳398。搖桿392因而能夠利用上及下翼件393、 395之對應的搖動’而相關於樞軸396搖動。搖桿392之移動係由腔室390之側壁391所限制，以致上翼件393能夠在 5如第6A及6B圖中所示的一位置，其中凸耳398係完全地向刖配置，與另一位置（未顯示），其中上臂393係完全地向後配置，之間搖動。位在下翼件395上的插銷397係可滑動地收納在，構成在個別搖動板223之内表面227中。如第3圖中清楚可見，〇下月罪元件374係由座位底盤元件171之後端部333向上延伸，並在其之上端部375處樞接至該上背靠元件394。該上月罪元件394包括二隔開的上側構件4〇2，以及一大體上為平坦的上膜片403，其係在該等上側構件4〇2之間延伸。該每一上側構件402具有一大體上為線性的後邊緣4〇4，以及 15 一大體上為線性的前邊緣405，並且該上膜片403係與該二後與前邊緣404、405向内地隔開，用以分別地形成前與後上凹部406、407。容納坐墊的下與上前凹部387、4〇7係經特別地設計，用以構成一舒適的背靠表面，其係與座位底盤兀件171上的坐墊結合，構成一乘客專用的座位表面。 2〇背罪所安裝的靠墊係與座位底盤元件171上的坐墊相配。為了清楚起見，在第6、6八、犯、7及8圖中省略了上與下月罪兀件之坐墊及墊襯物。上與下後凹部386、4〇6形成一大體上為連續的凹部，其係接受一大體上平坦的適用於形成一床舖表面的坐墊或床墊。再者，為了清楚起見，在第 61 玖、發明說明 6 6A、6B、7及8圖中將此部分省略。然而，特別地，配置在上與下前凹部387、4〇7中的背靠塾，係可具有與後座墊或床墊不同的風格或是坐墊色彩。再者，分別配置在背靠元件的前與後表面上的靠墊，係可針對座位及寢具的目 5 的而具有不同之適當的彈性程度。該每一上側構件402具有一上端部4〇9以及一下端部 411。每一上側構件402係在該上與下端部409、411中間的代表符號410處，樞接至個別的下側構件373之上端部，以致每一上側構件4〇2係自樞轉點41〇向下延伸，用以構 1〇成一腳部分412，該部分在其該下端部411處具有一大體上為U形狀的切除部分414。該ub狀的切除部分414滑動地容納構成在個別搖桿392之上翼件393上的凸耳398，用於將該臂392之搖動傳送至上側構件4〇2。因此，搖桿392相關於其之中心樞轉點396的搖動，致使在上與下背靠元件 15之間，上背靠元件394相關於樞轉點410對應地搖動。相關於第3圖’每一下側構件373之鼻部分379係經由無效運動裝置420而連接至位在螺帽320上的其中之一翼 4分325 ’該螺帽係安裝在個別搖動板223之線性螺桿3〇4 上。母一無效運動裝置420包括一插銷，其係於代表符號 2〇 328處附裝至個別的翼部分325，該插銷係收納在構成於下側構件373之鼻部分379中的一短狹縫中。相關於第9至12圖，每一搖動板223之拱形邊緣225面對上端部228構成有一突出的凸耳431，其係樞接至一臂構件432的一端部433，該臂構件432的末端係位在遠離凸耳 62 593064 玖、發明說明 431的另一端部434中。二臂構件432承載一橫向充填膜片構件440，該構件承載一大體上為直線的具有一上表面443 的填實坐墊442。與凸耳43 1並列之每一搖動板223的外表面226，係承 5載一小的折線構件（dog-leg member)450，其係在搖動板 223的凸耳431與下端部229之間於代表符號451處樞接至搖動板223。該折線構件45〇具有一第一翼件452，於翼件末端配置有一鉤453，以及一第二翼件454係配置一凸輪從動件455。每一臂構件432具有一向外延伸的支撐插銷456， 10並且母一搖動板223的外表面226係構成有一向外延伸的停止插銷457，其係位在板223之樞轉點451與拱形邊緣225之間。折線構件450係可相關於樞轉點45丨自由地轉動，並且如第9至12圖中所示停止插銷457係用以限制板223之折線構件450的順時針轉動。（位在另一搖動板223上的停止插 15銷係限制對應之折線構件450的逆時針轉動）。位在折線構件450之第二翼件454上的凸輪從動件455 ’係與構成在凹部144之個別側壁205、206上的一凸輪 460(見第8至12圖）嚙合，用於控制折線構件45〇的移動。如第3圖中所示，如之前所說明的第一座位總成14〇係 20可配置為一直立的座位形式，其中搖臂245相對於位在凹部144内的轉動軸50而向前延伸，並且連桿241大體上係與搖臂245共平面，以致聯合的搖動板223係定向在如第3、4 、6、7及10圖中所示的座位形式，其中每一搖動板223之線性邊緣224係在凹部144内向上及向後延伸，位在二搖動 63 593064 玫、發明說明板223上的拱形軌道36〇大體上係在凹部144内向下及向前延伸。當連桿241與搖臂的對角為18〇度，用以在座位位置構成一壓縮支柱時，施加至搖動板223上的任何負載係直線地施加至第二扭力管25〇，並無轉動力施加至蝸輪。 5有利地，座位總成之座位轉換子機構係能夠禁得起大的向前力量，而在座位移動機構與支撐結構之間不需任何附加的T脫離機械聯接器，諸如一射栓（shootjoit)。於直立的座位形式中，如第13圖中所示，螺帽320係配置在其之個別線性螺桿304的上端部305處，並且桿342之下端部343係 10配置在滑道350的上端部處，以致座位底盤元件171大體上係水平地配置在凹部144内，座位底盤坐墊的上表面大約係與位在座位外殼142上的第一及第二上表面147、148，以及位在軟墊凳165上坐墊167之上表面169位在相同的高度。位在下背靠元件374之下側構件373上的摩擦塊件371 15 ，係配置在位於搖動板223上拱形軌道360的上端部361處，以及位在搖桿392上的插銷397係配置在位於搖動板223 上線性狹縫365的上端部3 66處。因此，搖桿392之上翼件 393係完全向前地配置在其之個別的腔室39〇中，以致上背靠元件394大體上係與下背元件373共線的（C0-nnear)。於第3圖之直立位置中，位於搖動板223上的折線構件 450係自個別的凸輪構件46〇脫離，並且如第1〇圖中所示，於儲藏位置中，臂構件432係配置使充填坐墊442大體上係配置在座位外殼143之第一上表面147的下方。於直立位置中’位在上及下背靠元件394、373上的坐墊408，構成一 64 593064 玖、發明說明人類工程學之舒適在座位底盤元件171上具有坐墊的符合的座位。於直立位置中，由座位底盤元件171與背靠元件⑺所形成之座位，大體上係適用於進餐。軟塾覺單元165係鱼 5座位底盤元件171之前方隔開，並係可使用作為乘客用搁腳部分。由第3圖之直立位置，如下座位總成係可後仰至如第4 圖中所示的-完全後仰的位置。步進馬達318 一經作動，致使位在搖動板223上的線性螺桿304轉動。當限制螺帽 10 320與線性螺桿304 一起轉動時，螺帽係沿著線性螺桿綱平移地傳動，朝向構成在搖動板223之相對内表面Μ?中之凹部301的下端部302。當螺帽32〇係向下傳動時，座位底盤元件171之後端部333同時係相對於由桿342所支撐的前端部334向下傳動。座位底盤元件171之後端部333因而向 15下傳動，致使座位底盤元件在桿342之上端部341與座位底盤膜片330之間相關於樞軸向後傾斜。當線性螺桿3〇4在凹部144中向下及向前延伸時，座位底盤元件171係同時向前傳動，該向前的移動係藉由桿342相關於樞軸在個別滑道 350中桿342之下端部343與滑件345之間的向前搖動而容納。 0 座位底盤元件171之前端部334因而在凹部144中稍微向下地移動，但未達到如座位底盤元件171之後端部333的相同移動程度。藉由位在滑件345與搖動板223之間的拖曳支柱355 ’防止滑件345沿著滑道35〇向後移動。螺帽320之向前及向下移動同時致使背靠元件172對應 65 593064 玖、發明說明地移動，其係經由位在下背靠元件373之鼻部分379上的無效運動裝置420與螺帽320連接。背靠元件1?2之移動致使摩擦塊件371在位於搖動板223之相對内表面227上的其之個別的拱形軌道360中，從執道360之上端部361朝向下端 5部362滑動。如上所述，摩擦塊件371的相對方向與執道 360之彎曲造成，當摩擦塊件371沿著軌道36〇滑動時，下背靠元件373受引致如第4圖中所示由第3圖之直立位置，向後搖動至如第4圖中所示之完全後仰的位置。同時地，位在搖桿392上的插銷397係受引致，沿著位 10在搖動板223上的線性狹縫365滑動。當每一線性狹縫365 係自位在相同搖動板223上對應的拱形軌道360又開時，每一搖桿392之上翼件係受引動，在個別的腔室39〇中向後搖動。搖桿392之上翼件393的向後移動，致使上背靠元件 394之上側構件402相對於下背靠元件373而向前地搖動。 15當背靠元件m係藉由螺帽320之移動而向前及向下傳動時，上背靠元件394相對於下背靠元件373漸進地進而向前搖動，直至搖桿392與個別腔室390之側壁391嚙合為止，防止上者罪元件394的進一步向前搖動。構成在二搖動板223 上的凹部301、執道360及狹縫365的相對位置與外形係經 20仔細計算，用以確保當座位自第3圖之直立位置朝向第4圖之完全後仰位置後仰時，座位底盤元件ηι及上與下背靠元件3 94、374係移動經由複數之預定、符合人類工程學的舒適位置。控制步進馬達3 18以致螺帽320能夠停在線性螺桿3〇4 66 玖、發明說明之上與下端部305、306之間的任一中間位置處。因此，由座位底盤元件171及上與下背靠元件394、374所形成座位的移動，可在第3圖之直立位置與第4圖之完全後仰位置之間的任一中間位置處停止。於一後仰位置中由上與下背靠 5兀件394、374所造成之對角，致使下背靠元件374有利地提供使用座位總成140之乘客腰椎支撐。線性螺桿304係為不可逆的線性致動器裝置，因此本發明之座位總成具有之附加優點在於，施加在座位底盤元件171或是背靠元件172的力量無法經由螺帽320及線性螺 10桿304而傳送至馬達318。如此所具有的優點在於，施加至可移動座位元件171、374、394之突然的及/或強勁的力量，並未由步進馬達所，，承受”，因而降低了對步進馬達3 i 8 造成損害的風險。如之前所說明之第一座位總成14〇的一特別的性能在 15於，其能夠由第3圖之直立位置轉換成如第5圖中所示的一床舖形式。為了將座位總成140由直立形式轉換成床舖形式，馬達280作動致使蜗桿270轉動。將位在蜗輪外殼26〇上的蜗桿外殼273置於嚙合位置，蝸桿270之轉動致使蝸輪 271對應地轉動，並因而致使第二扭力管25〇轉動。扭力管 20 250之轉動依序致使搖臂245由如第15圖中所示的一座位位置，轉動至如第14圖中所示的一床舖位置。相關於第3及5圖，搖臂245向後地轉動致使連桿241相關於耳軸221向前地搖動該搖動板223。在凹部144内向前地搖動該搖動板223，致使下背靠元件374相關於耳軸221 67 593064 玖、發明說明向前地搖動。介於座位底盤元件171與螺帽320之間的水平自由接頭329，同時係相關於耳軸222轉動，並且搖動板 223之搖動致使拖曳支柱355沿著滑道350在桿342之下端部 343處向後及向下地拉動滑件354，從滑道之上端部351朝 5向下端部352。於凹部144内，座位底盤元件171之前與後端部334、333因而受引動下降，以致如第5圖中所示，背靠元件172向前搖動覆蓋座位底盤元件17ι。於第5圖之床舖形式中，座位底盤元件17丨係配置在位於凹部144中的一下儲藏位置，並且於背靠元件172之下與 10上後凹部386、406中的坐墊或床墊大體上係配置與座位外殼143之上表面147、148，以及位在軟墊凳單元165上的坐墊167共平面。同時由第5圖中可見，上及下背靠元件394 、374係按適當尺寸製作，以致在床舖形式中，上側構件 4〇2之上端部4〇9係與軟墊凳單元165接觸，以致位在背靠 15元件m之後表面上的坐墊或床墊，在軟墊凳單元165上以丄墊167構成一大體上為連續的表面，並在座位外殼143上構成一第二上表面148。有利地，上背靠元件394之上端部 4〇9，係與位在軟墊凳單元165上的一結構（未顯示）嚙合， 2以致在床舖形式中，部分之所施加至背靠元件172的負載 2〇，係部分地由軟墊凳單元所支承。搖桿392與位在下背靠凡件374之下側構件373上，其之個別的腔室之侧壁391嚙合，用以將上及下背靠元件394、374固定在一起，防止於床舖形式中，在承受負載下，背靠元件172發生屈曲。搖動板223由座位位置移動至床舖位置，同時係升高 68 593064 玖、發明說明在凹部144内承載充填坐墊443的臂構件432。於如第⑺圖中所示座位位置中，折線構件45〇係自構成在凹部144之側表面205、206上的凸輪460脫離，並能夠相關於樞轉點451 自由地枢轉。然而，如以上所述’折線構件45〇的移動係 5 由停止插銷457所限制。當搖動板223係向前搖動朝向第5圖之床舖形式時，位在臂432上的支撐插銷456係變成封閉在位於折線構件45〇之第一翼件452上之鉤453後方。當搖動板223係朝向床舖形式移動時，凸輪從動件455係與凸輪460嚙合，因而將折 10線構件450固定在適當位置，將支撐插銷456封閉在鉤453 後方。如第5圖中清楚可見，臂構件432、坐墊構件料2、支樓插銷456、折線構件450以及凸輪460係按適當形狀製作並定位以致，在床舖形式中，充填坐墊構件442之上表面 15 443係充填介於下背靠元件374之下端部376，與座位外殼 143之第一上表面147之前端部之間的一空間。充填坐墊構件442之上表面443大體上係配置與位在背靠元件172之背部上的坐墊或床墊，以及第一上表面147係為連續並為共平面’用以構成一伸展的、大體上為平坦的床舖表面。 20 裝配座位總成140之支撐結構142以致，在飛行過程中 ’地板表面130係與水平約成1·3度的角度，本發明之座位總成所提供之床舖表面相對於地面大體上係為水平的。換 5之’本發明之座位總成14 0抵鎖在飛行過程中飛機之猶微傾斜。 69 593064 玖、發明說明有利地，蝸輪、蝸桿總成271、270係為非可逆的，並因而於床舖及座位形式中，馬達28〇不致，，遭受”施加在搖動板223的過度力量。換言之，施加在搖動板的過度或是突然的力量，並未經由螞輪/蜗桿總成傳送至馬達280。 5 如之前所說明，第一乘客座位總成140係配備使用者可操作的控制器，其係方便地安裝至支撐結構142。該控制器包括用於操作步進馬達318的裝置，用於在第3圖之直立位置與第4圖之完全後仰位置之間，具選擇性地移動座位底盤與可移動背靠移動元件171、374、394，並且用於 10作動馬達280,纟第3圖之直立形式與第5圖之床舖形式之間，轉換可移動元件171、374、394，其中可移動背靠元件374、394係與支撐結構142之固定式輔助元件，亦即軟墊凳單元165，以及座位外殼143之第一與第二上表面147 、148配合，用以構成一伸展的、大體上為平坦的乘客用 15床舖。該控制器包括控制電路，用於確保當座位係處在後仰或是完全後仰位置時，假若乘客試圖將座位總成14〇由座位形式轉換成床舖形式，則步進馬達3丨8首先作動，用以在馬達280作動將座位轉換成床舖形式之前，將可移動月Λ元件171、374、394返回至完全直立位置。如果馬達 2〇 280或是飛機客艙電力故障，則藉由中斷如上所述之中斷鏈結裝置282、283，並手動向前地搖動搖臂245至第15圖之座位位置。如之刖所說明，本發明第一乘客座位總成丨4()，因而提供自備、個別的乘客用座位與睡眠舖位。 70 593064 玖、發明說明第17圖係顯不本發明之另一座位系統，其係包括複數之於之前相關於第3至16圖所說明之類型的第一乘客座位總成140。於第17圖中，在機身51〇之鼻部分515的一後方位置處，一飛機機身51〇係包圍出一客艙52〇。如第！圖之座位系、，4的狀況下，第17圖之客搶52()係由機身別之二相對的内部表面部分526、528、位在機身51〇内支撐在適當的支撐基礎結構（未顯示）上的一地板表面或甲板530、以及 ί匕板（同時並未顯示）所形成。該基礎結構包括複數對的座位執道532、534，其係嵌置在地板表面53〇中。第17 10圖之客搶520包括二外對之座位執道532，每一軌道係與機身510之相對表面部分似、似的其中一個別表面部分並列地延伸，以及一單一的中央對座位執道Μ#。每一對座位執道532、534 ’大體上係平行於由機S 51G所形成並係如第17圖中由鏈點線Α-Α所示之-飛機縱軸而延伸。 15 座位總成140係附裝至座位軌道532、534，用以構成複數行529。每—行529係固定地牢固至成對座位軌道532 的-中之個別一執道，並形成一由第i 7圖中線所不之抽象的縱行軸。每一座位總成14〇，係如第η中線所示，形成一抽象的縱座位軸，其與抽象的縱行軸b_b約成49度之對角。在客艙52()内，附裝至外對座位執道爪的座位〜、成140 ’係面向前並向内。附裝至中央對座位執道 534的座位總成14〇，係構成二群組兄了、。附裝至中央對座位軌道534的座位總成削之―前群組w係面向前，並向著客搶520之-側，同時一後群組538係面向前並向著 71 593064 玖、發明說明客艙520之另一側。如第1圖中所示，於每一行529中，第17圖之座位總成係縱向地互相偏移而並列地配置，俾便在當座位總成14〇係處在座位形式時，位於背靠元件172後方，在每一座位 5總成I40之後方形成一大體上為三角形或梯形的空間530。如上所述，每一座位總成140係為自備的，能夠提供一乘客用個別、伸展的平坦床舖，其之長度至少為8〇吋（2〇2公尺）並且根據第17圖之座位系統的座位總成1的配置，容許座位總成140以約為50至60吋（127-1·52公尺）的間距容納 10在客艙520内。因此，複數之本發明的座位總成14〇，每一總成提供一至少長度為80吋（2·〇32公尺）的個別床舖，能夠容納在一典型的乘客用商務艙内。一飛機機身51〇之内部表面於垂直橫截面係為凹入的，因此於第17圖之客艙52〇内，機身51〇之每一相對的内部丨5表面部分526、528,在客艙52〇的每—侧邊處形成一橫向凹部。有利地，此橫向凹部係由附裝至其中之一對外座位軌道532的每-座位總成刚之第—與第二乘客支撑輔助表面147、148所佔用。在床舖形式中，第一與第二支撐表面 147、148構成部分之由每_座位總成刚所提供之伸展的 Μ平坦床舖表面，同時在一直立或是後仰座位形式中，橫向 :部：具有足夠的淨空高度(head r_)，用以容納座位的 π整南度’其係用以容納部分之伸展的床舖表面，對於淨空而度需求較低係表示有效地使用客搶内可利用之空間。根據本發明，係可選定用於褒飾座位底盤元件工171的 72 593064 玖、發明說明墊襯物，以及配置在每一座位總成i4〇之背靠元件37斗、 394上的坐墊4G8，以致當所有或是大部分之第丨頂的座位系統的座位總成140係配置為一座位形式時，客艙具有一第一特別外觀及/或氣氛係適於用餐及/或休息。提供用於 5裝飾配置在位於背靠元件172上的下及上後凹部退、傷中的上塾的叙具材料，係可具有特別適於一睡眠環境的圖案及/或色彩設計。特別地，可選定寢具材料的式樣，以致當所有或是大部分之第17圖之座位系統的座位總成14〇係處在床舖形式時，客艙52〇可具有一不同的第二外觀或 10氣氛，與第一外觀相較更具有，，給人充分休息的,，感覺，並係更適於一睡眠環境。相關於伴隨圖式中之第18及19圖，本發明之另一具體實施例的-乘客容納單元，其係包括由二半殼610a610b 所裝配而成的一殼總成610。容納單元係用以配置在一飛 15機客搶中與至少-相鄰座位61〇，並列，並且二半殼缝、 610b係彼此相似’以致每—半殼構成二相鄰座位的一部分。每一半殼61〇a、610b係由一適合的飛機用等級、重量輕的結構材料製成為一單件。每谷、、、内單凡之设61〇包括一曲線的、直立後隔板… 20 ，以及一相對的、直立、曲線前隔板614，藉由一大體上為線性的側壁616互連，用以構成-封閉的乘客空間二該殼610包括—底部邊緣611，其係形成_平面並配置有複數之適合的固定裝置（未顯示），用於將容納單元附裝至飛機客餘中的座位軌道上。於一些具體實施例中，該單 73 593064 玖、發明說明元係使用三該等固定裝置充分地牢固至座位軌道上。該殼610配置一座位620用的適合支撐結構，其係包括一座位底盤622、一背靠624以及一背靠延伸部分626(見第 20A-20C圖）。特別地，容納單元之殼61〇包括一下座位底 5盤628(見第19圖），其係配置與後隔板612相鄰，並具有一大體上為平坦、水平的上表面，用以支撐座位底盤622。遠座位底盤622係在其之前邊緣623處樞接至下座位底盤 628，以及背靠，其通常係維持在一大體上係直立的位置，靠著後隔板612之内部表面，係於其之下端部625處樞接 1〇至座位底盤的後端部。該背靠延伸部分626在如上所述的通常位置下，係在背靠624之上邊緣的上方並且大體上係為連續的一位置處，永久地固定至後隔板612之内部表面。垓封閉的乘客空間618進一步地包括一托架64〇，其係支撐在殼610上的客艙地板上方與前隔板614鄰接。可任擇 15地，該托架640係可調整高度，其係為熟知此技藝之人士所熟知的任一合宜的方式。位在後隔板612之後方，座位單元之殼61 〇係按適當形狀製作，用以形成一中空的足箱630(見第21A及21B圖）。於第18及19圖中，係顯示相鄰座位的足箱63〇，。該足箱 20 63〇包括一大體上為水平的内殼，其所配置的垂直高度大體上係與下座位底盤628的高度相同，以及一開口 629係構成在殼610之後隔板612中，緊接著處在標準位置之背靠 624的後方，用以容許進出該足箱63〇的内部。该足箱包括一第一側壁632其係構成部分之相鄰單元 74 593064 玖、發明說明之设610的互連側壁616，其之方向大體上係與單元之抽象的縱軸平行。足箱630進一步地包括一第二相對側壁634， >、係與單元之抽象的縱軸成一對銳角，以致足箱之平面視圖係為具有一大體上為三角形或是梯形的形狀。於第18_ 21圖中，各納單元之足箱具有一大體上為三角形的形狀，但疋可在二侧壁632、634之間截頭成一端壁，將足箱構成為一梯形的形狀。可交替地，在希望將座位與一壁並列配置處，第一側壁632係可省略以致足箱之第一橫向側邊係為開啟的。足箱630之末端係位在後隔板612之上邊緣的下 10方，具有一大體上平坦的上壁636。該上壁636係構成為一大體上之三角形、平坦的部分638 ,其係使用作為供相鄰單元所用的一飲料用側臺（Side-table)。如第19圖中所示，位在足箱63〇與下座位底盤628内的上表面，係以厚的墊塞製作坐墊，或是支撐一床墊部分 15 652。同樣地，將座位底盤622之底側以及背靠624之後側製作墊子。於一“座位形式，，中，座位底盤622與背靠624通常係如第18、20A及21A圖中所示地配置，以致一乘客係可坐在座位上。然而，當乘客希望睡覺時，他或她可自座位起來 20並手動地將背靠624拉離後隔板612。如第20B圖中所示，背靠624係可相對於座位底盤622柩轉，並且連續地拉動背罪624，致使座位底盤622之後端部向上地提昇離開下座位底盤，並相關於其之前邊緣623樞轉。如第2〇c&21B圖中所示，係可操作座位底盤622及背靠624，用以提供一大體 75 593064 玫、發明說明上平坦且為連續的睡眠表面，其中背靠624之前側係支撐在托木640的-上表面上，介於背靠624、座位底盤⑵以及下座位底盤628之間的接頭係如第2〇c圖中所示地固定，用以構成一 “床舖形式，，。乘客因而可將他或她的頭部朝向 5前隔板6U而躺臥在平坦的表面上。藉由將背靠咖自後隔板612移開，露出通過殼㈣的開口㈣，容許乘客伸展他或她的下腿部通過開口進入足箱63〇中。在床舖形式中，擱板與下座位底盤628之裝有墊子的上表面，以及座位底盤622的底側與背靠624之背侧係可裝配適合的床單諸如床 10早與毯子，以及-乘客用枕頭係可放置在背靠似之後方於床舖$式巾所使用之單元的表面係可製作並裝上與在座位形式中所使用之不相同的塾子。當在客搶中所有的大部分單元係處在一或另一形式時，能夠在客艙内產生一特別的氣氛。 15 藉由將容納單元配置與飛機之前進方向約成4〇_5〇度的角度，較佳係約為45度，能夠提供一全長上達7呎（213 公尺）的乘客用床舖，同時配置大部分通常用在頭等艙的側檯638。與第1-2圖之座位單元4〇以及第夂5圖之座位總成相較’第18-21圖之容納單元係裝配用作為床舖形式，本 20發明之容納單元提供一大體上為水平的睡眠表面。第22-27圖中所示係為本發明之另一乘客容納單元。第22-27圖之單元的多數元件，係與上述於圖之單元的對應元件相似。因此，為了清楚可見，該等元件係以相同的代表符號加上1〇〇作為代表符號。因此，經由實例 76 593064 玖、發明說明，當第18-21圖之單元的後隔板係以代表符號612標示時，則第22-27圖之單元的後隔板係以代表符號712標示。因此，如第22圖中所示，另一乘客容納單元包括由二半殼710a及710b所構成的一殼710。該殼710包括一後隔板 5 712以及一前隔板714 ,其係藉由一互連的侧壁716而相互連接。於後隔板712的後方，殼包括一中空的足箱73〇其係具有相對之侧壁732以及一上壁736，該上壁73 6包括一大體上平坦、水平的部分738，其係使用作為供一相鄰座位所用的飲料用側檯。 10 第22_27圖之殼71〇係安裝在一底座（plinth)760上。該底座760係由一適合的飛機等級、重量輕的結構材料所製成，典型地係與殼710之材料相同，並且具有一平面的下壁762，其係配裝有適合的固定裝置（未顯示），用於將底座大體上固定至座位執道。 15 该底座760係構成有一凹部764，其係由具有一朝向内之上邊緣765的一直立側壁763所形成。該凹部764係在整個座位下方自前隔板714延伸進入足箱73〇中，該足箱係配置在地板高度。凹部764容納適於形成乘客用床舖的床墊或是相似的坐墊或墊塞。該凹部係按適當形狀製作用以抵 2〇銷於飛行當中飛機的些微傾斜，以致該床墊大體上係為水平的。與前隔板714並列的殼71〇承載一可移動拕架74〇，其係可在一大體上之垂直軸上，於第22及24八圖中所示之下展開位置，與如第24B圖中所示之一升高的儲藏位置之間移動。儘管對於熟知此技藝之人士而言顯而易見的是 77 593064 玖、發明說明複數種機構用於達成該托架的移動，但適合之機構的一實例係為配裝在前隔板714之内表面以及托架74〇上的互相。齒合滑道。配置適合的裝置，用於將托架74〇固定在上與下位置。 5 該殼710形成一乘客個人空間718，其係容納一座位 720係包括一座位底盤722以及一背靠724。該背靠724係永久地固定至後隔板712之内表面，同時座位底盤係在其之後邊緣723處樞接至後隔板712之内表面，用於在第22及 24A圖中所示之一下展開位置，與如第23及24^圖中所示 1〇之一儲藏位置之間移動。於展開位置中，座位底盤722之前邊緣725，係由構成在殼710上朝向内的突出部分乃2所支撐，其係構成座位總成720用的支撐結構。在座位底盤722的下方，殼71〇之後隔板712係構成有一開口 729，容許從乘客空間718進入足箱73〇之内部。該 15床墊係在座位總成72〇下方延伸通過開口 729進入足箱73〇内。位在座位底盤722與托架740的中間位置，凹部764係由一可移開假的地板嵌板770所覆蓋，其係由一適合的航工私準、承重材料所製成。該假的地板嵌板較佳地係 2〇與該互連側壁716連接，用於在第22圖中所示之一下展開位置，與一儲藏位置之間移動，該儲藏位置令嵌板770大體上垂直地延伸並與側壁716連續。於儲藏位置中配置牢固構件用於牢固嵌板。與一相鄰單元之座位底盤並列的足箱之第一侧壁732， 78 593064 玖、發明說明，其係構成一外凹部733,，在與相鄰單元之座位底盤722 相同南度處配置一裝有墊子的擱板73 5 ’，用以提供該座位底盤722之一橫向延伸部分。谷納單元720因而可在如第22及24A圖中所示的一“座 5位形式’’，其中座位底盤722係展開的，與如第23及24B圖中所示的一 “床舖形式，，，其中座位底盤722係相關於其之後邊緣723向上樞轉，之間具選擇性地操作用以在儲藏位置中平罪著为罪724之内表面。於床舖形式中，可移開假的地板嵌板770係可移動至儲藏位置，並且將托架74〇自其 ίο之下位置升咼至其之上升位置，從而露出位在托架76〇之凹部764内的床墊。將座位底盤722升高至其之儲藏位置，係有助於進入足箱730，並在床舖形式下於殼71〇内提供一更為寬敞的個人空間718。因此，於如第24A圖中所示的座位形式下，一乘客係 15坐在由單元720所提供之座位上，如有所需，並可在其之下位置中將他或她的腳搁置在托架74〇上。假若乘客希望睡覺，因而他或她可起立並抬起座位底盤722至其之位置，如第24B圖中所示。托架74〇可升高至其之升高的位置，並可將假的地板嵌板770移開。乘客因而可躺臥在凹 20部764内的床墊上，他或她的頭係朝向前嵌板了㈣且將他或她的腿伸人足箱73〇。藉由將趋“約成你％度的角度，例如，與載具之前進方向約成45度，並提供整體長度約上達7吸（2.13公尺）的一床舖。前隔板714係在睡著時用以保護乘客的頭部，並且托架76〇提供進入乘客個人空間 79 593064 玖、發明說明的一遞增部分，對多數乘客而言係具吸引力的。位在足箱 ^方的殼係可按適當形狀製作，用以提供—橫向座位延伸 P刀735 ’供-相鄰座位的座位底盤m所用，以及一大部分臨時的側檯738供相鄰座位所使用。 10 15 於第22-24圖之其他容納單元的一變化形式中，座位底盤722，於其之儲藏位置中，不相關於其之後邊㈣罐轉而平躺靠著背罪724之前表面’係可配置在如第26八圖中所概略顯示的一前位置’與於第25及26C圖中所示的一收回位置之間相對於喊7! 〇而滑動。於收回的位置中，座位底盤722或是至少為座位底盤⑶之大部分，係可於床塾上方垂直隔開的-位置處容納在足箱73〇内。適合達成該座位底盤722之滑動的複數種機構，對於熟知此技藝之人士而言係不言而喻的，例如配置在與座位底盤722鄰接之殼 710的内部表面上的線性軸承。有利地，滑動機構可配置一或更多的棘爪（未顯示），用於選擇地在至少一中間位置 ’諸如第26B圖中所示，停止座位底盤722移動。因此，於如第26A圖中所示之完全伸展的位置中，該單元係可針對放鬆而符合人類工程學地裝配而成，同時在如第26B圖中所不的中間位置，該單元係可裝配用以提供，例如，適於用餐或工作的一更加直立的乘客位置。於完全收回的位置中’ ¥座位係處在床舖形式時，大體上將座位底盤722儲藏用以容許進入足箱730。於第27圖中所示係為第22_24圖之容納單元的另一變化形式，其中可移開假的地面嵌板770係鉸接至互連側壁 80 20 593064 玖、發明說明 716，用於在一展開位置與一如第27圖中所示的儲藏位置之間移動，於展開位置中嵌板大體上係水平地覆蓋凹部 764用以保護床墊，於儲藏位置中嵌板大體上於垂直方向係為平坦，靠著互連側壁716。假的地板嵌板之底側 772係以適當的墊塞物製成墊子，以致連同床墊764，其係提供-沙發狀配置；於床舖形式，一乘客係可將他或她的月罪罪在瓜板770之底側772而斜向一邊地坐在床塾π#上。 ίο 15 20 於第28圖中所示，係為本發明之另一座位系統。第28 圖之特定系統係特別地設計使用在波音747.梅⑧型飛機的上”下甲板’但该系統可用在任一客機上，特別是在商務搶。第28圖之座位系統，在每一上與下^板上，包括複數之树㈣乘客容納單元例如第18-21圖或第22_27圖之容納單元。該每一容納單元8⑽係與一客驗側壁㈣並列 ’並且其之方向與並列的側壁810之縱方向约成你50度的角度，較佳約為45度’將單元之背部朝向壁81〇，以致座位大體上係面向驗内。藉由將單元8〇〇面向内，與座位大體上係前後對正的客搶相比較，此客搶係顯現較不擁擠的外觀。每一單元在單元的背部與並列的客艘侧壁810之間具有-大體上為三角形或梯形的伸展箱或空間請。一般地’飛機客驗壁在内部係為凹入的，並因此每一單元 _之延伸箱或”㈣’係延伸進人由壁所形成之凹部内 ^能夠最有效地利用客驗中空間。每一單元_包括用 ^供如上所述之床舖的構件，其係延伸入伸展箱或空間中，用以將可用的床舖長度達到最大。 81 593064 玫、發明說明於一些飛機地板平面圖中，同時可有足夠的空間用以朝向客艙之中心配置一或更多的單元，於第28圖中所示，係針對波音747-400⑧型飛機的下甲板。於該具體實施例中，配置二中央行之單元，其中每一單元的方向係與飛機前 5進方向約成45度的角度。中央單元800係成對地配置，每一座位大體上係面向客艙之前方並面向外，以致每對之二單元在向前的方向上相互叉開，並在後方之成對的單元的前方，在單元的後方大體上形成一四邊形空間。該四邊形空間840容納與每一單元8〇〇結合的伸展箱或空間，為了針 10對每一單元提供一伸展的床長。每一單元8〇〇包括相關於第18-21圖及第22-27圖之上述說明類型的一中空足箱處，母足相之上壁係可用以提供一方便的側檯或是其他的傢俱裝置供另一單元所用。相關於第29A至29C圖，本發明之一乘客載具用，例 15如，諸如飛機，第二乘客座位總成900，包括一固定的支撐、、Ό構’一般係以代表符號9丨〇標示，用於支撐離開載具之地板F的座位總成。該支撐結構9丨〇包括適於將座位總成附裝至地板的構件。例如，於座位總成9〇〇安裝在飛機上處，该支撐結構91〇典型地包括一或更多的固定裝置，用 2〇於將座位總成附裝至通常為飛機客艙之地板所用之類型的座位執道。與第卜2圖之座位單元40或是第3-5圖之第一座位總成相較，第二座位總成900之支撐結構可包括一底座或濩腋片，用於附裝至該座位軌道。該支撐結構910進而包括一升尚的乘客支撐構件912、914,該每一構件大體上 82 593064 玖、發明說明具有一平坦、水平的上表面（用以抵銷於飛行當中飛機的稍微傾斜）。該乘客支撐構件912、914係為隔開的，用以在支撐結構内形成一腔室916。该支撐結構910係可以任一為熟知此技藝之人士所熟 5知之適合的、飛機等級結構材料所製成。該支撐結構係可為骨骼狀，或可包括一或更多的實壁。典型地，該支撐結構係以一重量輕的合成材料所製成，但是前述之用於將支撐、’Ό構牛固至飛機中座位執道或是其他地板的固定裝置，係可包括一或更多之輕鋼材或鋁質的強化樑或底座。 1〇該腔室916容納一乘客座位，一般係以代表符號920加以標示。該乘客座位920大體上係由支撐結構91〇所支撐，並包括一背靠元件922以及一座位底盤元件924。該背靠元件以及一座位底盤元件922及924，係藉由一座位移動機構，一般係以代表符號930加以標示，與支撐結構91〇連接。 15 該座位移動機構930包括二相似的不規則形狀之多邊形板932，其係安裝在座位92〇之任一側邊上。應察知的是，於第29A至29C圖之側視圖中，僅能見到該其中之一板 932。每一多邊形板932係構成有一大體上為線性、伸長的狹縫934，其係與板之一邊緣935並列。與一相對邊緣％6 20並列，该板932承載二隔開的、朝向内之凸耳％?。介於凸耳937之間的一直線，係與該線性狹縫934成一對銳角。與該板932之另一邊緣939並列，該另一邊緣大體上在該一與相對邊緣935、936之間橫向地延伸，該板932係與一二配件連彳干組裝置940之一端部連接。該連桿組裝置包括一 83 593064 玖、發明說明第一構件941，其係樞接至該板932，以及一第二構件942 其係於一端部處樞接至第一構件941，用以構成一，，膝部，，接頭943，並於另一端部處與位在該支撐結構910上的一固定樞轉點944連接。 5 該座位移動機構包括用於將座位底盤與背靠連接的構件’以致背靠的下端部維持與座位底盤之後端部連續，同時容許該座位底盤與背靠彼此相對地樞轉。該線性狹縫934具有上及下末端954、955，並滑動地谷納一凸耳構件95 1，其係自座位底盤924之個別側邊突出 10 。與其之前端部925並列，該座位底盤924係與每一側邊樞接，於樞轉點952處，樞接至一線性支柱961的一端部。該線性支柱961係於其之另一端部962處樞接至一滑動臺架構件（未顯不），該構件係與位在座位底盤924下方的支撐結構 910連接。該滑動臺架構件係可移動地安裝至支撐結構 15 ，以致滑動臺架構件能夠在和第29A至29C圖對應的一上位置，與和第30A及3〇B圖對應的一下位置之間移動。配置適合的偏麼構件，例如，諸如彈菁、氣體支柱或相似物用於將/月動室架構件偏壓入上位置。具選擇性可鬆開的機械固定裝置通常係同時提供，用於將滑動臺架構件固定 20 在其之上位置。 β亥線性支柱961係搖動地安裝至滑動臺架構件，以致其能夠在如於第29Α圖中所示的—大體上為直立的位置，與如第29C圖中所示的—向前躺下位置之間搖動。該位在多邊形板932上隔開的凸耳937,係與—曲線的 84 593064 玖、發明說明軌道971嚙合，其係固定地牢固至背靠922的個別側邊上。如由第29A至29C圖及30A至30C圖中可見，該曲線的軌道 971係方便地構成在一伸長的板構件972中，其係附裝至背靠的側邊。該曲線的執道971分別具有上與下末端973、 5 974 〇相關於第29A圖，當該座位920係配置在一直立或“用餐”位置時，該二配件式連桿組裝置94〇係為一伸展的形式，以致第一與第二構件941、942大體上係互相為共平面的，並且該二第一與第二構件94 !、942大體上係自該樞轉點 1〇 944向上且向前延伸。該板932自附裝點向後延伸至第一連桿構件941，並定向以致該線性狹縫934向上並向後延伸。背靠部分922係位在一直立位置，而該隔開的凸耳係配置在曲線的軌道971之下末端處。座位底盤的方向大體上為水平’（於飛行當中）並且凸耳951係配置在線性狹縫州 15之上末端954處。滑動臺架構件（未顯示）係配置在如上所述其之上位置中，並且可搖動的線性支柱961其之方向大體上為垂直的。座位底盤924因而係在二乘客支撐構件912、 914之間向後地配置在腔室9丨6中。該座位底盤924具有-上表面926，其係適當地裝上塾 2〇子使用作為-座位元件。同樣地，該背靠元件922具有一前表面923,其係適當地裝上墊子使用作為一座位元件。較佳地，背靠元件之前表面923係經裝飾用以與座位底盤 924之上表面926配合。該其中之-的乘客支樓構件914係配置在座位920的前方’並使用作為—固定的腿靠部分似 85 玫、發明說明。該腿靠部分928具有一上表面929。 «亥線性支柱961係可操作地與一可具選擇性地操作的固定馬達傳動裝置（未顯示），其係能夠傳動支柱961，如上所述地，在第29A圖之直立位置與第29C圖之前傾位置之 5間相關於其之上端部962而搖動。在座位總成中配置適合的使用者控制裝置（未顯示），讓使用座位的一乘客能夠操作該固定傳動裝置。該背靠部分922具有一後表面921，其大體上係為平面的。當座位係如第29A圖所示為直立時，該後表面921係以 1〇一小間隙913與乘客支撐構件912隔開。該後表面921承載一床墊部分（未顯示），用以使用作為部分的床舖，該床墊 P刀係附裝至背靠部分922之後表面921，以致當背靠係為直立％，並未將床墊部分拆卸。該乘客支撐構件912同時具有一上表面911，其係支承著一床墊部分。一可移動充填之乘客支撐構件915係樞接至該乘客支撐構件Μ〗的一前 "^向邊4： 917。该充填構件9 i 5大體上係為直線的並具有上表面918，该大體上為平坦的上表面918係承載一床墊 P刀（未顯示）。该充填構件9丨5係可滑動地與背靠元件M2 後表面921連接。如第29A圖中所示，於直立位置中，充真構件915在固疋的乘客支撐構件9丨2與位在該間隙913中座位920的背靠元件922之間，大體上係直立地延伸。除了固定傳動馬達用於傳動線性支柱961之外，配置 $可具選擇性操作的機動化傳動裝置，用於相關於固定的樞轉點944向後地搖動該二配件式連桿組裝置940之第二 86 593064 玖、發明說明連桿構件942。該第二連桿構件942包括—向後延伸的较接部分945(見第遍圖），用於與該另一傳動馬達（未顯示）連接。同時可使用該使用者控制裝置，用以操作該機械固定 5裝置，在操作該第二傳動裝置的同時自其之上位置鬆開座位底盤。當座位係如第29A圖中所示為直立時，該座位係可藉 2操作㈣傳動馬達，用以相關於其之另—端部_而向前搖動該線性支柱961使座位後仰，同時滑動臺架構件（未 10顯示）支撐線性支柱961保持在其之上位置。藉由向前地搖動線性支柱961，座位之座位底盤元件924於腔室内係向前地受牵拉，並且凸耳951係沿著該狹縫934從該上末端 954滑動，朝向該下末端955。座位底盤之向前移動同時致使背罪922之下端部向前移動。背靠部分係受限制而於曲 U線軌道971内，藉由凸耳937之唾合而沿著一預定路径移動二軌道97K系按適當形狀製作’致使背靠奶在座位底盤向别移動時，漸進地向後後仰。當座位後仰時，凸耳937係沿著該曲線執道971，經由如第29B圖中所示的一中間位置而移動，並且該二凸耳奶 20係緊靠著曲線軌道971之上末端973，於該點處座位不能夠再進一步地移動，而座位係處在如第29C圖中所示之一後仆或疋倚罪”位置。應察知的是，固定傳動馬達之固定動作容許座位停止並固定在由第29八及29c圖所代表的二末端之間的任一所需之中間位置處。 87 593064 玖、發明說明當使用本發明之第二座位總成9〇〇的一乘客希望睡覺夺w亥座位總成係能夠轉換成一床舖。乘客操作該使用者控制裝置，用以將座位底盤由其之上位置鬆開，並致使第一機動化致動器如第3〇a圖中所示相關於該樞轉點944 ,向 5後地搖動連桿組裝置940之第二連桿構件942。當第二連桿構件942向後搖動時，介於第一及第二連桿構件94 J 之間的膝部接頭係中斷，容許第一連桿構件941相關於膝接 '"員943而向刖並向下地搖動，從而致使座位920之背靠凡件在腔室916内向前移動，並由其之直立位置向前地樞 1〇轉。當背靠元件922向前地樞轉時，其係在座位底盤部分 924上向下地推動，因而受引動在該滑動臺架構件（未顯示）上向下地移動，抵擋偏壓構件之動作。第二連桿組構件 942之持續的向後移動，致使多邊形板们2及背靠元件π〕朝向載具之地板F向下地移動直至，如第3〇3圖中所示，背罪元件922之後表面921係大體上水平地配置（於飛行當中），並且與乘客支撐構件912、914共平面為止。配置連桿組構件940、多邊形板932、曲線軌道971以及凸耳937，以致在如第30Β圖中所示的床舖形式中，背靠元件之上端部係緊靠著該向前乘客支撐構件914的後邊緣，用以與之構〇成一連績的表面。配置適合、可鬆開的固定裝置，用於將背靠922固定在端部位置。再者，如第3〇Α圖中清楚可見，當背靠元件922在腔室 916内向别摇動’並平移地向前移動時，充填構件915沿著背靠元件之後表面921滑動，受引動或容許向前樞轉直至 88 593064 玖、發明說明 ’如第3GB圖中所示，當背靠元件大體上係水平配置時，充填構件915在乘客支撺構件912與背靠元件似之後表面 921之間構成-橋接部分為止，以致乘客支樓構件912之上表面911、918、921、充填構件915以及背靠元件922大體 5上係為八平面，並構成一連續的表面。應察知的是，由乘客支撐構件912所承載的床塾部分、充填構件915以及該背靠元件922之後表面921，構成一伸長的床墊供乘客睡在其上。再者，在座位920之前方乘客支撐構件914之上表面 929,同時可承載一床塾部分，進一步地伸展由處在第遞 1〇圖之床舖形式的座位所構成的床舖。本發明之座位總成容許構成一連續的床舖表面，其之長度至少為78_8〇吋（1.98_ 2.032公尺）。於一些狀況下，由乘客支撐構件9ΐ2、Μ#之上表面9U、918、921、929、充填構件…5以及該背靠元件922之後表面921所構成的床舖，其之長度可超過以吋 15 (2.16公尺）。為了將座位總成900回復至一座位形式，第二馬達傳動裝置係受引動，用以相關於該固定的枢轉點944向前地搖動二配件式連桿組裝置940之第二連桿構件942，從而致使第一連桿構件941向後搖動，依次，致使多邊形板932向 2〇後搖動並向上移動，漸進地將背靠元件922恢復至其之直立位置。當背靠元件922回復至直立位置時，容許座位底盤元件924在該偏壓構件（同時未顯示）影響下，回復至位在承載構件（未顯示）上其之上位置。當座位底盤回復至其之上座位位置時，機械固定構件係自動地再次嚙合，用以將 89 593064 玖、發明說明座位保持在其之上位置。由檢閱第29A至20C圖可察知的是，該乘客支撐構件 912之上表面911，以及該充填構件915之上表面918，當座位總成係裝配為座位形式時，在座位92〇後方構成一便利 5的凹部98〇。該凹部980係至少部分地由座位920之背靠部分922所隱藏而不致看到。因此，該凹部98〇，例如，係可用於儲藏寢具材料，諸如枕頭、羽絨被及相似物。當座位總成係移動至第30B圖之床舖形式時，乘客能夠輕易地取用寢具材料並展開由如上述之座位總成之元件所構成的床 10 舖表面。之前所說明之乘客座位總成900的另一優點在於，該者Λ元件922之前表面923以及座位底盤元件924之上表面 926，能夠特別地裝上墊子並覆蓋使用作為座位元件。因此例如责罪元件與底盤元件922、924可承載發泡塾塞 15層，其係經特別的造型而使用作為座位構件。墊襯物之組織、圖案及/或色彩設計，以及用於覆蓋背靠元件之前表面923與座位底盤元件之上表面926的裝飾材料，係可為經特別選定使用作為座位的材料。相反地，由乘客支撐構件 912所承載的床墊部分、充填構件915以及背靠元件922之 2〇後表面921係可特別經設計用於使用作為寢具材料。因此，所使用之内部的彈起床墊部分或是發泡墊塞層係特別地按適當的形狀製作，而在將座位當作床舖使用時帶給乘客最大的舒適。特別地，用於裝飾床墊部分的材料與織物係可〃有、、文理、色彩等，其係特別地適於使用作為寢具材料 90 593064 玖、發明說明。用於裝塾部分的寢具材料，以及用以裝飾座位總成 ^座位部分的材料，彼此間係有相當不同的外觀。然而，可以察知的是，當該座位係裝配使用作為一座位時，寢具材料大部分係藉由背靠元件922加以隱藏，而僅能看到該座位之貫際構成部分之座位的該等部分。同樣地，當重新裝配座位而使用作為床舖時，背靠元件之前表面以及座位 &瓜7G件之上表面大體上係經隱藏而看不到，而僅能夠看 ίο 2寢具材料，其係包括位在乘客支撐元件912上的床塾部分、充填構件915以及背靠元件922之後表面921。 15 於一載具客驗中，例如，在飛機上安裝複數之本發明的乘客座位總成，其係可用以根據大部分的座位總成係配置為床舖形式或是座位形式，而帶給飛機客驗二種不同的 :覺外觀或氣氛。因此’在白天飛行期間，或是在一持久飛仃的白天部分’大部分的乘客座位總成係配置為座位形式，如第WC圖之其中一圖所示。寢具材料大體上係經隱藏’而僅能夠看到總成之座位表面。當然，座位總成係可裝飾成任-所需的設計但，例如，座位總成裝上墊子並經裝飾帶給錄具有私人會Μ樂部料觀。例如，座位底盤元件924之上表面926以及背靠元件似之前表面 923係可裝上皮質的塾子。在夜間飛行期間，或是在一持久飛行的夜間部分’大部分或是所有的座位總成係袭配為床舖形式，如第則圖所示’於該狀沉下，總成之座位部分大體上係受隱藏，而僅能夠看到乘客支撐構件912、之上表面911、918、921、929、充填構件915以及該背靠 91 20 593064 玖、發明說明元件922所支承的寢具材料。用於裝飾床墊部分的材料，與用以裝飾背靠元件922之背面的座位侧的材料相較具有一顯著地“較為柔和”的外觀，為了帶給乘客客艙一適於睡眠之具吸引力、悠閒的氣氛。第3 1及32圖係分別地顯示二不同的座位系統，每—系統包括複數之於之前相關於第29-30圖所示類型的座位總成。於第3 1圖中，一飛機客艙尤其係由二相對的曲線壁 1001、1002所形成。為熟知此技藝之人士所廣為熟知的是 ’該每一壁1001、1002大體上在其之内部表面上係為凹入 10 的。與該每一壁1001、1002並列地配置一行1029本發明之 15 乘客座位總成900。關於其中之一代表的座位總成9〇〇，每一座位總成900形成一係以代表符號1012標示的抽象的縱軸。座位總成900係定向相關於鄰接之客艙壁1〇〇1、1〇〇2 成一對銳角。第31圖同時顯示與壁1001並列的一抽象的“ 向前”軸1014。應察知的是，朝向飛機前方的“向前，，軸 1014，事實上並未相關於飛機之前進方向而精確地向前定向，但方向大體上係與鄰接侧壁1 〇〇 i之前後方向平行，而忽略該側11001的些微彎曲。該每一㈣座位總成9〇〇的方向，係在座位總成之抽象縱軸1G12與飛機客搶之抽象的 “向前’’軸1014之間形成一約為4〇度的α角度。每一座位總成係配置以致乘客支撐構件912延伸進入由該側壁麵、 1002之^特性所形成之凹部。座位92_關於客驗係配置面向⑴並向Θ W及—低的隱私隔板927係構成環繞著乘客支撐構件914的前端部，俾便環繞著每—座位總成形 92 20 593064 玖、發明說明成一乘客個人空間。藉由定位每一座位總成，以致乘客支撐構件912延伸進入由凹入的側壁1〇〇1、1〇〇2所形成的凹部，而在飛機客艙中形成最大的可使用空間。可以察知的疋，在將座位配置為床舖形式時，乘客支撐構件912係僅 5由乘客所使用，因而在乘客支撐構件912上方不需要全高淨空局度（full-height headroom)。在鄰接的座位之間配置合適的隱私隔板，並如第3 j圖中所示與母一座位總成鄰接並位在相鄰座位總成之乘客支撐構件912後方的一空間1015，係可用以提供一座位高 1〇度的表面，使用作為一雞尾酒檯或是類似裝置。於客艙空間容許的位置處，除了與客艙壁1〇〇1、1〇〇2 並列的座位總成9〇〇行之外，係可安裝一或更多之中央行 1030的座位總成900。第31圖係顯示一客艙設備，其中係女装一中央行1030的座位總成。在每一中央行1〇3〇内，如 15上所述，座位總成900係配置與飛機客艙之前後向軸成一對銳角。座位總成900同時係配置為二列，於每一列中，座位總成係背對背地配置，因此位在相同列内鄰接座位之乘客支撐構件912係互相連續地配置，因此位在相同列内郇接座位之乘客支撐構件912 ,係互相連續地配置，並且 2〇在座位係為座位形式時，大體上係由並列的座位920之背靠元件加以隱藏而不致看見。第32圖係顯示適用於包括三行1129、1130之座位總成 900的種座位系統，其係包括二行1129，分別地與客艙之二縱向壁1101、1102並列，以及一單一的中央行。與於 93 593064 玖、發明說明第31圖中所示的設置相較，在與其中之一客艙壁11〇1、 1102並列的每一行1129中的座位總成900，其係定向以致座位相關於客搶係面向前並向内。位在中央行113 〇内的座位總成，同時係配置成面向前且面相一侧邊。每一座位總 5成在座位總成9〇〇之抽象縱軸1112與客艙之前後向軸丨丨14 之間，係形成一約為49度的對銳角β。第33 Α至33C圖係顯示本發明之一第三乘客座位總成。對於第33A至33C圖之第三乘客座位總成的元件而言，係與第29A至29C圖以及第30A與30B圖之總成的對應元件 1〇相似，因而使用相對應的代表符號，但於符號之前加上 “12”以取代“9”。因此，第33A至33C圖之第三座位總成的支撐結構1210 ,係與第29A至29C圖之第二座位總成的支撐結構910相對應。第33A至33C圖之第三座位總成包括一支撐結構，一 15般係以代表符號1210標示，用於支撐總成離開一載具之地板F，例如，諸如一飛機客艙的地板。與上述第29及3〇圖之第二座位總成相似，第33A至33C圖之第三座位總成包括二升高、輔助的乘客支撐元件1212、1214，其係隔開並互相對置用以在支撐結構内構成一腔室1216。該腔室1216 2〇容納一座位，一般係以代表符號1220標示，該座位包括一背靠元件1222以及一座位底盤1224。該座位底盤1224具有月1J ‘部1225以及一後端部1223，並係在其之後端部1223 樞接至为罪元件1222之一下端部1226。該座位底盤1224係藉由一座位移動機構（未顯示）而可移動地連接至支撐結構 94 593064 玖、發明說明 1210，容許座位底盤1224於腔室1216内，大體上在如第 33A圖中所示的一上位置，與如第33C圖中所示的一下位置之間垂直地移動。配置適合的偏塵構件（未顯示），用於將座位底盤1224偏壓入上位置，並配置可具選擇性操作的 5固定裝置，用於將座位底盤1224固定在上位置。該背靠元件1222係於一固定的樞轉點1230處，樞接至該支撐結構1210。該背靠元件1222具有一後表面1221，其係包括一延伸部分1231位在背靠元件1222之下端部1226，當背靠元件1222係位在一直立位置時，延伸部分1231係向 10 下延伸越過固定的樞轉點1230。座位底盤元件1224之上表面與背靠元件1222之前表面，係裝上以特別設計針對使用作為座位的材料製成的墊子並覆蓋。乘客支撐元件1214係與座位122〇之前方袼隔開，並能夠在座位1220處在第33A圖中所示的直立位置時，能 15夠使用作為一搁腳部分元件1228。乘客支撐元件1212係配置在背靠元件1222之後方，並與其隔開一小的間隙1213。該背靠元件1222之後表面1221大體上係為平坦的，並承載一第一床墊部分（未顯示），其係經特別地設計並裝飾使用作為寢具元件。該乘客支撐元件1212具有一上表面 2〇 12U，其同時係承載一床墊部分。背靠元件1222與乘客支撐元件1212在者罪元件1222的後方形成一凹部1 280，其係用於儲藏寢具材料，諸如枕頭、羽絨被、小毯、毛毯及相似物。本發明之第三乘客座位總成的一優點在於，當背罪係位在如第33A圖中所示的直立位置日夺，凹冑128〇係被 95 593064 玖、發明說明隱藏而不致看到，因此整齊地將任何的儲藏在凹部内之寢具材料隱滅。該背靠元件1222相關於該固定樞轉點1230由第33A圖中的一直立位置，樞轉至於第33C圖中所示的一床舖位置 5 。該背靠元件1222以及該樞轉點1230係經設計，利用乘客支撐元件1212、1214，以致，於床舖位置中，背靠元件 1222之後表面1221係配置與該二乘客支撐元件1212、1214 為連續的，用以構成一大體上為平坦並與之為連續的表面。於第33C圖之床舖形式中，由乘客支撐元件1212之上表 10面1211所承載的第二床墊部分，以及由背靠元件1222之後表面1221所承載的第一床墊部分係互相緊靠或是幾乎緊靠，用以構成一伸展的床舖，可供使用該座位的乘客睡覺。乘客支撐元件1214之上表面1229,同時構成一作為床舖的伸展表面。與上述之第一與第二座位總成相較，根據第三 15座位總成，其係能夠用以構成一床舖，其之點對點的總長度係至少為78-80吋（1.98_2·032公呎），並且在一些例子中，至少為85吋（2.16公尺）。背靠元件1222在第33Α及33C圖之直立與床舖位置之間的移動係可機動化（未顯示），並可鄰接於座位^細配置 2〇適合的可使用者操作控制裝置⑺時未顯示），使乘客能夠控制座位的作動。當座位係處在如第m圖中所示的直立位置時，係可將固定機構移開從而將座位底盤自其之上位 f鬆開，並作動馬達傳動裝置致使背靠元件咖相關於固定的樞轉點】230向前地搖動。當背靠元件1222向前搖動時 96 593064 玖、發明說明 ’其係緊靠在座位底盤元件1224上，在腔室1216中向下地推動座位底盤元件丨224，抵擋前述偏壓構件的作用。於第33C圖中所示的床舖位置中，座位底盤元件1224 係το全地由背靠元件1222所隱藏。因此，與上述第一與第 5 一座位總成相較，背靠元件1222之前表面與座位底盤元件 1224之上表面係可以材料覆蓋，所造成之視覺外觀與客驗氣氛，與用以裝飾由背靠元件1222之後表面1221以及乘客支撐το件1212之上表面1211之寢具配件的該等材料所造成之視見外銳與客驗氣氛相較係完全不同。當背靠元件1222 10係為直立時，可見到背靠元件1222與座位底盤元件1224之座位表面，同時背靠元件1222之後表面1221與乘客支撐元件1212之上表面1211的寢具表面係被隱藏。另一方面，當座位係處在第33C圖之床舖形式中，背靠元件1222與座^ 底盤元件1224之座位表面係被隱藏，同時可看見寢具表面 15 1221及1211 。根據以上最先說明的第二及第三座位總成的一特別觀點，因此，背靠元件922 ; 1222具有一第一座位表面923 ;-其係與上表面926構成部分的座位；_座位底盤924; 1224以及-相對的床舖表面奶；1221係用以構成具有一 2〇或更多之其他辅助的乘客支撐元件912、914; 1212、1214。本發明之乘客座位總成因而係特別有利的，因為盆容許在飛機客艙或是其他載具中提供一乘客用之長的床舖，在最小的座位間距下甚至能夠提供身高超過冗⑴他 2.032公尺）之高個子乘客舒適地乘坐。根據本發明，藉由 97 593064 玖、發明說明 10 15 20 配置一座位總成與一凹入艙壁並列，將後乘客支撐元件 912，1212配置與該客艙壁相鄰，能夠有效率地使用客艙内的可用空間。於一座位形式中’背靠元件922 ; 1212係以後乘客支撐元件912 M212構成一凹部98〇 ; 128〇，其能夠用以整齊地將寢具材料，諸如小毯、毛毯、枕頭等加以隱藏。背靠元件922; 1212之座位與廢具表面能夠分別地造成不同的視覺外觀，以致在一客搶設施中，包括複數之本發明的座位總成，當所有或是大部分座位總成係配置為座位形式時，能夠達到一第一客艙氣氛，當所有或是大部分座位總成係配置為床舖形式時，能夠達到一第二、不同的客餘氣氛。再者，座位與寢具表面係能夠分別地針對其之特定的用途使用。因此’例如，背靠元件922; 1212之座位表面係可配置發泡塾塞或相似物，並係經特別造型而使用作為一座位元件，同時背靠部分之寢具表面係可配備 -床塾部分或是其他舒適、彈性層，其係按適當形狀特別地製作用以作為-床舖元件。本發明之座位總成的另一優點在於，於床舖形式中，座位底盤元件924; 1224係完全，或大體上係由背靠元件922; 1212所隱藏，以致用於覆 i座位底盤元件之材料的外觀’不至損壞由寝具材料所提供的外觀及氣氛。較佳地，本發明之座位總成包括一腿靠部分他㈣’係與座位92〇;㈣的前方隔開，於床舖 $式中’腿件構成部分之伸展的床舖表面。【圖式簡單明】面、概略平面第1圖係為一飛機機身的一前部分的截 98 593064 玖、發明說明圖，顯示本發明之一種包含複數之個別的座位單糸統。元的座位第1A圖係為第1圖之部分的放大視圖，顯座位單元。示三相鄰的 ίο 15 20 第2圖係為第ία圖之三相鄰的座位單元的等角視圖。於第2圖中，其中之一座位單元係顯示為直立座位形式，另-所示為後仰座位形式，以及第三者係顯示為_床舖形式。第2A圖係顯示於第2圖中所示類型的個別座位單元的一支樓結構的-部分，其中將可移動座位元件移開。第3圖係為本發明之一種載具用第—乘客座位總成的一概略側視圖，係顯示一直立的座位形式。、第4圖係為第3圖之第一乘客座位總成的另一概略的側視圖，係顯示一完全後仰的座位形式。、第5圖係為第3及4圖之第一座位總成的另一概略的侧視圖，係顯示一床舖形式。第6圖係顯示第3至5圖處在直立座位形式之第-座位總成的部分的一等角視圖’其中將坐墊移除。土第6A圖係為構成部分之第6圖的第—座位總成的一背罪元件的一侧視圖。第6B圖係為第6八圖之背靠元件的-等角視圖。^圖係為在第6圖中所示之部分的第—座位總成之另一專視圖，其中座㈣成係處在完讀㈣座位形式。糊係為第6及7圖之部分的第—座位總成的另-等 99 玖、發明說明角視圖’其中座位總成係處在床舖形式。第9圖係為第3至8圖之部分的第—座位總成的一座位動機構的-等角視圖，其令所示為床舖形式。第1 〇圖係為第9圖之部分的# A # $ 丨77的座位移動機構的一側視圖 ’其中所示為座位形式。第11圖係為第9及1 〇圖之邻八沾产〜、 p刀的座位移動機構的另一側視圖，其中所示為床舖形式。苐12圖係為第9至11圖之部公的亦丨刀的座位移動機構的一放大的等角視圖。 10 第13圖係為第3至8圖之第一座位總成的部分之座位後仰子機構的一等角視圖。第14圖係為第3至8圖之第一座位總成的部分之座位轉換子機構的一等角視圖，其中所示為床舖形式。 15 第15圖係為第14圖之部分的座位轉換子機構的另一等角視圖，其中所示為-座位形式將一蜗桿(赠㈣咖）自 -對應的職(丽m gear)中移開，用以容許在座位與床舖形式之間手動地移動座位轉換子機構。第16圖係為第14及15圖之部分的座位轉換子機構之一放大、截面側視圖。 20 扣圖係為本發明之另-座位系統的-截面、概略平面圖。第18圖係為本發明之一乘客容納單开 +谷、乃早凡的一等角視圖其中所示係為一座位形式。第19圖係為第18圖之一乘客容納單元的一等角視圖 100 593064 玖、發明說明其中所示係為一床舖形式。第20A-20C圖係顯示第18及19圖之乘客容納單元在床舖形式與座位形式之間互相轉換的概略側視圖。第21A圖係為第18及19圖之乘客容納單元的一概略、 5等角視圖，顯示一乘客使用處在座位形式下的座位。第21B圖係為第18及19圖之乘客容納單元的一概略、等角視圖，顯示一乘客使用處在床舖形式下的座位。第22圖係為本發明之另一容納單元的一等角視圖，其中所示為一座位形式。 10 第23圖係為第22圖之乘客容納單元的一等角視圖，其中所示為一床舖形式。第24A圖係為第22及23圖之乘客容納單元的一概略、等角視圖，顯示一乘客使用處在座位形式下的座位。第24B圖係為第22及23圖之乘客容納單元的一概略、 15等角視圖，顯示一乘客使用處在床舖形式下的座位。第25圖係為第22及23圖之乘客容納單元的一變化形式的等角視圖’其中係包含一滑動座位底盤。第26A-26C圖係概略地顯示滑動座位底盤之不同位置的側視圖。 20 第27圖係為第22及23圖之乘客容納單元的另一變化形式的等角視圖。第28圖係為一飛機機身之一前部分的上及下甲板的概略、截面平面圖，顯示本發明之另一座位系統應用在一波音747-400⑧型飛機之上與主曱板。 101 593064 玖、發明說明第29A圖係為本發明之一第二乘客座位總成的一概略側視圖，其中所示的座位總成係處在進餐位置。第29B圖係為第29A圖之第-恭安广“ ^ 1 ^ . 口心弟一聚客座位總成的一概略側視圖，其中所示係處在一中間後仰位置。 5 第29C圖係為第29A及29B圖之第二乘客座位總成的一概略侧視圖，其中所示係處在一完全後仰位置。593064 发明 Description of the invention (the description of the invention should state: the technical field to which the invention belongs, the prior art, the content, the embodiments, and the drawings). The new 5-wing seat system for passenger vehicles, especially aircraft. The present invention also relates to a passenger accommodating unit for a vehicle ', which is a passenger facility suitable for providing individual, self-provided seats and sleep. The accommodating unit of the present invention can be used in any passenger vehicle, including buses, buses, ferries, and train cars, but it is particularly suitable for use in aircraft. The invention also includes improvements for vehicles, especially aircraft, 10 passenger seats or related. C Prior Art 3 Background of the Invention 15 20 A passenger seat for a conventional aircraft includes a backrest and a seat chassis that is supported away from the floor of the vehicle by a suitable support structure that is fixed to A pair of seats on the floor were on the way. When a passenger using a seat is viewed in perspective, the seat system forms an abstract longitudinal axis of the seat, and a plurality of such seats are arranged in rows in the cabin of the aircraft fuselage, each row extending transversely. Passing the cabin, one after the other, each-Yu Zhihuan body is aligned with the longitudinal axis of the fuselage so that the mother-seat is facing forward. Normally, during the flight, seat month # 月 ^ is sufficient to recline from the upright position to a recline position where passengers using the seat feel comfortable. -Some of the prior-art passenger seats, especially those used for business and first-class inspections of aircraft, in which the distance between adjacent door seats is larger than that of economic seats, and the same includes-leg rest (Ieg . Coffee) 7 593064 64, description of the invention /, is connected to the front of the seat chassis 'and can be in the lower or storage position, wherein the legrest is suspended from the seat chassis and is generally perpendicular to the floor' and-raised Or in an unfolded position, where the legs are extended forward from the seat chassis to support the passengers' legs moving off the ground. Therefore, it is said that the first-type pawl passenger seat is able to obtain a considerable degree of comfort by reclining the back and raising the legrest with a legrest fitted. The above-mentioned traditional aircraft passenger seats are generally satisfactory for short-haul transportation that lasts three to four hours, but not for longer flights that passengers want to sleep. Even if 10 is in the reclined position described above, the passenger using the seat remains in a sitting position. Most passengers find it difficult to sleep comfortably when sitting. In recent years, the number of passengers on long-haul flights has increased significantly, so the industry tends to design passenger seats that allow passengers to adopt a recline position during flight to help sleep. This is especially important for business travelers, who need to feel refreshed and alert when they arrive at their destination. 20 The industry has revealed that to increase the degree to which an aircraft passenger seat can recline, it can be adjusted, but it includes the extent to which a backrest can be extended backward and the legrest can be raised. Using this technique, it stretches to its limit when the back is leaning back and the leg is raised. It is able to form a generally flat bed, which is generally configured to be in common with the seat chassis each time it is stretched to this condition. flat. The -systemic-disadvantage is that the spacing between adjacent rows of seats must generally increase the maximum height to accommodate passengers. Although this situation sometimes occurs in the areas of the head of the aircraft, it is generally not slow for commercial products. The description of the invention is from white, °, and even though it can form a flat surface that is arranged substantially horizontally. 4 The surface is still not ideal, because foam or other cushions on the seat are generally used as a seat, but for a bed, the system needs to have a substantially flat surface. 10 15 In German patent GB23 Assist 4A, a seat unit for first-class grabbing of an aircraft is disclosed, which includes an auxiliary seat system configured to face a main seat. The auxiliary seat has a _ seat part system configured to cooperate with one of the main seats. When used to form a flail, flat surface for sleeping when the backrest of the main seat leans back to a horizontal position. The seat unit defines an abstract spoon longitudinal axis, and a plurality of the seat units are related to the relationship between the longitudinal axis of each seat and the longitudinal deviation, and can be arranged side by side in the guest inspection. The direction of each seat unit It is at an acute angle to the longitudinal axis of the aircraft fuselage, so that a generally triangular or trapezoidal space is formed in front of or behind each seat unit (depending on whether the seat unit faces outward or inward relative to the cabin). This space uses w to accommodate the worktop (counter_top) to the side of an adjacent seating unit, and can optionally be a food cabinet or other storage space. The advantage of German patent GB2326824 A is that in combination with an additional, auxiliary seat in a flat sleeping surface with the backrest, seat part and legrest of the main seat, it can form a long sleeping surface, which can provide height At 6 feet (1. 83 meters) for passenger comfort. However, the seat unit of the German patent GB2326824 A provides even higher overhead costs in terms of cabin space compared to the conventional system described above. In addition, it still has the disadvantage that the seat cushion is mainly designed to be used as a seat rather than as a bed. . One disadvantage of the seat of German patent GB2326824 A is that it takes up 9 20 593064 930, a large floor area in the description of the invention. Given its overall length, the seat unit of German patent GB2326824 A is completely unsuitable for use in the business class of an aircraft. . The world patent WO 00/21831 A2 discloses a seat unit, which is mainly used in the business class part of an aircraft cabin, and can convert the seat unit into a bed. The seat unit of the world patent WO 00/21831 A2 includes a pair of oppositely facing seats, each seat including a seat space for the occupant's body and an extension space for the occupant to place legs. The seat is configured to allow each side of an abstract dividing axis to extend one seat space beyond that axis into the extension space of the other seat. When installed in the cabin 10 of an aircraft, one of the seats is generally forward facing, while the other seat is generally rearward facing. Each seat of the seat unit of the world patent WO 00/21831 A2 contains a main seat, which is substantially the same as the main seat of the aforementioned German patent GB2326824 A but does not have a leg rest, and a 15 20 auxiliary The unit is #square with the main seat. Each seat thus includes a main seat with a reclining back and seat chassis, and an auxiliary unit including a raised cushion which is used as a footrest Part of the rest). The main seat can be reclined, so that when the backrest is reclined, the seat chassis moves forward to contact the auxiliary unit, which is used to constitute-continuous table:, the surface is used as-sleep for passengers Surface. Compared with the German patent GB2326824 A, the seat unit of the world patent w00 / 2i83i A2 therefore has the advantage of providing passengers with a substantially horizontal sleep: surface during long flights. However, the world patent w00 〇 / 2183i Seat M is long wasted in terms of the space available in a typical business class, and its disadvantage when assembled as a bed is that each seat cannot Material 10 玖 Description of invention Tall passengers get comfortable service. Compared with the seat of the prior art described above, each seat of the seat unit of the world patent WO 00/2183 1 A2 has its seat cushion not specifically for use as The sleeping surface is designed, and its contour assembly is mainly aimed at the disadvantages of the use of the seat surface. Another feature of the passenger seat used in the first class of the aircraft is the wide seat width. It is the same as the world patent WO 00/21831 A2. A further disadvantage associated with seat units is that in order to accommodate the largest total number of people in business class, the seat width is reduced to make most passengers feel uncomfortable. Although the seat unit of the world patent WO 00/21831 A2 is targeted during flight It is recognized as an advantage to provide a substantially flat sleeping surface for passengers, but its overall size makes passengers with height and / or weight above average feel slightly narrower. Furthermore, privacy barriers are arranged in Between the adjacent seating units, plus the total number of seating units configured in the business-class restricted space A 'leads to the cabin There is a slightly crowded scene on it. French Patent No. 987559 A discloses a public transport vehicle, such as an electric car, a bus and similar vehicles, which uses a seating device that includes rows of seats, each seat including a supporting structure It is used to support the seat off the vehicle floor, a seat chassis and a backrest. A walkway is formed between two adjacent rows of seats. The seat chassis of one of the seats adjacent to the aisle can be adjacent to the aisle. The three-seat support structure is removed and lifted in an upside-down direction to form an additional seat in the aisle. The back of a seat can thus be swung forward into the space previously occupied by the seat chassis 'To provide the seat with an alternative seat chassis. The back of a seat has front and back surfaces, both of which can be used as part of the 593064 kan, invention description seat. The entire row of seats is optionally capable of supporting a mattress to form a reclining seat. However, the device of French Patent No. 987559 a is not suitable for use on passenger aircraft, because the aisle of the aircraft must be kept open at all times. Furthermore, a plurality of adjacent seats are used to provide support for a single seated and dual-use 5 seat. . Therefore, the device of French Patent No. 987559 A cannot provide one seat and one seat for each seat. Japanese Patent No. 5-13838 A discloses a seat system for vehicles such as buses and trains, which includes a plurality of seats. Each seat contains a seat chassis and a backrest that can be swung between 10 positions in an upright position and a reclining position, and the seats are arranged in the cabin, which is angled and facing outward with respect to the centerline of the passenger grab. A substantially triangular space is formed between each seat and one of the walls of the cabin. This space accommodates a box +, which contains a footrest for adjacent seats. 15 20 French patent 647809 discloses _ a kind of seat system for sleeper cars, in which a plurality of seats are arranged with the longitudinal axis of the sleeper car _ Xiao degree, and are facing inward to form a general behind each seat Triangular: space is used to accommodate a small table for adjacent seats. SUMMARY OF THE INVENTION Therefore, the purpose of the present invention is to provide improved passenger inspection for commercial use of passenger aircraft. In particular, it is an object of the present invention to provide the passenger grabber which combines a flat sleeping surface having a maximum length ' and preferably a maximum width at the same time. The purpose of the present invention is to provide an improved passenger accommodating sheet for vehicles. The invention description is particularly for aircraft. The accommodating unit is used to provide passengers with their own, individual seats and sleeping passengers, especially It is used in the business class of aircraft, where the spacing between adjacent rows of seats is typically 50_60 inches (127 to 1. 52 meters). Another object of the present invention is to provide a passenger accommodating unit which can be converted into a bed with a maximum length to accommodate tall passengers, especially those who are taller than 6 feet (0.83 meters). Another object of the present invention is to provide a load-carrying passenger accommodating unit having a seat surface, which is particularly used as a seat surface and a bed surface, and is particularly used as a bed surface. 15 20 A different object of the present invention is to provide a passenger accommodation unit that can be converted into a $ bunk and can contribute to the lift or the atmosphere of the first cabin when assembled into a seat, and can Improve or contribute to the different cabin atmosphere. Therefore, another object of the present invention is to provide a seat system for vehicle cabins, which includes a plurality of passenger accommodation units that can be replaced with beds. When all or most of the units are assembled as seats, they are capable of Bringing passengers a special overall visual appearance and 'when all or most of the units are assembled as beds, this is enough to give the cabin a second overall look or atmosphere. Another object of the present invention is to provide a passenger vehicle, especially an aircraft, with a seat system which can make the most efficient use of passenger space. / Another object of the present invention is to provide a passenger seat system of the __ type, which has a substantially non-crowded appearance. Further objects of the present invention are described by the following inventions and specific examples of the present invention: 13 593064 发明, description of the embodiment of the invention, it is obvious to those skilled in the art 0 10 15, using passenger accommodation unit, which is Used to provide passengers with their own, individual seats and sleeping berths, the accommodation unit includes: a support structure for supporting the assembly leaving the floor of the vehicle; one or more movable passenger support, structural elements; And a member for connecting the movable, structural element to the structure, so that the element is optionally in the form of a seat with a plurality of passenger supports on the one or more structural, movable elements The surface or the support structure is used to form a passenger seat, and a bed form, wherein the plurality of support surfaces are substantially coplanar and continuously arranged 'for formation-moving between passenger beds; its characteristics It is at least that the movable element is double-sided, including the _th and second opposite sides, and among which, the side has a _th seat surface attached to the seat In the form of constituting the seat portion, and another - with a side surface of the second bed in the system " hai bed constituting the form of the portion of the bed. ★ Double-sided, movable, structural elements may include an internal, load-bearing diaphragm with first and second opposite surfaces, and first and second outer seat layers 20 = to be placed at the first- Support 2 with the diaphragm on the second surface. Therefore, 'the one side of the two-sided movable element, for example, the contoured surface of the foamable padding layer can be made in an appropriate shape and used as a seat element And, the other transparent system can carry a foamed packing layer with a substantially denier surface, which is used as a part of the bed. The first side of the two-sided 17-personal moving element! You have a first appearance, which is 14 593064, the description of the invention helps or enhances-the overall passenger appearance suitable for the seating environment. For example, the first surface may have a leather or leather-like seat cover. The second surface may have a visual appearance that contributes to or enhances the overall cabin atmosphere suitable for a sleeping environment. Therefore, the second surface can be fitted with a fabric or a cushion whose appearance is usually combined with the bedding material. The vehicle side is preferably a double-sided member. The backrest element can be connected to the support structure so that it can optionally be pivoted between a first substantially upright position and a second inclined position, the first substantially upright position with the first surface being configured A seat for forming a part, and a second 10 inclined position, wherein the second surface is a bed configured for forming a part. Preferably, the surface of the second bed of the 7G Moon Sin is substantially horizontal in the second inclined position. In some embodiments, one or more of the passenger support surfaces may form a seat chassis. The backrest element system can be connected to the structure so that the backrest element system covers the seat chassis in the first inclined position. Therefore, according to the present invention, the seat chassis may have a dedicated seat surface which is made in a proper shape and fitted with a cushion, and is particularly used as a seat. In the 幵 7 style of the bed, the seat chassis in the second inclined position can be hidden by the backrest element in whole or in part, so that the seat appearance of the seat chassis is hidden by the backrest 20. In some embodiments, the seat chassis may include one or more of the movable elements, which are connected to the supporting structure to move a party with a vertical element between an upper unfolded position and a lower storage position upwardly. , And the seat chassis moving member is arranged when the backrest element is moved from the upright position 15 593064 发明, the description of the invention is moved to the inclined position, used to move the seat chassis from the upper deployment position to the lower storage position. Therefore, in this second inclined position, the backrest element system can occupy the space occupied by the seat chassis in the upper unfolded position. In the form of a bed, the seat chassis can be moved to a storage position below it. This feature of the fifth aspect of the present invention allows the bed surface of the seat assembly to be disposed at a relatively low height from the floor of the vehicle, making it easy for passengers to climb on and get out of the bed. In a preferred embodiment of the present invention, one or more of the passenger support surfaces include a bed extension surface. 'In the seat form, the bed extension surface is configured or deployable to forward or backward the seat. Configuration. The crescent element may be connected to the structure such that in the inclined position the surface of the second bed and the surface of the bed extension form a substantially continuous surface. The bed (extended surface is configurable or expandable to position the seat chassis elements forward so that 'in the form of the seat' the extended surface of the bed can be used as a footrest b. The accommodation unit therefore does not have a connection to the seat The chassis and legrest elements that can be unfolded from the seat chassis. Therefore, the 'accommodation unit of the present invention may be located at a position spaced from the front of the seat chassis, including a -minute surface. In some embodiments, one or more Many of the passenger support surfaces may include a back extension surface located behind the backrest element, and the backrest μ element system may be connected to the structure such that, in the inclined position, the second bed surface and the extension surface are substantially The upper system is coplanar. In some embodiments, in the inclined position, the backrest element system can be separated from the front surface of the back extension surface, and a movable filling element is provided, which is connected to the structure. So that it can be moved between a storage position and-unfolding 16 593064 发明, invention description position, when the filling element is unfolded, the filling element includes a "branch" filling form The surface is extended between the backrest element and the back surface extension surface so that the back surface extension surface, the filling surface, and the second bed surface form a substantially flat surface, and can be configured to stand upright as the backrest element. When the position is moved to the tilted position, it is used to move the filling element from the storage position to the „helium unfolding position. The filling element can be rotatably installed in the rear S position of the back piece in the middle of the rear extension surface so that it is in the storage position ' The filling element can be formed with the horizontal plane, and it can be expanded to the unfolded position. Therefore, in the form of a bed, a back surface can be extended by a filling surface and a footrest surface, and the back of the element can be used. The second surface constitutes a bed. The total length of the bed of the present invention is at least 78 leaves. 98 meters), and in some embodiments, the length is over 85 忖 (2. 16 meters). 15 Preferably, The backrest element is connected to the structure for selective movement between an upright position and a fully reclined position, The backrest element is swung backwards relative to the upright position. In some specific embodiments, One or more 4 movable 70 pieces can contain _ seat chassis, It is connected to the support structure so that it can pivot between the first and second positions relative to the branch structure, And when the configuration member pivots back 20 from the upright position to the fully reclined position, Used to gradually pivot the seat chassis from the first position to the second position. It was unexpectedly discovered that the plurality of passenger accommodation units of the present invention can be arranged in the business class part of an aircraft cabin, Without reducing the number of seats. Each-seat system defines an abstract vertical axis, Relative to normal use seat 17 593064 玖, The mode of the invention extends back and forth. It was found that if each passenger accommodation unit was configured in such a way that its abstract axis was paired with the vertical axis of the aircraft (3) The angle range is between 35 and 55 degrees, Then, the maximum number of passenger accommodating units of the present invention can be accommodated in an aircraft passenger inspection. 5 Therefore, According to another aspect of the invention, Provide a passenger vehicle, Especially an airplane, The seating system includes a plurality of seating units, Each bit unit is defined-the abstract longitudinal axis of the seat, And includes a standard structure for attaching the seating unit to the vehicle floor, A molded member or a member configured to form a seat including a seat chassis and a seat back; It is characterized in that the 10-seat table is configured to form a column to define an abstract vertical axis, The seating unit in the row is in a longitudinally offset relationship, Arranged side by side at an acute angle to the abstract row axis, Thus forming the back space of each seat, Each seating unit further includes shaped members or is configured to form a substantially flat bed, The main part of the bed is arranged in front of the 15-seat seat. The bed extends back into the space to stretch the flat bed. Preferably, the space behind each seat is generally triangular or trapezoidal. The acute angle is typically in the range of 30-60 degrees, Preferably it is 20.4-50 degrees, E.g, 40 degrees, μ degrees or 50 degrees. usually, The seating unit is installed in a cabin of the vehicle, The cabin defines an abstract cabin longitudinal axis. The abstract axis is generally parallel to the cabin axis, Or as a pair of acute angles. therefore, In an aircraft cabin, The seat unit of the present invention can be "herringbone, , Configuration. 18 593064 Rose, Description of the invention ▲ The seating unit can be arranged adjacent to one side wall of the vehicle and facing inward. ㈣, The cabin includes two opposite side walls, And a row of seat units are consecutively arranged or are adjacent to each side wall so that each seat faces the cabin, and an extended surface located behind the seat back is arranged adjacent to the side wall. The seat thus has its back to the carrier wall, Give the guest an overall uncrowded appearance. 々Cabin Workshop Valley § Noon ’can arrange seat units of _ or more additional rows towards the center of the passenger inspection. If the seat of the Central Bank of China II can be accommodated in any known passenger robbery, The seats in such rows are therefore preferably arranged substantially back-to-back. Each seat unit preferably further includes a footrest portion disposed in front of the seat 2. The foot part can thus be used by the seat erector, In a raised position during flight to support his or her feet, And / or be able to sit on the seat when another passenger visits the seat user. If the 15-chat part is configured, it is found that the passenger does not need to combine the seat unit with the movable legrest as a seat forming member of the part. In some specific examples, Each ^ / fr ® ^ -r ^ ^ may be further included forward. A first privacy divider, It is arranged in the footrest 20 that the seat forming member and the bed forming member may include one or more movable passenger support elements ’which are selectively configured to, Under the seat form, At least part of the passenger seat, Or, In bed support, For at least part of the flat bed, And a flat bed in the form of a bed pin, The system is advantageously arranged at substantially the same height as the seat chassis under the seat form. 19 593064 玖, Description of the invention The car seat's mother-seat unit includes a first fixed position in the space behind the seat, "Customer support elements, When it ’s time to move the element in the form of a bed, The first passenger support element is generally configured to be coplanar with the one or more movable elements, It is used to form the flat bed of this part. The first-passenger support frame may be generally triangular or trapezoidal. It should be noted that When the seat unit is configured as a bed, the passenger support TL system, Used only by passengers It is therefore possible to configure the seating unit so that the first passenger support element extends into a lateral recess formed by the side wall of the recessed cabin 10, It is used to maximize the use of space in the cabin. 15 Advantageously, Each seat unit further comprises a second passenger support element 'which is preferably fixed to the side of the seat, The second passenger support element is generally configured to be coplanar with the first-passenger support element, And when the movable element is assembled under the bed form, Used to form this part: The flat bed 'thus stretches the flat bed laterally. The second passenger support element may be substantially triangular or trapezoidal. The first fixed element of a seat unit is generally arranged to be continuous with the second fixed element of an adjacent seat unit 'and the first and second elements can be separated from each other by a second privacy barrier. The first and second elements are generally Takes up all the space behind the seat. The invention thus provides a seating system, It is particularly suitable for use in business class, one of the passenger aircraft. The seat system of the present invention provides Individual undercarriage and optional footrest, Used to allow passengers to rest their legs in an elevated position during the flight. Each seat unit is 20 20 593064 玖, DISCLOSURE OF THE INVENTION A self-contained component is provided for forming a substantially flat bed, And by arranging the flat bed behind the seat, it stretches back, Into a space formed by the arrangement of seating units, And can make full use of the space in the cabin. Surprisingly, It was found that according to the present invention, it is possible to provide flat beds up to 7 feet (2.13 meters) in business class 5 In general, the total number of passengers will not be sacrificed. Furthermore, The patent applicant has found that the seat unit of the present invention can be configured, Used to give the cabin a generally non-crowded appearance. The support structure may be any suitable, well-known person skilled in the art, Meet aviation standards, Made of lightweight materials, And can be equipped with solid components suitable for ίο σ, Used to secure the seat unit to a seat track in the cabin of an aircraft. Preferably, The support structure includes an armrest (pile price) or plinth for attachment to the seat. According to another perspective of this month, Provide a passenger vehicle seat module, The seat module includes a seat section, A foot rest, A single support b, , , . It is configured to support the seat portion and the footrest portion leaving the vehicle floor, and the attachment member is used to attach the support structure to a pair of seat tracks located in the floor of the vehicle; It is characterized in that the attachment member includes two spaced-apart trowels for fixing the support structure to one of the pair of rails at two spaced-apart points and a single third fixing portion for Will support, " Consolidate 疋 to another track ’so as to occupy the fixed between the seat module and the seat track, This configuration allows a plurality of the seat modules to be attached to a pair of seat tracks, one by one, Thus, a plurality of seat sheets are formed. A seat unit includes a seat portion of a module. And the footrest of another adjacent module. 21 593064 玖, Description of the invention It has been found that According to the present invention, a three-point fixing method is used between a single seat supporting structure and a pair of seat channels. Allow the pair of seat rails to form a greater degree of deflection, If, for example, when the fuselage is subjected to excessive stress, such as in the event of an emergency or crash 5 landlng, Moving relative to each other, This reduces the likelihood that the structure will disengage from the seat track at one or more fixed points under these conditions. According to another aspect of the invention, Provide a passenger vehicle, Especially the passenger ’s seat assembly for the aircraft, The assembly is used to provide passenger seats and sleeping facilities. The assembly includes: 0 — supporting structure, It is used to support the assembly off the vehicle floor; 70 seats, It includes a seat chassis element and a crime element 4 # element including first and second opposite sides, One of the sides has a first seating surface, And the other side has a substantially flat second bed surface; 15 20 or more auxiliary receiving elements, It is connected with the supporting structure or is composed of 疋. 卩刀之忒 support structure, And is configurable or expandable with, Hai seat side by side ’the or each auxiliary accommodating element has an auxiliary, A substantially flat passenger support surface; And it is used to connect the seat element to the support structure, a seat moving mechanism ’, the seat moving mechanism includes a seat changing sub-mechanism, It is used to accommodate the movement of the seat TL, so that the seat element can be selectively used in a seat form for providing a passenger seat, With the bed form used to provide passenger beds, The seat changer mechanism is used to control the movement of several crimes, So that the backrest element can be in the-upright position, 22 593064 玖, Description of the invention wherein the first seat surface of the backrest element cooperates with the seat chassis element for forming a seat, Pivot to-second tilted position, Among them, the surface of the second bed is generally arranged with a silk oramp; + _ 乂灵夕的， The auxiliary passenger support surface is coplanar or continuous. Used to form a bed. 5 Now, according to the present invention, Provide—a passenger seat assembly, It has a plurality of movable seat elements, Used to form a seat. The seat assembly can be converted into a bunk at the same time. The backrest element and one or more auxiliary 7L pieces constitute a passenger sleeping surface. The invention is characterized in that: The backrest element has a first surface specifically for use as a seating surface, 10 and the second opposing surface are specifically used as a sleeping surface. Preferably, The seat moving mechanism is used to control the seat chassis element and the provincial crime element to move in relation to each other. The seat changer mechanism can be used to control the movement of the backrest element, So that when the backrest element moves from the first position to the second position, The backrest element is shaken forward to cover the seat bottom 15 disc element, And the backrest element in the second inclined position overlaps and covers the seat chassis element. Advantageously, So in bed form, The bed surface of the seat chassis element and the first seat surface of the backrest element are not part of the surface. Therefore, the seat can be cushioned with a material which is particularly suitable for the seat. Similarly, In seat form, Do not use a second backrest surface to form a 20-seat seat, The bed surface system can therefore be particularly adapted to be used as a bed for padding. Furthermore, In the form of seats and beds, The materials used to place the cushions on the seat elements can be different colors ’and / or have different textures, And / or different patterns, When all or most of the passenger assemblies of the present invention are assembled into one of these ways, Risi 23 593064 玖, Invention Description 俾 will produce _ 第 —Atmosphere or _ in the cabin of the aircraft, , Situation, , , And when all or most of these passenger assemblies are assembled in that other way, Produces a second different atmosphere or a "scenario, , . The surface of the backing element can bear-a foamed congestion layer with a first surface that conforms to the contour, It is used to form the backrest of the seat of the moon Λ or guillotine, And the other surface may carry a foamed cushion layer having a substantially flat second surface, It is used to form part of the bed. The seat changing sub-mechanism can be used to control the movement of the seat chassis element ’so that when the backrest element moves from the _ upright position to the second inclined position 10, The seat chassis element is induced to move downward relative to the support structure. therefore, The bed surface of the seat assembly can be arranged at a relatively low height from the vehicle floor. It is easy for passengers to climb to and from the bed. Preferably, Equipped with a suitable motor unit for automatically moving the backrest element between upright and tilted positions, And a control device which can be operated by the user is provided for controlling the operation of the motor device. 忒 The seat moving mechanism preferably further includes a seat reclining sub mechanism, It is used to allow the seat to be selectively reclined from an upright position to a fully reclined position, The seat reclining mechanism is used to control the movement of the backrest element, So that when the seat is reclined from the upright position to the fully reclined position, The 20 backrest element is rocked backwards from the first upright position to a fully reclined position. The seat reclining mechanism can advantageously be further used to control the movement of the seat chassis elements, So that when the backrest element is swung backwards from the first upright position to the third fully reclined position, This causes the seat chassis element to tilt backwards. therefore, In the fully reclined position, Backrest element and seat bottom 24 593064 玖, SUMMARY OF THE INVENTION The disc elements can be individually oriented to provide an ergonomically comfortable seating position for passengers using the seat assembly. The reclining motion of the backrest element and the tilting motion of the seat chassis element can be motorized under the control of a user-operable control device. 5 Preferably, One or more of the auxiliary accommodating elements are disposed or expandably disposed elsewhere or behind the seat. In some specific embodiments, One or more of the auxiliary receiving elements may include a footrest, Is deployed or expandable in front of the seat, And in this second position, The surface of the second bed that carries the sin component is generally arranged to be coplanar with the footrest portion 10 and continuous. -Or more of the auxiliary element may include a fixed extended back surface, Placed behind the seat. In some specific embodiments, The seat assembly may further include-removable filling elements, And the seat changer mechanism can be used to allow the filling element to Storage location and-rise 15, Move between expandable positions, Wherein the filling element extends in the second inclined position and is substantially coplanar and continuous with the second surface of the backrest element, And the back extension surface, Thus forming a substantially flat, Stretched bed surface. The seat changing sub-mechanism can be further used to control the filling element 2. 2 moves, So that when the backrest element is moved from the first upright position to the inclined position, The filling element is induced to move from the storage position to the unfolded position. The filling element system, It is pivotally connected to the lower end of the backrest element so that when the backrest element system is moved from the first position to the second position, the 70-pack system is moved from the storage position to the deployed position. The seat conversion sub-mechanism may include a seat support mechanism, It is towed 25 593064 玖, Description of the invention For rocking between a first seating position and a second bed position. The backrest element can be mounted on a supporting device, So that the backrest element can be shaken from the first position to the second position, And can pivot from the first upright position to the second tilted position, And 5 can be provided with detachable fixing means for selectively fixing the supporting means in the first and second positions. In some specific embodiments, The seat support device may include two opposing swing plates. The shaking plates can be interconnected by one or more torsion tubes. The seat chassis element is pivotally mounted on a support device, This arrangement is such that when the support system is shaken from the first position to the second position, The seat chassis element is moved downward from an upper unfolded position to a lower storage position, And the backrest element is shaken forward to cover the seat chassis element, So that in the second tilted position, The backrest element covers the seat chassis element. The seat chassis element may include a front end portion and a rear end portion relative to the backrest, And the seat chassis element can be pivoted to the supporting device at the rear end portion or toward the rear end portion. Conveniently, The seat moving mechanism further includes a seat chassis support. Used to support the front end of the seat chassis element. The seat chassis support device may include a-slide, It is arranged under the seat chassis element π, -The foot member has two opposite ends, Among them, the end portion can be thumb-connected to the front end portion of the seat chassis element and the other end portion can slidably engage in the slideway, And-the tow leg is connected to the other end of the foot member to the support device, This configuration is such that when the supporting mechanism is shaken from the first position to the second position, Move the tow pillar to induce or allow the other 26 玖, Description of the invention W slides in the slide, The slide is shaped so that when the support moves from the first position to the second position, The feet are moving down, This causes or allows the front end of the seat chassis element to move progressively downward. The foot structure can be pivoted to the slideway at the end of the material to the end of the recording bottom m. On—this and ... " In other specific embodiments, The front of the seat chassis can be cut by two pieces, Each piece is slidably sprayed into and out of the individual slideways, side by side with individual seats. 10 Preferably, The seat moving mechanism further includes a seat shuttle mechanism. When the supporting device is disposed in the first seat position, It is used to allow the seat element to selectively move between an upright position and a fully reclined position. The seat reclining mechanism includes a curvilinear way, It is attached to the support and the discrepancy is formed in the support device, And having two opposite track ends 1 and spaced track followers attached to the backrest element, 15 The follower follower is used to merge and slide along the track teeth, Assemble the channel so that the channel follower slides from the end to the other end along the track, The backrest element is gradually and backwardly shaken from the first upright position to a third fully reclined position " The rear seat mechanism of the seat can further include a two-way transmission device capable of selective operation. It is used for translationally moving the backrest element relative to the support, This configuration causes the transmission device to act to slide the track follower to the curved track, As a result, the backrest element is gradually shaken between the first and third positions. Advantageously, The transmission device may include a linear actuator connected between the flats which are backed by Yuanrenhai Branch. E.g, Such as a linear screw (linear 27 593064 玖, Description of the invention A linear actuator rew) or a ball screw, It can stop at any intermediate position between the first and second positions, Thus allowing 7L pieces of Moon Sin to continuously lean back between the first and third positions, It can be stopped at any desired intermediate position. 5 In some specific embodiments, The linear actuator may include a linear screw or a ball screw fixedly secured to the supporting device, A screw engaging device is pivotally connected to the backrest element and a bidirectional motor with a selective surface carried by the supporting device, Used to drive the linear or ball screw in rotation. The seat chassis element may have a front end portion and a rear end portion relative to the backrest element, And the linear actuator is pivotally connected between the supporting device and the seat element, The linear actuator is attached to the seat chassis element at the rear end portion or toward the rear end portion, For progressively driving down the seat chassis element relative to the support structure, From a first upper position when the backrest element is in the first upright position to a second lower position when the backrest element is in the third fully reclined position B, And the seat moving mechanism can further include a seat chassis support device, Used when the rear end of the seat chassis element is driven down again, Support the front end of the seat chassis element, This causes the seat chassis to gradually tilt back when the backrest element is swung backwards. therefore, In an upright position, The backrest element can be generally upright, And the 20-position chassis can be arranged horizontally. In a fully reclined position, The moon Λ element is shaken backward relative to the upright position, And the seat chassis element is tilted rearward relative to the upright position to form a comfortable reclining seat position. Preferably, The shape of the curve, Length and position of linear actuator 28 593064 bumps between the linear actuator and the backrest element and the seat chassis element Description of the invention And the form of seat chassis support, Causing the seat to gradually recline from the upright position to the fully reclined position, It moves through a series of reservations, Ergonomically comfortable seating position. In the middle of the predetermined position, The shape of the curve orbit can be determined by interpolation. 5 In some specific embodiments, In order to allow the backrest element and the seat chassis element to adopt the aforementioned ergonomically comfortable position, The linear actuator can be connected to the backrest element via a lost motion device, The capacity σ is relatively laterally shifted between the seat chassis element and the backrest element to a small extent. The seat change sub-mechanism may include a selectively actuable bidirectional actuator. It is used for fixing the supporting device between the first seating position and the second bed position. The actuator may include a four-bar double-rocker linkage, The connecting rod set includes a rocker and a connecting rod connected between the supporting device and the rocker. And a bidirectional rotary transmission with optional operation, For actuating the joystick, The 15 configuration causes the rocker to actuate to cause the support device to rock between the first and second positions. The rotary transmission device may include a motor, A worm gear and a worm wheel, The worm wheel (womm wkd) is firmly fixed to the rocker. A worm gear / worm wheel device is a non-reversible device. Therefore advantageously, Example 20 In the case of an overweight passenger sitting violently in the seat, The excessive force on the supporting device is not transmitted to the motor via the worm gear / worm wheel device. Furthermore, The rotary transmission is fixed in the first and second positions. However, in order to allow the support device to be manually adjusted to the first 29 593064 when needed, Description of the invention E.g, When the motor or electric power is faulty in the aircraft passenger ’s worm gear (WGnn gear), it can be removed from the pot wheel. The actuator can be attached to the branch structure of the seat assembly, It's under the seat 5 pieces. The support device may include two spaced apart side members, They are arranged on opposite sides of the back-to-back element, respectively. The connector connecting rod system can be connected with the side member, It is located below the planting point between the support device and the support structure. therefore, The present invention provides a vehicle, Especially an airplane, Passenger seat 10 assembly, One of the backrest elements is mounted on a supporting structure, So that for the comfort of the passengers, reclining backwards from the upright position to the reclining position, It can pivot forward to a generally horizontal tilted position covering the top of a seat chassis element. One of the first surface of the seat chassis element and the backrest element is mounted so that it is suitable as a seat. however, The second reverse surface of the backrest element 15 is used as a bedding surface. Seats can include one, And preferably two, The fixed or expandable auxiliary extension surface is located behind and / or in front of the seat ’and the backrest element is pivotally connected to the support structure, So that when pivoted to the second tilted position, It is in contact with one of the extended surfaces, Used to form a substantially continuous surface with it. Can be equipped with a removable filling 20 filling pieces, Used to fill the space provided between the backrest element and another extended surface. The seat assembly of the present invention can thus be converted from a seat to a bed, It can even accommodate tall passengers. Advantageously, The seat assembly of the present invention can be drawn at an angle between -35 degrees and 55 degrees relative to the longitudinal direction of the aircraft cabin, It is preferably 40 to 50 degrees, So that the position 30 593064 玖, Description of the invention An extended surface behind the backrest element extends into a recess formed by a typical recessed interior wall of an aircraft cabin. Although the cabin area juxtaposed with the recessed cabin wall is not suitable, And the headroom is insufficient, To accommodate the backrest element in an upright position, But it can be used in accordance with the present invention to accommodate the back extension surface, In bed form, Forms the surface of the bed. Extended surface, The filling element and the second surface of the backing element, Preferably, a cushion made of foam padding or any equivalent material particularly suitable for use as a bed is fitted. therefore, The bed surface of the seat assembly of the present invention may have a substantially flat surface, It is roughly 10 levels when unfolded. It can be further known that When the seat assembly is configured as a seat, Stand back against the element, The back extension surface located behind the seat is generally concealed and forms a useful storage space. Conveniently, This storage space can be used to store 15 bedding materials required only when the seat assembly is converted into a bedding form. E.g, The storage space formed by the back extension surface located behind the backrest element f is 1, It can be used to store a duvet and / or-a blanket and-or more pillows. Advantageously, Such bedding materials are concealed when the seat assembly is in the seat form, Bring the cabin _ overall neat appearance. When the seat assembly is converted into a bed, The back element is rocked forward, covering the top of the seat chassis element, To expose the back extension surface, And allows easy access to bedding material stored on the extended surface of the back, Its department: Enough to spread manually on the surface of the bed. ’'According to another aspect of the present invention, Describes the fact that it is a special tie, For example, the reclining seat assembly used on the carrier of the aircraft ’includes a fixed support 31 593064 玖, Description of the invention Floor 4 knife 'is used to support the floor assembly of the vehicle, A reclining seat section, It includes a seat chassis and a backrest 'and a seat connection device for connecting the seat part with the support part, The connecting device includes a seat reclining mechanism for allowing and controlling the movement of the seat portion between a first upright position and a first fully reclined position, And optionally, At first glance, the two-way motor device, Used to drive the seat part in the first and second positions; The seat reclining mechanism includes an irreversible linear actuator connected between the motor device and the seat portion. 4 An irreversible linear actuator system may include a lead screw drive or 10 a ball screw drive, Or any other equivalent, Irreversible device. Between the first upright position and the second fully reclined position, Using this irreversible actuator for driving the seat part, The advantage is that Excessive force in the seat knife or sudden force i is not transmitted to the motor 15 so that the risk of damage to the motor is low, And consequently prolong its life. For example, a passenger who is too heavy suddenly sits in his or her seat: Therefore, a sudden, Strong power, This strong force is not transmitted to the motor device via an irreversible linear actuator. Linear actuators can include-linear or ball screws, Attached to the 20 support part and one of the seat parts (or part of the connection), And the -screw coupling device is attached to the seat part and the other-part (or-part connection) of the support part. In some specific embodiments, Linear actuator can be connected to the seat chassis, Used along the part relative to the branch, A predetermined linear path between -the first position and -the second position, Drive the seat chassis. 32 593064 玖, SUMMARY OF THE INVENTION The seat chassis may have a front end portion and a rear end portion relative to the backrest, And the linear actuator can be turned to the seat chassis at or towards the rear end, It is configurable to drive the rear end of the seat chassis downward when it is moved from the first position to the second position. The seat reclining mechanism can be 5 steps-step i also includes-support equipment f, When the rear end of the seat chassis is driven down, Used to support the front end of the seat chassis, Thus, when the backrest is swung backward, the seat chassis is tilted backward. Linearly actuated descent can be connected to the backrest alternately or It is used to translate the backrest 10 in translation between a first upright position and a second recline position. The seat reclining mechanism may further include a guiding device, When the backrest system moves from the first upright position to the second fully reclined position, For rocking the backrest gradually backwards relative to the support portion. The guidance system may include a curved path, It is attached to the support part or a part is connected to the support part, And plural followers separated, It is attached to the backrest, The 15-track follower is used to engage and slide along the track. Advantageously, The linear actuator is pivotable to the seat chassis, And can be pivoted to the backrest via an invalid motion device, To allow relative pivoting and translational movement between the seat chassis and the backrest, To allow for freedom of movement between the backrest and the seat chassis, So that these seating elements can use a plurality of 20 relative, Scheduled, Ergonomically comfortable location. In another aspect of the invention, To provide a seat with a reclining back, The seat includes a fixed support section, It is used to support the seat off the floor, A seat part includes a reclining backrest and a seat connection member, It is used to connect the seat part with the support part, 33 593064 Rose, Description of the invention 5 10 15 The money receiving member includes a back-to-back mechanism, It is used to allow and control the movement of the back-to-back between a first upright position and a second fully reclined position; Wherein the backrest includes a first lower backrest member having an upper end portion, And — j Last month ’s sin component ’is placed on the backrest component, And tied at the upper end or pivoted towards the upper end, 俾 It is convenient for the translational movement of the transmission, And the back-to-back mechanism includes first and second extension guides attached to the support portion or a part connected to the support portion, The first track has two opposite track ends, The plurality of first spaced-apart articulated driven members are attached to the first backrest member and used for the first track order, Merge sliding ’and a second orbit coupling member, It is attached to or is partially connected to the backrest member, And used to slump and slide in the second orbit, the first orbit is curved, So that when the first orbit coupling member is slid along the first track from the end to the other end, Causing the backrest member to swing progressively relative to the wing portion between the first upright position and the second fully reclined position, And the shape of the second track causes that when the second track coupling driven member system is affected to slide along the second track, The second backrest member is caused to gradually shake in relation to the first backrest member. 20 This advantage may also have different relative configurations with the lower backrest member in the upright and fully reclined positions. Furthermore, The relative arrangement of the upper and lower backrest members can be continuously adjusted between the upright position and the full recline position. Preferably, In the first upright position, The components of the people above and below are generally coplanar. Used to construct-a generally flat back-to-surface. In the second fully reclined position, 上 ik 下北土 " , , The sin component next month can be a pair of obtuse angles, So the next 34 593064 玖, Description of the Invention The Crescent member is inclined from an upright position at a larger angle than the upper backrest member. Therefore, the lower back reading system can constitute a lumbar vertebra support part for seat passengers. / The back-to-back mechanism can include a 5-shaft talent with two arms that are pair-pure angles, The rocker is dragged to the first backrest member at a position in the middle of the two arms, One of the arms carries the second track-end driven member, And a connecting rod with two opposite ends, One of the ends is pivoted to the other arm of the pure rod, And the other end is fixedly secured to the second backrest member; # This configuration causes when the second driven member system is affected to slide along the second track 10 ’the rocker system is affected and its peak is shaken to the first backrest member, This caused the link to pivot about its pivot to the other arm of the rocker, As a result, the pivot of the second backrest member is pivoted to the first backrest member. The recumbent reclining mechanism may further include a member for restricting movement of the rocker and / or link. 15 The seat connecting member may further include a bidirectional wire 14 actuator which can be selectively operated, It is connected to the supporting part or a part connected to the supporting part and the backrest, For moving the backrest in translation relative to the support part, This configuration causes when the backrest is induced to move translationally relative to the support portion, The first driven member located on the first backrest member is guided to move gradually along the first track, As a result, the backrest is gradually shaken between the first upright position and the second fully reclined position. . The seat section generally includes a seat chassis. The linear actuator can be connected to the seat chassis, It is used to move the seat chassis from a first position to a second position along a predetermined linear path. The linear actuator can pivot 35 593064 玖, Description of the invention To the seat chassis. Advantageously, The linear actuator is pivotally coupled to the backrest by an inactive motion device. The following is a description made by way of example only with reference to accompanying drawings of specific embodiments of the present invention. 5 Schematic description Figure 1 is a cross section of a front part of an aircraft fuselage, A schematic plan view 'shows a seat system including a plurality of individual seat units according to the present invention. 1〇帛 1A is an enlarged view of a part of FIG. 1, Three adjacent seating units are shown. Series 0 is an isometric view of the adjacent seat unit in Figure 2A. ; In Figure 2, One of the seating units is shown as an upright seat, Another-shown in the reclining seat form, And the third one is shown as a bunk-shaped 15 style. Figure 2A shows a part of a supporting structure of an individual seating unit of the type shown in Figure 2, Where the movable seat element is removed. Figure 3 is a schematic side view of a first passenger seat assembly for a vehicle according to the present invention, The system shows an upright seat form. 〇 Figure 4 is another schematic side view of the first passenger seat assembly of Figure 3, The system shows a fully reclined seat form. , Fig. 5 is another schematic side view of the first seat assembly of Figs. 3 and 4, The department shows a bunk form. Figure 6 shows the 3rd to 5th figures in the upright seat form—seat 36 593064 玖, Description of the invention An isometric view of a part of an assembly, The seat cushion was removed. Figure 6A is a side view of a criminal component of the seat assembly in Figure 6 of the component. Figure 6B is a _ # angle view of the backrest element from the second figure. 5 Figure 7 is the other-isometric view 'of the part shown in Figure 6-where the seat assembly is in the fully reclined seat form. Fig. 8 is another isometric view of the first seat assembly of parts of Figs. 6 and 7, The seat assembly is in the form of a bed. Fig. 9 is an isometric view of the seat-moving mechanism of the seat-assembly 10 of the parts of Figs. 3 to 8; Fig. 10 is a side view of the seat moving mechanism of the part of Fig. 9 ', which shows a seat form. Figure U is another side view of the seat moving mechanism of the parts of Figures 9 and 10, It is shown in the form of a bed. Figure 5 帛 12 is an enlarged isometric view of the seat moving mechanism in the parts of Figures 9 to 11. Fig. 13 is an isometric view of the seat back mechanism of the seat assembly part of Figs. 3 to 8. 20 Figure Η is an isometric view of the seat change sub-mechanism of the part of the first seat assembly in Figures 3 to 8 ', which shows the form of a bed. Fig. 15 is another isometric view of the seat changing sub-mechanism of the part of Fig. 14, It is shown in the form of a seat that moves a worm (w_sc called from-the corresponding worm gear (_m gear), Used to allow the seat change sub-mechanism to be manually moved between the seat and the bed form. 37 593064 玖, Description of the Invention Figure 16 is the seat change sub-mechanism of the parts of Figures 14 and 15-enlarged, Section side view. Figure 17 is a cross-section of another seat system of the present invention, A rough plan view. 5 帛 18 is an isometric view of the passenger accommodation unit of the present invention. Shown here is a seat. Figure 19 is an isometric view of the passenger accommodation unit of Figure 18, It is shown in the form of a bed. Figures 20A-20C are schematic side views showing the passenger accommodation units of Figures 18 and 19 switching between bed 10 and seat format. Figure 21A is a schematic diagram of the passenger accommodation unit of Figures 18 and 19, Isometric view, Shows a passenger using a seat in a seat format. Figure 21B is a schematic view of the passenger accommodation unit of Figures 18 and 19, Isometric view, Shows a passenger using a seat under a bed. 15 FIG. 22 is an isometric view of another accommodating unit of the present invention. It is shown in the form of a seat. Figure 23 is an isometric view of the passenger accommodation unit of Figure 22, It is shown in the form of a bed. Figure 24A is a schematic diagram of the passenger accommodation unit of Figures 22 and 23, 20 isometric view, Shows a passenger using a seat in a seat format. Figure 24B is a schematic diagram of the passenger accommodation unit of Figures 22 and 23, Isometric view, Shows a passenger using a seat under a bed. Figure 25 is an isometric view of a variation of the passenger accommodation unit of Figures 22 and 23, It includes a sliding seat chassis. 38 593064 玖, DESCRIPTION OF THE INVENTION Figures 26A-26C are side views schematically showing different positions of the sliding seat chassis. Figure 27 is an isometric view of another variation of the passenger accommodation unit of Figures 22 and 23. 5 Figure 28 is an outline of the upper and lower decks of a front part of an aircraft fuselage. Sectional plan view, It is shown that another seat system of the present invention is applied on a Boeing 747-400⑧ aircraft and main deck. Figure 29A is a schematic side view of a second passenger seat assembly according to the present invention, The seat assembly shown is in the dining position. Figure 29B is a schematic side view of the second passenger seat assembly of Figure 29A. It is shown in an intermediate recline position. Figure 29C is a schematic side view of the second passenger seat assembly of Figures 29A and 29B. The illustration is in a fully reclined position. Figure 30A is a schematic side view of the second passenger seat assembly of Figures 29A to 29C. The system shown here is in another intermediate switching position. Figure 30B is a schematic side view of the seat assembly in Figures 29A to 29C and Figure 30A. The illustration is in the form of a bed. Figure 31 is a schematic plan view of another seat system including a plurality of passenger assemblies of the present invention. 20 Figure 32 is a schematic plan view of another seat system including a plurality of passenger seat assemblies of the present invention. Fig. 33A is a schematic side view of the third passenger seat of the present invention. The seat assembly shown therein is in the form of a seat. Figure 33B is a schematic side view of the third seat assembly of Figure 33 A 39 593064 玖, Description of the invention The system is shown in an intermediate position. Figure 33C is a schematic front view of the third assembly of Figures 33A and 33B. It is shown in the form of a bunk. L 实施方式; L implementation; 3 5 Detailed description of the preferred embodiment A passenger aircraft generally includes a hollow, a front end and a rear end. Spindle-shaped body. In an example shown in the i-th accompanying figure, A front end portion 12 of a typical aircraft fuselage 10 is arranged toward the front end portion 11. The fuselage 10 is between a front end portion and a rear end portion, The system 10 defines a longitudinal axis of an aircraft as shown by a chain point line A-A in FIG. And the fuselage 10 is pushed toward the front end 11, Used to form a nose portion 15. The fuselage 10 accommodates various features and facilities of the aircraft, Including one or more passenger cabins20, twenty one. Passenger cabins 20, With its number and size, It depends on the space in the fuselage available for the passenger cabin and the form required for the passenger cabin. The present invention is not limited to use in any particular shape, Size or number of cabins. however, In Figure 丨, Is only an example, As shown in the figure two cabins 20, The 21 series is located in the front 12 of the fuselage. A first cabin 20 is located in the nose portion 15 of the aircraft, And a second cabin 21 is arranged behind the first cabin 20, A common area 22 is equipped with 20 in two cabins 20, Between 21. As the first! As shown in the figure, The common area 22 may include a kitchen 23 and one or more passenger toilets 24. As shown in Figure 1, An aircraft cabin 20, 21 is generally composed of two opposite surface portions 26 of the inner surface of the fuselage 10, 28 formed. Actually, ^ Opposite surface portion 26, 28 constitutes a cabin 20, 21 的 opposite sidewalls. On machine 40 593064 玖, Description of the invention 21 also includes a floor or deck 30, It is supported by a suitable infrastructure (not shown), And a ceiling (not shown) extends above the floor 30 between the opposing side walls. The opposite side walls 2 6, 2 8 pass ΐ 乂 plural prefabricated, Synthetic panels are lined to give the cabin an attractive 5 / main purpose look, And in the cabin 20, 21 provides thermal insulation between the exterior of the aircraft. The basic structure of the fuselage embedded in the floor 30, It includes plural types of seats on the seat widely known to those skilled in the art 32, 34, This is shown by the dotted line in Figure 1. Each pair of doctrines is generally linear, 10 and includes a pair of substantially parallel tracks, It is used to securely secure multiple seats or other devices to the aircraft's infrastructure. In general, An aircraft cabin 20, 21 including the second foreign seat 32, Each track system is configured with two opposite cabin side walls 26, One of 28 individual side walls is adjacent. If space permits, One cabin 20, 21 may also include one or more central 15 pairs of seats 34, It is arranged in the middle of the outside seat seat 32. As shown in Figure 1, The first cabin 20 includes a single central pair of seat tracks 34 'while the second cabin 21 includes two juxtaposed central pair of seat tracks 34'. Typically, A central pair of seat lanes 34 extends generally parallel to the longitudinal axis A of the aircraft. In the cabin of an aircraft, 21 is arranged toward the center of one of the fuselage 20 minutes, And before leaving the aircraft at the end and rear end, E.g, Such as the side wall 21 of the first passenger ship 21 in the i-th figure 21, 2 8 extends substantially parallel to the longitudinal axis A-A of the aircraft, And the outer seat rail 32 follows the side wall 26, 28 straight Therefore, at the same time, it extends substantially parallel to the longitudinal axis A-A of the aircraft. however, Towards the nose part 15, The opposite side wall 26, 28 41 593064 玖, The invention is arched and converges toward the front end portion 11. therefore, Under these conditions, Outer facing seats 32 are associated with the aircraft's longitudinal axis A-A at a pair of acute angles. 20 per cabin 21 accommodates a plurality of seat units 40. As shown in Figure 1, Located in each cabin 20, 21, The seating unit 40 is configured to construct 5 into a plurality of seating units 29. As detailed below. Each row 29 is fixedly secured to the individual pair of seat tracks 32, 34, And extend substantially parallel to it 'and define an abstract line axis as shown by line B-B in FIG. As shown in Figure 1, The first cabin 20 includes a second row of seating units 40, Each row 29 is fixedly fixed to 10 of the other opposite seat lanes 32 and one other lane. The outer facing seat track 29 in the first cabin 20 is inclined in relation to the longitudinal axis A-A of the aircraft, Abstract row axis B-B of seat units 40 in each row of 29 in the first cabin, At the same time, it forms an acute angle with the longitudinal axis a-A of the aircraft. The second cabin 21 includes a seat unit 40 of the second layman 29, And a central bank seat unit 40 next to each other. Each layman 2 9 is a detached lane with 15 mounted to the outside seat 32. And each central bank 29 is attached to a different track of the central counter seat 34. As mentioned above, The center-to-seat channel 34 extends substantially parallel to the longitudinal axis A_A of the aircraft, The seat unit 40 of each central bank 29 therefore extends substantially parallel to the aircraft longitudinal axis A-A at substantially the same time. In the second cabin 21, The 20-bit orbit 32 of each outer pair extends substantially parallel to the longitudinal axis A-A of the aircraft at the same time, Each layman 29 of the second passenger cabin 21 therefore extends substantially parallel to the aircraft axis a_a. Figures 1A and 2 show three adjacent seating units 40 in a row of Figure 丨 of the constituent parts. Each seat unit 40 includes a support structure 42 for placing 42 593064 玖, DESCRIPTION OF THE INVENTION The seat soap is attached to the floor 30. The support structure 42 can be made in any suitable manner known to those skilled in the art, But preferably includes a load-bearing, Aerospace grade steel sub-frame (not shown), It is covered with one or more synthetic panels suitably made in shape. Each seat unit 40 has a front end 51, A rear end portion 52 and two opposite side edges 53, 54. Support structure 42 juxtaposed with rear end portion 52, It includes a seat shell 43, As shown in Figure 2A, It generally forms a cubic recess 44. Behind the recess 44, The support structure 42 forms a first, A generally flat and generally dihedral surface 47, When the seat unit 40 is installed in a passenger cabin 20, 21 at 10, It is generally parallel to the cabin 20, 21 the floor 30 extends, But slightly tilted, As detailed below. A support structure 42 juxtaposed with one of the first side 53 of the seating unit 40, It forms a generally flat and generally triangular surface 48, It is substantially coplanar with the first surface 47, And in some specific embodiments, As shown in Figures 2 and 2A, It is substantially continuous with the first surface 47. The first and second surfaces 47, 48 is strong enough to support at least part of the weight of a passenger. The second surface 48 has a first concave lateral edge 45, It extends from one front end portion of the seat shell 43 outwardly and rearwardly to an intermediate point 46 between the front end portion of the shell 43 and the rear end portion 52 of the seat unit 40. The first and second surfaces 47, 48 forms a second lateral edge 49 which is substantially linear on 20, It extends rearwardly and inwardly from this point 46 to the rear end portion 52 of the seating unit. The first and second surfaces 47, 48 thus extends to the rear and one of the sides of the cube recess 44, An upper portion of the recessed portion 44 is formed. The first and second surfaces 47, 48 is supported by the support structure 21 at a predetermined height. 43 593064 玖, Description of the invention Located at the second side 54 of the seat unit 40, The seat shell 43 includes an upright arched partition 60, It has a rear portion with a convex surface, the rear end portion 52 of the seat unit 40 extending to the cube recess, the rear end portion, And a substantially linear portion 62 which extends between the front and rear ends of the recess 44. The rear convex portion 61 has a curvature ′ in a plan view as shown in FIG. 1A, which corresponds to the curvature of the first concave lateral edge 45 of the second surface 48. The partition 60 extends substantially above the first and second surfaces fa, And use as ί, Privacy partitions for passengers using seat unit 40, Surrounding the rear end portion 52 and the second side edge 54 of the seat unit 40. 1〇 #Seat unit 4G front end 51 side by side support structure 42, It includes a soft ottoman extending upward from the floor 30, It has a substantially flat upper surface 66. The upper surface 66 is used to carry a seat cushion 67, Its thickness causes the seat pan 67 to be configured substantially to the first and second surfaces 47, /, Plane " The Hai cushion no 65 series is strong enough to support the weight of a passenger 15 ’ The seat cushion 67 can be used as an auxiliary seat. The support ... structure 42 further includes a relatively small, Auxiliary privacy partition 68, The front end portion 51 of the seat unit 40 is circled. The side cube recess 44 receives a plurality of movable passenger support elements, This is done by a seat movement mechanism which will be explained in more detail below, It is connected to the branch structure 20. The movable passenger support element includes a seat chassis 71 and a backrest 72. The seat movement mechanism allows the passenger support element to be selectively assembled, To provide a passenger seat, The center and right-hand side seating units 40 shown in Figure 2, Or, make a bed on the left-hand side as shown in Figure 2. In seat form, Movable passenger support element ", 72 series can 44 593064 玖, Description of the invention It is optionally in an upright or dining position as shown in the seat unit 40 on the right-hand side of FIG. 2, And it moves between a reclining or reclining position as shown in the center seat unit 40 in FIG. 2. The movable passenger support element 71, 72 is connected to the branch structure 42 via the seat moving mechanism with 5 waves. In seat form, The seat chassis 7 is housed in a cube recess 44 of the housing 43, And the backrest 72 extends upward from the recess 44 to the rear of the seat chassis 71, And on the first and second sides 53 of the seat unit 40, 54 extends laterally. therefore, As perceived by a passenger using a seating unit, The seating unit 40 defines an abstract longitudinal axis of the seat, It is 10 before the seat unit 40 and the rear portion 51, Extending between 52, This is shown by the dashed lines C-C in Figure 1A. In a fully upright position, The seat chassis 71 is generally arranged with the first surface 47 and the first surface 47, 48 at the same height, And separated from the back of the soft palate 65, So that the seat cushion 67 provides a footrest portion for the passenger 15 using one of the seat unit buckles. In the back position, The backrest 72 leans back relative to its position in the upright position, And the seat chassis 71 is tilted slightly backward, To provide an ergonomically comfortable reclining seating position. Furthermore, In the leaning position, The seat cushion 67 of the upholstered stool 65 serves as a footrest for passengers. The backrest 72 includes a front surface 73 and a rear surface 74. In the upright and back positions, The backrest front surface 73 cooperates with the seat chassis 71, Used to form passenger seats. In the form of beds, As shown on the left hand side of Figure 2 The backrest is swung forward relative to the seat unit, And partly trough in the cube recess 44, So that the surface 74 after the back 72 is substantially 45 玖, Description of the invention With first and second surfaces 47, 48 coplanar, It is coplanar with the cushion 67 of the upholstered stool 65. In bed form, The surface 74 behind the backrest 72 is substantially continuous with the second surface 48 and the cushion 67 at the same time. The seat moving mechanism includes a movable filling element 76, As shown in Figure ία, When the seat is converted from a seat to a bed, It is moved from a storage position to an unfolded position. In the form of beds, The filling element 76 is arranged in the middle position, And it is substantially coplanar with the surface 74 behind the backrest 72 and the first surface 47 and is continuous. In the form of beds, The seat unit 40 thus provides a passenger extended bed surface, The bed surface extends behind the seat by a first surface 47, With the second surface 48 extending laterally from the seat, It extends in front of the seat by the cushion 67 of the upholstered stool 65. Related to Figures 1 and 1A, The seat units 40 in each row 29 are attached to individual pairs of seat tracks 32, 34, So that the abstract seat vertical axis c_c of each seat unit 40 forms a pair of acute angles with the abstract row vertical axis b-b, 15, The seat units 40 are arranged side by side offset from each other in the longitudinal direction. So that each seat unit 40 is at each seat 71, Behind 72, a substantially triangular or trapezoidal space 36 is formed. This seat unit 40 is arranged in row 29, So that the convex portion 61 of the privacy partition 60 of the seat unit 40, In general, it abuts continuously on the first concave lateral edge of another adjacent seating unit 40. 〇 As clearly shown in Figure 1A, Seat 71 per seat unit 40, After 72 square space 36, It is therefore occupied by the first surface 47 of a seat and the second surface 48 of another adjacent seat, The first and second surfaces 47 of the one and the other seating unit 40, The 48 series are separated from each other by a privacy partition 60 of a seat unit 40. So use 71 in each seat Space behind 46 593064 玖, Invention Description 36, Used to place seats 71, 72 extends back into the space 36, While extending the bed surface provided by the seating unit 40, 7 4. 7 6 length. An acute angle formed by the seating units 40 in a row 29, The system is oriented relative to the abstract line axis B-B depending on the required passenger configuration. however, Typically, The acute angle between the abstract seat axis c_c and the row axis B_B of each seat unit 40 is in the range of 30 degrees to 60 degrees. And preferably it is 40 degrees to 50 degrees, As shown in Figure 1, For example, about 40 degrees. The orientation of the seat unit 40 may be related to the cabin 20, 21 while facing inward or outward. In the first cabin 10 20 in Figure i, What you can see is that Each layman 29 is configured with opposite side walls 26, One of the individual side walls of 28 is adjacent, And in each row of the 29 seats where the 40 series face inward. The second lateral edge 49 of the seating unit 40 in each row 29 is substantially coplanar, To form an extended outer edge, It extends to the side walls 26 of the cabin 20, 28 tied. Due to the side walls 15 26 in the first cabin 20 Curvature of 28, So on the lay edge and each side wall 26, 28 has a J gap of 27 ' and the gap 27 is typically filled with a suitable filling panel of a type well known to those skilled in the art. In the second cabin 21, The seat unit 40 of each layman 29 is facing inward and forward with respect to the passenger 21. As can be seen in Figure 1, When the side wall 26 of the second passenger 20 cabin 21, 28 and side walls 26 of the first cabin 20, 28 is less curved than the second edge 49 of the seating unit 40 and the position in the first cabin 20 is closer to the side wall 26, 28, Therefore, on the outside edge of the seat and the opposite side wall 26, There is no or substantially no gap between 28. The second cabin 21 bis seat unit 40 of the central bank 29 is also 47 593064 玖, DESCRIPTION OF THE INVENTION However, the direction of the passenger ship 21 is outward facing. The two central banks' 29 series are configured back-to-back. So that a second linear unit 49 of each seat unit in Yin Central Bank 29, Generally, the second linear edge corresponding to one of the other seat units 40 located in another central bank 29 is continuous. however, 5 Compared with the first cabin 20 trip 29, Seat unit 40 on line 29 of second cabin 21, It is so configured that in each seat 71, After 72, The seating unit forms a generally triangular or trapezoidal space 36, It is occupied by a first surface 47 of one seat 40 and a second surface 48 of another-adjacent seat unit 40. 10. The private partition is located between the two Central Banks of China. The partition may include a movable section member, It's in the middle of the seat 40 of each pair of the two Central Banks 29, The positioning member can selectively move in an unfolded position between storage and retracted standing position, In the deployed position, the positioning member effectively forms a privacy barrier between the two pairs of seats 40, While; Remove the positioning member in the storage and retrieval position, So that the passenger using the second corresponding seat is in the form of a bed or a seat, There is no boundary between them. The seat system of the present invention allows each seat unit 40 under the bed form, Provide a passenger bed surface, Its length is at least 80 inches (2'032 a feet) 'in each row of 29. The distance between the adjacent seat unit buckles is 50 to 60 忖 ⑽ to ⑸ meters). In some cases, It is possible that the size of the bed provided in the form of a bed at a distance of more than 1 inch (2. 16 meters). It should be noted that Husband 3 is also one of Tamoto's miscellaneous seats. 40 mobile passengers 48 593064 玖, Description of the invention 72, As shown in Figure 2, Is configured as a dining or reclining seat, Seat 71, The space 36 behind 72 is concealed by an upright or backrest 72. therefore, When the seat unit 40 is used as a seat, Space 3 6 provides a useful storage space, In particular, it can be used to store bedding materials, Such as pillows, blanket, Duvets and the like. Edge net bedding material can be stored in seat 71, 7 2 The space behind 3 2 ’so that the bedding material is made up of seats 71, The rear surface 72 is supported by the first surface 47. When a passenger wishes to sleep, Movable passenger support element 7 丨, 72, The 76 series can be selectively moved to the bed form 1 shown in Fig. 2, So seat 71, The rear space 36 is exposed after 72, Allows easy access to bedding stored in it. Using movable seat elements 71 in the form of beds 72, 76, The extended bedding surface provided by the seating unit 40 is used to manually place bedding material by passengers or flight attendants. It is used to provide a fully finished bed for passengers. 15 In the seat format, A first passenger using a seat unit can sit on a seat composed of a seat chassis 71 and a backrest 72, And a second passenger who wishes to see the first passenger can sit in the auxiliary seat provided by the upholstered seat 65. As shown in Figure 1A, The second surface of the seat unit 40 carries a hinged arm joint 75, It is hinged to the support structure 42 for use between a storage position and an unfolded position (not shown) as shown in FIG. Shake in the plane of the second surface 48, The armrest extends substantially parallel to the second linear edge 49 in the storage position, In the deployed position, the armrest is in the cube recess parallel to the seat composed of the seat chassis 71 and the backrest 7 2 * * 49 Description of the invention Roughly parallel to the abstract seat axis C-C, f The passenger who uses this seat—the passenger can pick one of his or her—arm off the arm * 75 ° can be grounded ’The armrest 75 can be stored in a -recess (not shown) formed in the plane 48, And a component can be provided for vertically translating the arm rest ′ to a storage position_the arm rest system 2 between the storage position and the -1 position flush with the top surface 48, The armrest protrudes from the recess in the deployed position to provide an armrest for use by a seat user. The advantage of this deliverable j method is that In storage locations, There is no collision of the arm against the available surface area provided by the top surface M. Another fixed armrest (10) is supported by the partition 60. The seating system of the present invention includes a plurality of self-provided seating units 40, Each unit provides passengers with separate seats and sleeping berths. In every 仃 29, As you can see, The partition 60 of the second side 54 of one seat unit 40 and the partition 60 of the other adjacent seat unit 40 are arranged side by side with the first side 53 of a seat unit 15 4o. Form a part of the closure, private space, For passengers using this one seat unit 40. Each seat unit 40 of the present invention includes a seat shell 43 and a cushion 65 first. The cushion stool 65 is spaced from the front of the seat shell 43. however, As described above, the seat unit 40 of the present invention can be conveniently formed by integrally molding the seat shell 43 of one seat sheet 40 and the upholstered seat 65 of another adjacent seat unit 40. therefore, The support structure 42 forming the seat shell 43 of one seat unit 40 is integrally formed with the support structure 42 of the upholstered bench 65 forming another adjacent seat unit 40. therefore, The seat system of the present invention, As shown in Figure 1A, It can be composed of multiple seat modules 80. Per module 50 593064 玖, DESCRIPTION OF THE INVENTION 80. A movable seat element 71 including a seat shell 43 and a seat unit 40, 72, 76, And another upholstered bench 65 of the adjacent seating unit 40. By attaching a plurality of the seat modules 80 to a passenger cabin 20, A pair of seats in 21 34, Can assemble multiple seat units 40, Each seat unit 5 400 includes a seat shell 43 of one module and an upholstered seat 65 of another adjacent module 80. The female seat module 80, As shown in Figures 1 and 1a, Attached to a pair of seats at three o'clock 32, 34. In particular, Each seat module 80 is attached to the pair of seat rails 32 at two separation points 38, 34 of them, 10 of them, Attached to the pair of seats at a single point 39, Another seat at 34 presided. 80 per seat module, It can be directly attached to the pair of seat rails 32, 34 or, Alternately, The support structure 42 of each module 80 may include a base or armrest (not shown), The base or armrest is attached to the seatway 32, 34. In either case, The support structure 42 or the base 15 or the armrest are attached to the seat rail 32 using foot fixing devices known to those skilled in the art 34. Using the three-point fixing method 38, 39 for attaching a seat module 80 to a pair of seat rails 32, 34, Has been found to be advantageous, Beyond a traditional four-point fix. In particular, It was found that the two-point fixing method allows the There is a large degree of deflection between the two seat rails of track 34. This allows the two seats to move or flex relative to each other in an emergency landing situation, Or lower the seat module 80 when falling down. 34 The risk of separation is reduced. The form of each seat unit 40, And the configuration of the seat unit 40 in a cabin according to the present invention, Allows users of 40 per seat unit 51 玖, Description of the invention Easy access to the seating unit 40 from the aisle, vice versa. The first passenger seat assembly shown in Figures 3 to 5 is a first passenger seat assembly of the present invention. , The seating unit 40 of the seating system illustrated in Figures 2 and 2A. however, Those skilled in the art should know that, The seat system of the present invention is not limited to the seat assembly shown in Figs. The above-mentioned seating system can basically include any seat single 40, It defines an abstract seat longitudinal axis c_c, And includes a support structure 42 for supporting the seat unit forming member 71, which is separated from the floor 30 of a vehicle, 72 or can be assembled to form a seat, It includes a seat chassis 71 and a backrest 72 and members 48, 67, 74, 76, Formed or assembled to form a substantially flat bed, The main part of the bed is placed in front of the seat, The bed is extended behind the seat to stretch the bed flat. In Figures 3 to 5, The first passenger seat assembly and the 1A, 2 and 15 2A The seat unit 40 is the same as the component, It is indicated by adding the same symbol "Γ" to it. The first passenger seat assembly 14 of the present invention has a front end portion 151, A rear end portion 152 and two opposite side edges 153, 154. The seat assembly 14o includes a branch #, , Ό 结构 142, For fixedly fixing the seat assembly 4o to the seat track embedded in the floor 130 of a 20 carrier, It is also used to leave the seat assembly when the seat assembly is 140. Any suitable foot fixture of the type known to those skilled in the art, The system can be used to secure the support structure 142 to a pair of seats. Although the first passenger seat assembly 14 in Figures 3 to 5 is particularly suitable for use on aircraft passenger aircraft, But it can also be applied to other forms of multiplication 52 593064 玖, Description of the invention E.g, Such as trains, Long-distance buses and water-borne craft, Includes passenger ships as well as ferries and hovercrafts. The supporting structure 142 includes a seat shell 143, It is generally arranged toward the rear end 152 of the assembly 140, And an upholstered stool 165 is generally arranged 5 toward the front end 151 of the assembly 140. The seat shell 143 forms a generally linear or cubic recess 144, It is open at the upper end 201 and the front end 202, And at its rear end 203 by a substantially vertical rear wall 204, And the opposite, separated by two on each side, Generally vertically extending side walls 205, 206 is closed. In Figures 3 to 5 of Figure 10, Only one of the side walls 205 is seen. Behind the recess 144, The seat shell 143 forms a substantially flat first upper surface 147, And a middle side of the recess 144 and a side 153 of the assembly, The housing 143 further forms a substantially flat second upper surface, It is generally coplanar with the first surface 147, And are generally continuous at the same time. The first and 15 second upper surfaces 147, The I48 is strong enough to support a portion of the weight of passengers using the seat assembly 140. The upholstered stool 165 is separated from the front of the seat shell 143, And has a substantially flat upper surface 166 which carries a pad 167, A flat upper surface 169 of the seat cushion is generally connected to the first and second upper surfaces 20 and 147 of the seat shell 143, I48 is coplanar. The ottoman unit 165 is also sufficiently sturdy at the same time, To support the weight of passengers and can be used as an auxiliary seat. Each side wall 205 of the recess 144, 206 carries a rotary bearing to]. The rotary bearings 222 are aligned with each other, To form a horizontal axis which extends laterally through the recess m and is substantially parallel to the floor surface 13 °, But slightly tilted 53 593064 玖, Invention Description As detailed below. The rotation bearing 222 is disposed higher than the floor surface 130 ', and its height is approximately on the floor surface 130 and the first and second upper surfaces 147, Intermediate position between 148. The rotary bearing 222 is also disposed substantially backward in the recess 144 at the same time. Toward the rear wall 204. Each of the rotary bearings 222 accepts another one of the seat moving mechanisms 220 as shown in one of FIGS. 6 to 8. Trunnion 221 extending horizontally, Where for clarity, The supporting structure will be omitted. Each trunnion 221 is generally attached centrally to another, A substantially flat, lenticular lens-shaped shaking plate 223 Facing the surface 10 surface 226. Each shaking plate 223 has a first edge 224 that is substantially linear, And an opposite arched second edge 225. Figures 9 to 丨丨 are detailed drawings of the shaking plate 223. Each shaking plate has an upper end portion 228 and a lower end portion 229. And the two shaking plates 223 are formed by a substantially cylindrical shape, Having two opposite ends 231, The first torsion tube 232 of 232 is fastened 15 together. Each end 231 of the torsion tube 230, 232 is connected to an inner surface 227 of one of the special shaking plates 223 juxtaposed with the lower end portion 229. The first torsion tube 230 is thus used to unite the two shaking plates 223, It forms a recess 235 in the middle of its respective opposite inner surface 227. The combined swinging plate 223 can thus be related to the trunnion 221 connected to the rotary bearing 222, And the housing 143 relative to the seat 20 shakes. The chevron-shaped edge 225 of the female rocker plate 223 is pivoted to a lower end portion 229 of the female rocker plate 223 to an end portion 242 of a link M1 through a suitable pin joint. The other end portion 243 of the connecting rod 241 is pivotally connected to one end portion of a rocker arm. 2 4 Figures 14 and 15 show, The other end 2 of the rocker 245 is privately secured 54 593064 玖, Description of the invention Dingniu solid ground and individual end portions 251 of a first rotatable torque tube 25 252 tied. At one end 251, The second torsion tube 25 is rotatably supported in the hollow worm gear housing 260. At the other end 252, The second torsion tube 250 is rotatably mounted in a bearing 5 53 supported by the second side wall 206 of the recess 144. The worm gear housing 260 has a substantially flat bottom surface%, And form a substantially cylindrical inner chamber 262, It is a bearing 253 for receiving one end 251 of the second torsion tube 250. One end portion 251 of the second torsion tube 25 is fixed coaxially and firmly to a worm wheel 10 271 received in the cavity 262. The casing 260 has an upper wall 263 which is partially cut away to expose the teeth of the worm wheel 271 as shown by the reference numeral 264. The casing 26 is behind the recess H4, Juxtaposed with rear wall 204 Located below the second upper surface 148, The support structure 142 of the first seat assembly 140 is fixedly secured in a recess (not shown) in the first side wall 205. 15 The upper wall 263 of the casing 260 forms a generally upwardly extending lug 265, And a generally cylindrical ant housing 273 is hinged to the lug 265, For an engagement position as shown in Figure 14, Move to a disengaged position shown in Figure 15. The worm housing 273 is made in an appropriate shape. So that in the engaged position, The casing 273 is engaged with the upper wall 263 of the worm wheel casing 2620. As shown in Figure 15, The worm housing 273 is cut off as shown by the representative symbol 274. It is used to allow the teeth of the worm gear 271 to extend into the worm gear peripheral 273. As shown in Figure 16, The worm housing 273 receives a sprocket 270, It is rotatably mounted between two opposing thrust bearings 272. The worm 270 is rotatable via a coaxial mandrel 275, With having a horse 55 593064 玖, Description of the invention The electric motor 280 of the housing 281 is combined, It is fixed firmly to the worm housing 273. As shown in Figure 16, The motor housing 281 is connected via two links 282, 283 is connected to the worm gear housing 260, Form a "break-link" device. One of the links 282 is pivotally connected to the motor housing 5 281 at one end 284, It is pivotally connected to the first end of the other link 283 at the other end 285. A second end portion 286 of one of the other links 283 is pivotally connected to the worm gear housing 260. The one link 282 is substantially larger than the other link 283. And in the engaged position, Three pivot points 284, 285, 286 is coplanar, So that the pivot point between the second end of the other link 283 and the worm gear housing 260, Series 10 is configured between two link 282, A pivot point 284 of a link 282 between 285 to a middle position between the motor housing 281 and the pivot point 285, This prevents the worm housing 273 from being detached from the worm gear housing 260. The link 282 can be selectively rotated clockwise as shown in FIG. 16. Causing the other link 283 to rotate clockwise at the same time, "Destruction" Three Pivot Points 284, 285, 286 of the alignment. 15 The worm 273 is thus able to disengage from the worm gear, The swing arm 245 is allowed to rotate freely in relation to the axis formed by the second torsion tube 250, Connecting rod 282, 283 is used to limit the degree to which the worm housing 273 can disengage from the worm housing 260. Alternately, Instead of a break-link device, The worm housing 273 can Such as a removable bolt, Releasably fastened to the worm gear housing 260 20 〇 As shown in Figure 9, The inner surface 227 of each shaking plate 223 is constructed with an elongated, A substantially linear recess 301, Its cross section is generally linear, And substantially parallel to the first edge from the lower end portion 302 juxtaposed with the lower end portion 229 of the shaking plate 223, Extend to the position of the shaking plate 223 56 593064 玖, Description of the Invention 4 Upper and lower end portions 228, An upper end 303 at an intermediate point of 229. As shown in Figures 3 to 5, The elongated recess 301 receives a linear screw 304, As shown in Figure 3, it has upper and lower ends 305, 306. In some specific examples, the 'ball screw' or any other suitable, An irreversible linear actuator device can be used to replace the two linear screws. At its upper end 305, Each linear screw 304 is rotatably mounted in a bearing 307. It is fastened to the rocking plate 223 at the upper end 303 of the recess 301. The lower end 306 of each linear screw 304 is accommodated in a gear housing 31. It is fixed firmly to the inner surface 227 of the individual shaking plate 223. (In Figures 13 and 10, Omit one of the gear housings 3 10, It is used to show the detail at the end of the linear screw 304 at the end 306). The lower end portion 306 is supported by a rotary bearing 308 in a gear housing 310. It is rotatably coupled to a respective end portion 313 3 14 of a rotating transmission shaft 312 via a helical gear 3 11. At one end 3 14 Transmission shaft 3 12 is a pair of pinions 315 meshing with each other 15 316 is connected to a stepping motor 3 18, It is mounted to the gear housing 310 so that the actuation of the motor 318 causes the shaft 312 to actuate, As a result, the linear screw 304 is rotated. Each linear screw 304 carries a nut 32o, It includes a main body 321 made in a suitable shape. The main body 321 has a cross-sectional shape of τ 2. And includes a substantially straight slider portion 322, It is made in the proper shape, It is used to form a tight but free sliding fit in the linear recess 301 'formed in the inner surface 227 of the individual shaking plate 223. The slider part 322 accommodates a linear screw 30 therein, And contains internal structure (not shown), Used to mesh with the screw 304. The main body 321 further includes 57 593064 玖, Description of the invention A pair of opposing wing portions 324, Each part has a generally flat outer surface 325, The outer surfaces 325 of the two-wing portion 324 are substantially coplanar with each other. The main body 321 has a substantially flat inner surface 326. The / month piece portion 322 is inserted into the linear recess 301 of the individual shaking plate 223, The outer surface 325 of the 5-wing portion 324 is closely adjacent to the inner surface 227 of the swing plate 223. Related to Figure 6, Each nut 320 passes through a horizontal free joint 329 and an individual lateral side edge 331 of a structural diaphragm 330 of the seat chassis element 171 constituting the part. 332 connections, It is arranged in the recess 235, 10th place is in the middle of two opposite shaking plates 223. The diaphragm 330 may include a light weight, Moulded into a dare board or a porous sheet. The seat chassis element 171 has a rear end portion 333 and a front end portion 334. The horizontal free joint 329 is fitted to the diaphragm 330 toward the rear end portion 333. To allow the front end portion 334 of the seat chassis element 171 to tilt up or down relative to the rear end portion 333, Relative to the shaking plate 223, it moves less. The seat chassis element 171 includes suitable cushions and pads, It is supported by diaphragm 330, Provides a comfortable seating surface for passengers using the seat assembly 140. (For clarity, (Seat cushions and padding are omitted in Figures 6 to 8). The diaphragm 330 juxtaposed with the front end portion 334, It is pivotally connected to an upper end portion 341 of a suspension rod 342. The other end of the rod 342 is pivotally connected to a slider 345, The slider is slidably held in an elongated, In the generally linear slide 350, It is fixed firmly in place in the side wall 205 of the seat shell 143 in the recess 144, One of the individual side walls of 206. As can be clearly seen in Figure 3, The direction of each slide 35 is relative to the floor 58 5193064 玖, DESCRIPTION OF THE INVENTION The surface 130 is at an angle, So that the slideway 350 extends forward and upward in the recess 144 between an upper end portion 351 and a lower end portion 352 '. The other end portion 343 of the rod 342 is also pivotally connected to a lower end portion 354 of a tow post 355. An upper end portion 356 of the tow post 355 is pivotally connected to a first linear edge 224 of an individual swing plate 223 juxtaposed with a lower end portion 229 of the swing plate 5 223. Related to FIG. 9, The inner surface 227 of each shaking plate 223 forms an elongated sacral track 360 at the same time. It is tied between an upper end portion 361 juxtaposed with an end portion 228 above the plate 223 and a lower end portion 10 362 juxtaposed with an end portion 229 below the plate 223, It extends parallel to the second arched edge 225. In the middle of the linear recess 301 and the arched guide 360, The inner surface 227 of each shaking plate 223 forms a short linear slit 365 at the same time. It is formed from an upper end portion 366 which is juxtaposed with the upper end portion 361 of the road 36. It extends to the lower end portion 367 which is juxtaposed with the upper end portion 303 of the linear recessed portion 301. As can be clearly seen in Figure 3, The linear fissure 365 is related to the linear edge 224 of the plate 223 at an angle, So that when the slit extends downward from the upper end portion 366 to the lower end portion 367, It extends inwardly from the linear edge 224 towards the arched runner 360. You can also see that, The arched track 360 and the linear slit 365 are separated from their respective upper ends 361, 366 toward its respective lower end 362, 367 split away from each other. Twenty arched rails 360 on each rocker plate 223 receive slidable two spaced friction block pieces 371, As shown in Figure 6AA6B, It is fixedly secured to the outer surface 372 of the individual underside member 373, one of the several offending pieces 374. The lower back rests on the element 374, Together with a top-back element component-back Λ το element 172 detailed below. Each-underside member 373 is generally dagger-shaped 59 593064 玖, DESCRIPTION OF THE INVENTION The upper end portion 375 and the lower end portion 376 and the substantially linear rear edge 377 are provided. At the lower end portion 376, Each lower side member 373 includes ’, There is an enlarged foot portion 378 with a nasal portion 379. Each lower member 373 has a substantially linear front edge 381, It is 377 degrees to the rear edge—a slight angle, Extending between the upper end portion 375 and the enlarged foot portion 378. As shown in Figures 6A and 6B, On each lower side, One of the friction block members 371 is attached to the outer surface 372 at the end 376 below the side member 373, At an angle of about 45 degrees to the rear edge 377. The other-capricorn block 371 is attached to the upper and lower ends 375, "376 Middle spoon" occupies the women's clothing on the outer surface 372 juxtaposed with the rear edge 377. 4 Another friction piece 371 is also at an angle to the rear edge 377, However, this angle is smaller than the angle formed by a friction block member 371 and the rear edge 377. 15 in the middle of the two lower side members 373, The lower backrest element 374 includes a generally flat diaphragm 385, Is it related to the front and back edges? " , 381 within one. 卩 separated, Used to form rear and front recesses% 6 and 387, respectively. Similarly, The seat diaphragm 385 may include a molded synthetic panel or a porous metal sheet of a type well known in the aircraft seat manufacturing industry. The outer surface 372 of each side member 373 further forms a substantially linear cavity 39o, It has a surrounding sidewall 391. The chamber 390 is covered by a cover plate 38 (for clarity, Attached to Figures 6-8 and 6] 3), It is fixedly secured to the outer surface 372 of the side member 373. The chamber 390 receives a generally triangular rocker 392, It has an upper wing member 393 and a lower wing member 395. The rocker 392 is substantially centrally pivoted to the side member 373 at its obtuse apex 396. At the end of the lower wing member 395 60 20 玖, DESCRIPTION OF THE INVENTION The head is provided with a bolt 397 facing outward, A lug 398 is arranged at the end of the upper wing member 393. The rocker 392 can thus use the upper and lower wings 393, The corresponding shaking of 395 'is related to the shaking of the pivot 396. The movement of the rocker 392 is restricted by the side wall 391 of the chamber 390, So that the upper wing 393 can be in a position as shown in Figures 6A and 6B, The lug 398 is completely arranged toward 向, With another location (not shown), The upper arm 393 is completely rearward. Shake between. The latch 397 on the lower wing member 395 is slidably stored, Formed in the inner surface 227 of the individual shaking plate 223. As can be clearly seen in Figure 3, 〇The next month's crime element 374 extends upward from the rear end 333 of the seat chassis element 171, It is pivotally connected to the upper backrest element 394 at its upper end 375. The last month sin component 394 includes two spaced-apart upper members 402, And a generally flat upper diaphragm 403, It extends between the upper side members 402. Each upper member 402 has a substantially linear rear edge 404, And 15 a generally linear front edge 405, And the upper diaphragm 403 is connected with the two rear and front edges 404, 405 separated inland, To form the front and rear upper recesses 406, 407. The lower and upper front recesses accommodating the cushion 387, 4〇7 is specially designed, To form a comfortable backrest surface, It is combined with the cushion on the seat chassis element 171, Constructs a passenger-specific seating surface. 20 The back cushion installed on the back is matched with the cushion on the seat chassis element 171. For clarity, On the 6th, 6 Eight, Commit, Figures 7 and 8 omit the cushions and cushions of the upper and lower moon criminal elements. Upper and lower rear recesses 386, 4〇6 forms a generally continuous recess, It accepts a substantially flat cushion or mattress suitable for forming a bedding surface. Furthermore, For clarity, On page 61, Invention Description 6 6A, 6B, This section is omitted in Figures 7 and 8. however, In particular, Configured in the upper and lower front recesses 387, Back to back in 4〇7, The system can have a different style or color from the back cushion or mattress. Furthermore, Cushions respectively arranged on the front and back surfaces of the backrest element, The degree of flexibility may be different for the purpose of seat and bedding. Each of the upper side members 402 has an upper end portion 409 and a lower end portion 411. Each upper member 402 is attached to the upper and lower end portions 409, 410 in the middle of 411 represents the symbol, Pivoted to the upper end of the individual lower member 373, So that each upper side member 402 extends downward from the pivot point 41o, To form 10 into a foot part 412, The portion has a substantially U-shaped cutout portion 414 at the lower end portion 411 thereof. The ub-shaped cut-out portion 414 slideably receives a lug 398 formed on the wing member 393 above the individual rocker 392, It is used to transmit the swing of the arm 392 to the upper member 402. therefore, Rocker 392 phase about its central pivot point 396, So that between the upper and lower backrest elements 15, The upper backrest element 394 is shaken corresponding to the pivot point 410. Corresponding to FIG. 3 'The nose portion 379 of each lower side member 373 is connected to one of the wings 320 on the nut 320 via the invalid movement device 420. The nut is linearly mounted on the individual swing plate 223 Screw on 304. The female-invalid movement device 420 includes a latch, It is attached to the individual wing section 325 at the symbol 20 328, The latch is received in a short slit formed in the nose portion 379 of the lower member 373. Related to Figures 9 to 12, The arched edge 225 of each of the shaking plates 223 forms a protruding lug 431 facing the upper end 228, It is pivotally connected to one end 433 of an arm member 432, The end of the arm member 432 is located away from the lug 62 593064 玖, DESCRIPTION OF THE INVENTION In the other end 434 of 431. The two-arm member 432 carries a transverse filling membrane member 440, The member carries a generally reclined cushion 442 having an upper surface 443. The outer surface 226 of each of the shaking plates 223 juxtaposed with the lug 43 1 1, Fasten a small dog-leg member 450 for 5 years, It is pivotally connected to the rocking plate 223 between the lug 431 and the lower end portion 229 of the rocking plate 223 at a symbol 451. The folding line member 45 has a first wing member 452, A hook 453 is arranged at the end of the wing, And a second wing member 454 is provided with a cam follower 455. Each arm member 432 has an outwardly extending support pin 456, 10 and the outer surface 226 of the female-rocking plate 223 constitutes a stop bolt 457 extending outward, It is located between the pivot point 451 of the plate 223 and the arched edge 225. The polyline member 450 can be freely rotated in relation to the pivot point 45 丨 And, as shown in Figs. 9 to 12, the stopper pin 457 is used to restrict the clockwise rotation of the fold line member 450 of the plate 223. (The stop pin 15 on the other shaking plate 223 restricts the counterclockwise rotation of the corresponding folding line member 450). The cam follower 455 ′ located on the second wing member 454 of the folding line member 450 is connected to the individual side walls 205, A cam 460 (see Figures 8 to 12) on 206 engages, Used to control the movement of the polyline member 45. As shown in Figure 3, As explained earlier, the first seat assembly 1440 series 20 can be configured as an upright seat, The rocker arm 245 extends forward relative to the rotating shaft 50 located in the recess 144. And the connecting rod 241 is substantially coplanar with the rocker 245, So that the joint shaking plate 223 is oriented as in the third, 4 6. The seating patterns shown in Figures 7 and 10, The linear edge 224 of each of the shaking plates 223 extends upward and backward within the recess 144, At the second shake 63 593064 Rose, DESCRIPTION OF THE INVENTION The arched track 36 on the plate 223 extends substantially downwardly and forwardly within the recess 144. When the diagonal of the connecting rod 241 and the rocker arm is 180 degrees, Used to form a compression post in the seat position, Any load applied to the shaking plate 223 is applied linearly to the second torsion tube 25, No turning force is applied to the worm gear. 5 Advantageously, The seat conversion sub-mechanism of the seat assembly can withstand large forward forces, There is no need for any additional T disconnection mechanical coupling between the seat moving mechanism and the support structure, Such as a shootjoit. In the upright seat form, As shown in Figure 13, The nut 320 is disposed at the upper end portion 305 of each of the linear screws 304, And the lower end 343 of the rod 342 is arranged at the upper end of the slide 350, So that the seat chassis element 171 is disposed substantially horizontally within the recess 144, The upper surface of the seat chassis cushion is approximately connected to the first and second upper surfaces 147, 147, 148, And the surface 169 above the cushion 167 on the ottoman 165 is at the same height. The friction piece 371 15 on the side member 373 under the lower backrest element 374, It is arranged at the upper end portion 361 of the arched track 360 on the shaking plate 223, The latch 397 on the rocker 392 is disposed at the upper end portion 3 66 of the linear slit 365 on the rocker plate 223. therefore, The upper wing member 393 of the rocker 392 is arranged completely forward in its individual cavity 39. As a result, the upper back element 394 is substantially collinear with the lower back element 373 (C0-nnear). In the upright position in Figure 3, The folding line member 450 on the rocking plate 223 is disengaged from the individual cam member 46. And as shown in Figure 10, In the storage location, The arm member 432 is disposed so that the filling cushion 442 is disposed substantially below the first upper surface 147 of the seat shell 143. In the upright position ’on the upper and lower backrest elements 394, Seat 408 on 373, Form a 64 593064 玖, Description of the invention Ergonomic comfort A conformable seat with a cushion on the seat chassis element 171. In the upright position, The seat formed by the seat chassis element 171 and the backrest element ⑺, Generally suitable for meals. The soft sensation unit 165 is a fish. The 5-seat chassis element 171 is separated from the front side. It can be used as a footrest for passengers. From the upright position in Figure 3, The following seat assembly can be tilted back as shown in Figure 4-fully reclined position. Once the stepping motor 318 is activated, The linear screw 304 on the shaking plate 223 is caused to rotate. When restricting the nut 10 320 to rotate with the linear screw 304, The nut is driven in translation along the linear screw The opposite inner surface M? The lower end portion 302 of the middle concave portion 301. When the nut 32 is driven downward, The rear end portion 333 of the seat chassis element 171 is simultaneously driven downward with respect to the front end portion 334 supported by the lever 342. The rear end portion 333 of the seat chassis element 171 is thus driven downward 15 The seat chassis element is caused to tilt rearward relative to the pivot axis between the upper end portion 341 of the lever 342 and the seat chassis diaphragm 330. When the linear screw 30 extends downward and forward in the recess 144, The seat chassis element 171 is driven forward simultaneously, This forward movement is accommodated by the forward swing of the lever 342 relative to the pivot between the lower end 343 of the lever 342 and the slider 345 in the individual slideway 350. 0 The front end portion 334 of the seat chassis element 171 thus moves slightly downward in the recess 144, However, the same degree of movement as the rear end portion 333 of the seat chassis member 171 is not achieved. The dragging post 355 'located between the slider 345 and the rocking plate 223 prevents the slider 345 from moving backward along the slide path 35o. The forward and downward movement of the nut 320 causes the backrest element 172 to correspond to 65 593064 玖, Description of the invention It is connected to the nut 320 via an inactive movement device 420 located on the nose portion 379 of the lower backrest element 373. Back to element 1? The movement of 2 causes the friction block member 371 in its respective arched track 360 located on the opposite inner surface 227 of the shaking plate 223, It slides from the upper end portion 361 of the holding channel 360 toward the lower end portion 362. As mentioned above, The relative direction of the friction block 371 and the bending of the execution path 360, When the friction piece 371 slides along the rail 36 °, The lower backrest element 373 is caused by the upright position shown in FIG. 3 as shown in FIG. 4, Swing back to the fully reclined position as shown in Figure 4. At the same time, The latch 397 on the rocker 392 was caused by Slide along the linear slit 365 on the shaking plate 223 at position 10. When each linear slit 365 is opened from the corresponding arched track 360 on the same shaking plate 223 again, The wings above each rocker 392 are actuated, Shake backwards in individual chamber 39. The rearward movement of the wings 393 above the rocker 392, The upper side member 402 of the upper backrest element 394 is caused to swing forward with respect to the lower backrest element 373. 15 When the backrest element m is driven forward and downward by the movement of the nut 320, The upper backrest element 394 swings progressively further forward relative to the lower backrest element 373, Until the rocker 392 engages with the side wall 391 of the individual chamber 390, The further forward movement of the crime component 394 of the above is prevented. The recesses 301 formed on the two shaking plates 223, The relative position and shape of the road 360 and the slit 365 have been carefully calculated. It is used to ensure that when the seat is reclined from the upright position in FIG. 3 to the fully reclined position in FIG. 4, Seat chassis elements and upper and lower backrest elements 3 94, 374 is moving through multiple reservations, Ergonomically comfortable position. Control the stepping motor 3 18 so that the nut 320 can stop at the linear screw 3 04 66 玖, Description of the invention Upper and lower end portions 305, Any intermediate position between 306. therefore, The seat chassis element 171 and the upper and lower backrest elements 394, 374 formed by the movement of the seat, You can stop at any intermediate position between the upright position in Figure 3 and the fully reclined position in Figure 4. In a recline position, back 5 and 394 from top and bottom, The diagonal caused by 374, Causes the lower backrest element 374 to advantageously provide passenger lumbar support using the seat assembly 140. The linear screw 304 is an irreversible linear actuator device. Therefore, the seat assembly of the present invention has an additional advantage in that: The force applied to the seat chassis element 171 or the backrest element 172 cannot be transmitted to the motor 318 via the nut 320 and the linear screw 304. This has the advantage that, Applied to movable seat element 171, 374, The sudden and / or powerful force of 394, Not by a stepper motor, , bear", This reduces the risk of damage to the stepper motors 3 i 8. As explained before, a special performance of the first seat assembly of 140 It can be converted from the upright position in FIG. 3 to a bed form as shown in FIG. 5. In order to convert the seat assembly 140 from an upright form to a bed form, The motor 280 is activated to rotate the worm 270. Place the worm housing 273 on the worm gear housing 260 in the engaged position, The rotation of the worm 270 causes the worm wheel 271 to rotate correspondingly. As a result, the second torsion tube 25 is caused to rotate. The rotation of the torsion tube 20 250 causes the swing arm 245 to move from a seat position as shown in FIG. Turn to a bed position as shown in Figure 14. Related to Figures 3 and 5, Rotating the rocker arm 245 backward causes the link 241 to rock the rocker plate 223 forward with respect to the trunnion 221. Shaking the shaking plate 223 forward in the recess 144, Causes the lower backrest element 374 to be related to the trunnion 221 67 593064 玖, Description of the invention Shake forward. A horizontal free joint 329 between the seat chassis element 171 and the nut 320, At the same time is related to the rotation of the trunnion 222, And the rocking of the rocking plate 223 causes the tow post 355 to pull the slider 354 back and down along the slide 350 at the end 343 below the rod 342, From the upper end portion 351 to the lower end portion 352 of the slideway. Within the recess 144, Front and rear end portions 334 of the seat chassis element 171, 333 was motivated to fall, So as shown in Figure 5, The backrest element 172 is rocked forward to cover the seat chassis element 17m. In the bed form in Figure 5, The seat chassis element 17 is disposed at a lower storage position in the recess 144. And under the backrest element 172 and 10 upper back recesses 386, The seat cushion or mattress in 406 is generally arranged on the upper surface 147 of the seat shell 143, 148, And the cushion 167 on the ottoman unit 165 is coplanar. As can be seen in Figure 5, Upper and lower backrest elements 394, 374 is made to proper size, So that in the form of a bed, The upper end portion 409 of the upper side member 40 is in contact with the ottoman unit 165, So that it rests on a cushion or mattress on the surface behind 15 elements, On the ottoman unit 165, a pad 167 forms a substantially continuous surface, A second upper surface 148 is formed on the seat shell 143. Advantageously, The upper end of the upper backing element 394 409, Is engaged with a structure (not shown) on a ottoman unit 165, 2 so that in the form of a bed, Part of the load 20 applied to the backrest element 172, The system is supported in part by a ottoman unit. The rocker 392 is located on the lower side member 373 of the lower backrest 374. The side walls 391 of its individual chambers engage, Used to place the upper and lower backs on the element 394, 374 fixed together, Prevent in bed form, Under load The backrest element 172 is flexed. The swing plate 223 moves from the seat position to the bed position, At the same time it was raised 68 593064 玖, DESCRIPTION OF THE INVENTION An arm member 432 filling a cushion 443 is carried in the recess 144. In the seat position shown in Figure ⑺, The folding line member 45 is formed from the side surface 205 formed on the side of the recess 144, Cam 460 on 206 is disengaged, And can pivot freely in relation to the pivot point 451. however, As described above, the movement system 5 of the 'broken line member 45' is restricted by the stopper pin 457. When the rocking plate 223 is rocked forward toward the bed form of FIG. 5, The support pin 456 on the arm 432 becomes closed behind the hook 453 on the first wing 452 of the folding line member 45. When the shaking plate 223 is moved toward the bed, The cam follower 455 is engaged with the cam 460, The fold 10 wire member 450 is thus fixed in place, The support pin 456 is closed behind the hook 453. As can be clearly seen in Figure 5, Arm member 432, Cushion material 2, Support building latch 456, The folding line member 450 and the cam 460 are made and positioned in an appropriate shape so that In bed form, Filling the upper surface 15 443 of the cushion member 442 is filling the end portion 376 between the lower backrest element 374, A space from the front end of the first upper surface 147 of the seat shell 143. The upper surface 443 of the filling cushion structure 442 is generally a cushion or mattress disposed on the back of the backrest element 172, And the first upper surface 147 is continuous and coplanar ’to form a stretched, A substantially flat bed surface. 20 Assemble the supporting structure 142 of the seat assembly 140 so that During the flight ’the floor surface 130 is at an angle of approximately 1.3 degrees to the horizontal, The bed surface provided by the seat assembly of the present invention is substantially horizontal relative to the ground. For 5 ', the seat assembly of the present invention, 140, locks the aircraft slightly tilted during flight. 69 593064 玖, DESCRIPTION OF THE INVENTION Advantageously, Worm gear, Worm assembly 271, 270 is irreversible, And thus in the form of beds and seats, The motor 28 will not, , Suffering "excessive force exerted on the shaking plate 223. In other words, Excessive or sudden force on the shaking plate, It is not transmitted to the motor 280 via the worm gear / worm assembly. 5 As explained earlier, The first passenger seat assembly 140 is equipped with a user-operable controller. It is conveniently mounted to the support structure 142. The controller includes a device for operating a stepper motor 318, Between the upright position in Figure 3 and the fully reclined position in Figure 4, Selective moving seat chassis and movable back-to-back moving element 171, 374, 394, And for 10 actuation motors 280, 间 Between the upright form in Figure 3 and the bed form in Figure 5, Conversion of movable element 171, 374, 394, Among them movable backrest element 374, 394 is a fixed auxiliary component with support structure 142, Which is the soft pouf unit 165, And the first and second upper surfaces 147 of the seat shell 143, 148 cooperation, Used to form a stretch, 15 beds for roughly flat passengers. The controller includes a control circuit, Used to ensure that when the seat is in a reclined or fully reclined position, If a passenger attempts to convert the seat assembly from a seat form to a bed form, Then the stepping motor 3 丨 8 operates first, Before the seat is converted into a bed by the motor 280, Will be removable month Λ element 171, 374, The 394 returns to the fully upright position. If motor 20 280 or aircraft cabin power fails, By interrupting the interrupt linking device 282, as described above, 283, And manually rock the rocker arm 245 forward to the seat position in FIG. 15. As illustrated by The first passenger seat assembly 4 () of the present invention, So provide your own, Individual passenger seats and sleeping berths. 70 593064 玖, Description of the invention Figure 17 shows another seat system according to the invention, It includes a plurality of first passenger seat assemblies 140 of the type previously described in relation to Figures 3 to 16. In Figure 17, At a position behind the nose portion 515 of the fuselage 51, An aircraft fuselage 51o encloses a passenger cabin 52. As the first! Figure of the seat system, , 4 conditions, The passenger grab 52 () in FIG. 17 is the internal surface portion 526 opposite to the other two of the fuselage. 528, A floor surface or deck 530 located within the fuselage 51 and supported on a suitable support infrastructure (not shown), And the formation of a dagger (not shown). The basic structure includes a plurality of pairs of seat lanes 532, 534, It is embedded in the floor surface 53. In Figure 17-10, the guest grab 520 includes the second foreign seat 532, Each track is similar to the opposite surface of the body 510, Like one of the other surface parts running side by side, And a single center-to-seat seat M #. Each pair of seats holds 532, 534 'is formed substantially parallel to the plane S 51G and extends the longitudinal axis of the aircraft as shown by the chain-dotted line A-A in FIG. 15 seat assembly 140 series attached to seat track 532, 534, Used to form plural lines 529. Each line 529 is fixed to the individual seat of the pair of seat tracks 532, And form a vertical axis which is not abstracted by the lines in the i7 figure. Each seat assembly is 14 Is shown as the nth center line, Forming an abstract vertical seat axis, It is approximately 49 degrees diagonal to the abstract vertical axis b_b. In cabin 52 (), Attached to the seat of the outside facing claw ~, 140 ′ is facing forward and inward. The seat assembly 14 attached to the center counter seat 534, Formed a second group of brothers, . Attach to the center The seat assembly of the seat rail 534 is sharpened—the front group w faces forward And grab the 520-side towards the passenger, At the same time, the rear group 538 is facing forward and facing 71 593064 玖, Description of the invention The other side of the cabin 520. As shown in Figure 1, In each line 529, The seat assembly of FIG. 17 is arranged side by side offset from each other longitudinally, When the seat assembly 14 is in the seat form, Behind the backrest element 172, A substantially triangular or trapezoidal space 530 is formed behind each seat 5 assembly I40. As mentioned above, Each seat assembly is 140 series, Able to provide a passenger passenger, Stretched flat beds, Its length is at least 80 inches (202 meters) and according to the configuration of seat assembly 1 of the seat system of FIG. 17, The seat assembly 140 is allowed to be accommodated in the cabin 520 at a distance of about 50 to 60 inches (127-1.52 meters). therefore, A plurality of the seat assemblies of the present invention is 140, Each assembly provides an individual bed of at least 80 inches (2.032 meters) in length, Can be accommodated in a typical passenger business class. The internal surface of an aircraft fuselage 51 is concave in a vertical cross section, Therefore, in cabin 52 of Figure 17, Each opposing interior of the fuselage 51, 5 surface portions 526, 528, A lateral recess is formed at each side of the cabin 52. Advantageously, This lateral recess is formed by attaching one of the outer seat rails 532 to each of the outer seat rails 532 and the second passenger support auxiliary surface 147, 148 occupied. In bed form, First and second support surfaces 147, 148 of the extended M flat bed surface provided by each seat assembly, At the same time in the upright or reclining seat form, Horizontal: unit: Have sufficient headroom (head r_), The π integer south to accommodate the seat ’is the surface of the stretched bed to accommodate part of it, Low demand for headroom means the effective use of available space in passenger grabs. According to the invention, 72 593064 可, which can be selected to decorate the seat chassis element 171, Description of the invention And 37 buckets of backrest elements arranged in each seat assembly i4〇, 4G8 cushion on 394, So that when all or most of the top assembly of the seat system 140 series is configured as a seat, The cabin has a first special appearance and / or atmosphere suitable for dining and / or rest. Provides for 5 decorative lower and upper rear recesses arranged on the backrest element 172, The narrative material of the wounded mandible, The system may have a pattern and / or color scheme that is particularly suitable for a sleeping environment. In particular, You can choose the style of bedding material, So that when all or most of the seat assembly 14 of the seat system of FIG. 17 is in a bed form, The cabin 52 may have a different second appearance or 10 atmosphere, Compared with the first appearance, , Give people a good rest, , feel, And it is more suitable for a sleeping environment. Related to Figures 18 and 19 in the companion diagram, A passenger accommodation unit of another specific embodiment of the present invention, It consists of a shell assembly 610 assembled from two half shells 610a610b. The accommodating unit is configured to be deployed in the first flight of 15 passengers and at least-adjacent seats 61, Tied And two half-shell seams, 610b are similar to each other 'so that each half-shell forms part of two adjacent seats. 61〇a per half shell, 610b is composed of a suitable aircraft grade, The lightweight construction material is made as a single piece. Every valley, , , The inner single set of 61 includes a curve, Upright rear partition ... 20 And a relative, upright, Curved front bulkhead 614, Interconnected by a generally linear sidewall 616, Used to form a closed passenger space. The shell 610 includes a bottom edge 611, It forms a plane and is provided with a plurality of suitable fixtures (not shown), Used to attach the accommodating unit to the seat track in the aircraft passenger surplus. In some specific embodiments, The single 73 593064 玖, Description of the Invention The element system uses three or more of these fixing devices to be sufficiently fastened to the seat track. The shell 610 is provided with a suitable supporting structure for a seat 620, It includes a seat chassis 622, A backrest 624 and a backrest extension 626 (see Figures 20A-20C). In particular, The housing 61 of the accommodation unit includes a lower seat bottom 5 plate 628 (see FIG. 19), Its configuration is adjacent to the rear bulkhead 612, And has a generally flat, Horizontal top surface, Used to support the seat chassis 622. The far seat chassis 622 is pivotally connected to the lower seat chassis 628 at its front edge 623, And back to back, It is usually maintained in a generally upright position, Leaning against the inner surface of the rear bulkhead 612, At the lower end 625, it is pivoted to 10 to the rear end of the seat chassis. The backrest extension 626 is in the normal position as described above, Tied above the upper edge of the backrest 624 and at a generally continuous position, It is permanently fixed to the inner surface of the rear bulkhead 612. 垓 The enclosed passenger space 618 further includes a bracket 64. It is supported above the cabin floor on the shell 610 and abuts the front bulkhead 614. Optional 15 places, The bracket 640 is adjustable in height. It is any suitable method known to those skilled in the art. Behind the rear bulkhead 612, The shell 61 of the seating unit is made in an appropriate shape, Used to form a hollow foot box 630 (see Figures 21A and 21B). In Figures 18 and 19, Department showing the foot box 63 of the adjacent seat, . The foot box 20 63〇 includes a substantially horizontal inner shell, Its configured vertical height is generally the same as the height of the lower seat chassis 628. And an opening 629 is formed in the partition 612 behind the shell 610, Immediately behind the standard position, behind the 624, Used to allow access to the inside of the foot box 63o. The foot box includes a first side wall 632 which is an adjacent unit of the constituent parts 74 593064 玖, DESCRIPTION OF THE INVENTION Its direction is generally parallel to the abstract vertical axis of the unit. The foot box 630 further includes a second opposite side wall 634, > , Is a pair of acute angles with the abstract vertical axis of the unit, So that the plan view of the foot box has a substantially triangular or trapezoidal shape. In Figures 18_21, The footbox of each nano unit has a generally triangular shape, But 疋 can be on the second side wall 632, 634 cut off into a wall, The foot box is formed in a trapezoidal shape. Alternately, Where you want to place your seats side by side, The first side wall 632 may be omitted so that the first lateral side of the foot box is open. The end of the foot box 630 is located below the upper edge of the rear partition 612, It has a substantially flat upper wall 636. The upper wall 636 is formed as a substantially triangular shape, Flat part 638, It is used as a beverage side-table for adjacent units. As shown in Figure 19, Located on the upper surface of the foot box 63o and the lower seat chassis 628, The cushions are made with thick cushions, Or support a mattress section 15 652. Similarly, The bottom side of the seat chassis 622 and the back side of the backrest 624 are made into cushions. In a "seat format, , in, Seat chassis 622 and backrest 624 are usually as described in section 18, 20A and 21A are arranged as shown in the figure, So that a passenger can sit in the seat. however, When passengers wish to sleep, He or she can get up from the seat 20 and manually pull the backrest 624 off the rear bulkhead 612. As shown in Figure 20B, The backrest 624 can be swiveled relative to the seat chassis 622, And continuously pulling the sin 624, Causing the rear end of the seat chassis 622 to be lifted upwards away from the lower seat chassis, And related to its front edge 623 pivot. Like 2〇c & As shown in Figure 21B, Can operate seat chassis 622 and backrest 624, Used to provide a large 75 593064 rose, Description of the invention Flat and continuous sleeping surface, Among them, the side is supported on the top surface of the bracket 640 before the backrest 624, Between backrest 624, The joint between the seat chassis ⑵ and the lower seat chassis 628 is fixed as shown in Figure 20c. To form a "bed form, , . The passenger can thus lie on a flat surface with his or her head facing 5 front partitions 6U. By removing the backrest coffee from the rear partition 612, Opening 通过 through the shell ㈣, The passenger is allowed to stretch his or her lower leg through the opening into the foot box 63o. In bed form, Cushioned upper surface of shelf and lower seat chassis 628, And the bottom side of the seat chassis 622 and the back side of the backrest 624 can be fitted with suitable sheets such as a bed 10 morning and a blanket, And-the pillows for passengers can be placed on the back of the unit used for bed towels, and the surface of the unit can be made and fitted with a rafter different from that used in the seat form. When most of the units in the passenger grab are in one form or another, Can create a special atmosphere in the cabin. 15 By arranging the accommodating unit at an angle of about 40-50 degrees from the forward direction of the aircraft, It is preferably about 45 degrees. Can provide a passenger bed up to 7 feet (213 meters) in length, At the same time, most of the side tables 638, which are usually used in first-class cabins, are equipped. Compared with the seat unit 40 of Fig. 1-2 and the seat assembly of Fig. 25, the accommodation unit of Fig. 18-21 is assembled as a bed form, The accommodating unit of the twentieth invention provides a substantially horizontal sleeping surface. 22-27 show another passenger accommodation unit of the present invention. Most elements of cells in Figures 22-27, It is similar to the corresponding element of the unit shown in the figure above. therefore, For clarity, These components are represented by the same symbol plus 100. therefore, Via Example 76 593064 玖, Invention Description When the rear partition of the unit in Figures 18-21 is marked with the representative symbol 612, The rear partitions of the units in Figures 22-27 are marked with the representative symbol 712. therefore, As shown in Figure 22, Another passenger accommodation unit includes a shell 710 composed of two half shells 710a and 710b. The shell 710 includes a rear partition 5 712 and a front partition 714. It is interconnected by an interconnected side wall 716. Behind the rear bulkhead 712, The shell includes a hollow foot box 73 which has opposite side walls 732 and an upper wall 736, The upper wall 73 6 includes a substantially flat, Horizontal part 738, It is used as a side table for beverages for an adjacent seat. 10 The case 71 of Figure 22_27 is mounted on a plinth 760. The base 760 consists of a suitable aircraft class, Made of lightweight construction materials, It is typically the same material as the shell 710, And has a flat lower wall 762, It is fitted with a suitable fixture (not shown), Used to generally secure the base to the seatway. 15 The base 760 is formed with a recess 764, It is formed by an upstanding side wall 763 having an inwardly facing upper edge 765. The recess 764 extends from the front partition 714 into the foot box 73 under the entire seat. The foot box is configured at the floor height. The recess 764 contains a mattress or similar cushion or cushion suitable for forming a passenger bed. The recess is made in an appropriate shape to resist the slight tilt of the 20-pin aircraft in flight. So that the mattress is generally horizontal. The casing 71, which is juxtaposed with the front bulkhead 714, carries a movable stent 74, It can be on a substantially vertical axis, In the extended position shown in Figures 22 and 24, Move to an elevated storage location as shown in Figure 24B. Although it is obvious to those skilled in the art that 77 593064 玖, DESCRIPTION OF THE INVENTION Several mechanisms are used to achieve the movement of the carriage, However, an example of a suitable mechanism is a mutual fit on the inner surface of the front partition plate 714 and the bracket 74o. Tooth slide. Configure suitable devices, It is used to fix the bracket 74o in the up and down positions. 5 The shell 710 forms a passenger personal space 718, The 720 series includes a seat chassis 722 and a backrest 724. The backrest 724 is permanently fixed to the inner surface of the rear partition 712, At the same time, the seat chassis is pivotally connected to the inner surface of the rear bulkhead 712 at its rear edge 723, For deployment in one of the positions shown in Figures 22 and 24A, And one of the storage positions as shown in Figs. 23 and 24 ^. In the expanded position, Front edge 725 of the seat chassis 722, Is supported by the protruding part 2 which is formed inward on the shell 710, It is a support structure for the seat assembly 720. Under the seat chassis 722, After the shell 71, the partition 712 is formed with an opening 729, Access to the inside of the foot box 73 from the passenger space 718 is permitted. The 15 mattresses extend through the opening 729 below the seat assembly 72 and into the foot box 73. Located in the middle of the seat chassis 722 and the bracket 740, The recess 764 is covered by a removable floor panel 770, It is approved by a suitable airline, Made of load-bearing materials. The dummy floor panel is preferably connected to the interconnecting side wall 716, For deployment in one of the positions shown in Figure 22, To a storage location, This storage location allows the panel 770 to extend substantially perpendicularly and be continuous with the side wall 716. Place a solid component in the storage location to secure the panel. The first side wall 732 of the foot box juxtaposed with the seat chassis of an adjacent unit, 78 593064 玖, Invention Description It constitutes an outer recess 733, , A cushioned shelf 73 5 ′ is arranged at the same south degree as the seat chassis 722 of the adjacent unit, A laterally extending portion of the seat chassis 722 is provided. The Ganna unit 720 can thus be shown in a "seat 5-bit form '" as shown in Figures 22 and 24A, The seat chassis 722 is unfolded, As shown in Figures 23 and 24B, , , The seat chassis 722 is pivoted upwards in relation to its rear edge 723, The selective operation is used to equate the inner surface of the crime 724 in the storage location. In the form of beds, The removable floor panel 770 can be moved to the storage position. And raise the bracket 74 from its lower position to its raised position, As a result, the mattress located in the recess 764 of the bracket 76 is exposed. Raising the seat chassis 722 to its storage position, Department helps to get into the foot box 730, It also provides a more spacious personal space 718 within the shell 71 in the form of a bed. therefore, With the seat format shown in Figure 24A, A passenger train 15 sits in the seat provided by unit 720, If needed, It is possible to rest his or her feet on the bracket 74 in its lower position. If a passenger wants to sleep, He or she can thus stand and lift the seat chassis 722 to its position, As shown in Figure 24B. The bracket 74 can be raised to its raised position, The fake floor panel 770 can be removed. Passengers can then lie on the mattresses in recess 20, 764, His or her head is tied towards the front panel and extends his or her legs into the foot box 73. By "approximately your angle, E.g, About 45 degrees from the forward direction of the vehicle, And provides an overall length of up to 7 suction (2. 13 meters). The front partition 714 is used to protect the passenger's head when they are asleep, and the bracket 760 provides access to the passenger's personal space 79 593064 玖, an incremental part of the invention description, which is attractive to most passengers. The shell system located in the foot box can be made in an appropriate shape to provide-transverse seat extension P knife 735 'for-the seat chassis m of adjacent seats, and a large part of the temporary side table 738 for adjacent seats Used by. 10 15 In a variation of the other accommodating units in Figures 22-24, the seat chassis 722, in its storage position, is not related to the subsequent transfer of the side cans to the flat surface of the back 724 It can be arranged to slide between the front position 'as schematically shown in Figs. 26 and 8 and the retracted position shown in Figs. 25 and 26C with respect to shouting 7 !. In the retracted position, the seat chassis 722, or at least a large part of the seat chassis ⑶, can be accommodated in the foot box 73 at a position vertically spaced above the bed sheet. A plurality of mechanisms suitable for achieving the sliding movement of the seat chassis 722 are self-evident to those skilled in the art, such as a linear bearing arranged on the inner surface of the housing 710 adjacent to the seat chassis 722. Advantageously, the sliding mechanism may be configured with one or more pawls (not shown) for selectively stopping the movement of the seat chassis 722 in at least one intermediate position, such as shown in FIG. 26B. Therefore, in the fully extended position as shown in FIG. 26A, the unit can be assembled ergonomically for relaxation, while in the middle position as shown in FIG. 26B, the unit can be assembled. Fitted to provide, for example, a more upright passenger position suitable for dining or work. In the fully retracted position, when the seat is in the form of a bed, the seat chassis 722 is generally stored to allow access to the foot box 730. Shown in Fig. 27 is another variation of the accommodating unit shown in Figs. 22-24, in which the removable floor panel 770 is hinged to the interconnecting side wall 80 20 593064 发明, invention description 716, used in a Move between the unfolded position and the storage position as shown in FIG. 27. In the unfolded position, the panel generally covers the recess 764 horizontally to protect the mattress. In the stored position, the panel is substantially vertical. It is flat against the interconnect sidewall 716. The bottom side 772 of the fake floor panel is made of cushions with appropriate cushions, so that together with the mattress 764, it is provided in a sofa-like configuration; in the form of a bed, a passenger may charge him or her Sitting sideways on the bed 塾 π # on the bottom side 772 of the melon board 770. ίο 15 20 As shown in FIG. 28, it is another seat system of the present invention. The specific system in Figure 28 is specifically designed for use on the Boeing 747. The upper "lower deck" of the Meiji aircraft, but the system can be used on any passenger aircraft, especially in business grabs. The seat system of Fig. 28, on each of the upper and lower panels, includes a plurality of tree raft passenger accommodation units For example, the accommodating units in Figs. 18-21 or 22_27. Each of the accommodating units 8 'is juxtaposed with a guest side wall ㈣ and its direction is about 50 degrees with the longitudinal direction of the side wall 810, which is more than It's about 45 degrees' with the unit's back facing the wall 81, so that the seat is generally facing the interior. By facing the unit 800 inward, the passenger is compared with the front and back seats of the passenger. The grabbing system shows a less crowded appearance. Each unit has a generally triangular or trapezoidal extension box or space between the back of the unit and the side wall 810 of the passenger ship side by side. Generally, the aircraft passenger inspection wall is inside It is recessed, and therefore the extension box or "㈣" of each unit is extended into the recess formed by the wall. It can make the most effective use of the space in the inspection. Each unit includes components for the beds as described above, which are extended into extension boxes or spaces to maximize the available bed length. 81 593064 The invention is described in the floor plan of some aircrafts, and there is enough space to arrange one or more units towards the center of the cabin. As shown in Figure 28, it is for the Boeing 747-400⑧ aircraft. Lower deck. In this specific embodiment, units of the two central banks are configured, and the direction of each unit is an angle of about 45 degrees with the forward direction of the aircraft. The central units 800 are arranged in pairs, and each seat is generally facing the front of the cabin and facing outward, so that two units of each pair diverge from each other in the forward direction and in front of the rear pair of units, A quadrilateral space is formed substantially behind the unit. The quadrangular space 840 accommodates an extension box or space combined with 800 for each unit, and provides an extended bed length for each unit for the needle 10. Each unit 800 includes a hollow foot box of the type described above in relation to FIGS. 18-21 and 22-27. The upper wall of the mother foot can be used to provide a convenient side table or other The furniture unit is for another unit. In relation to Figures 29A to 29C, a passenger vehicle of the present invention is used, for example, 15 such as an aircraft, the second passenger seat assembly 900 includes a fixed support, and the structure is generally represented by the symbol 9 丨〇 Marking, used to support the seat assembly off the floor F of the vehicle. The support structure 9 includes a member adapted to attach the seat assembly to a floor. For example, where the seat assembly 900 is mounted on an aircraft, the support structure 910 typically includes one or more fixtures for use in attaching the seat assembly to the floor of an aircraft cabin, typically Types of seats dominate. Compared with the seat unit 40 in FIG. 2 or the first seat assembly in FIGS. 3-5, the supporting structure of the second seat assembly 900 may include a base or axillary armrest for attaching to the seat. track. The support structure 910 further includes a lift passenger support member 912, 914, each of which is generally 82 593064 mm. The invention description has a flat, horizontal upper surface (to offset the slight tilt of the aircraft during flight). . The passenger support members 912, 914 are spaced apart to form a cavity 916 within the support structure. The support structure 910 can be made of any suitable aircraft-grade structural material known to those skilled in the art. The support structure may be skeletal or may include one or more solid walls. Typically, the support structure is made of a lightweight synthetic material, but the aforementioned fixtures used to secure the support to the seatway or other floor in the aircraft may include one or More light steel or aluminum reinforced beams or bases. 10. The chamber 916 accommodates a passenger seat, and is generally marked with a representative symbol 920. The passenger seat 920 is generally supported by a support structure 910, and includes a backrest element 922 and a seat chassis element 924. The backrest element and a seat chassis element 922 and 924 are connected to the supporting structure 91 through a seat moving mechanism, which is generally marked with a representative symbol 930. 15 The seat moving mechanism 930 includes two similarly irregularly shaped polygon plates 932, which are mounted on either side of the seat 92. It should be noted that in the side views of Figures 29A to 29C, only one of these plates 932 can be seen. Each polygonal plate 932 is formed with a generally linear, elongated slit 934 that is juxtaposed with one edge 935 of the plate. Juxtaposed with a relative edge% 6 20, the plate 932 carries two spaced, inwardly facing lugs% ?. A straight line between the lugs 937 forms an acute angle with the linear slit 934. It is juxtaposed with the other edge 939 of the plate 932, which substantially extends laterally between the one and the opposite edges 935, 936. The plate 932 is connected to one end of a two-piece flail stem device 940 . The link assembly includes an 83 593064 玖, a first member 941 of the invention, which is pivotally connected to the plate 932, and a second member 942 which is pivotally connected to the first member 941 at one end to constitute The knee joint 943 is connected to a fixed pivot point 944 on the support structure 910 at the other end. 5 The seat moving mechanism includes a member for connecting the seat chassis to the backrest so that the lower end portion of the backrest remains continuous with the rear end of the seat chassis, while allowing the seat chassis and the backrest to pivot relative to each other. The linear slit 934 has upper and lower ends 954, 955, and slides into a lug member 95 1 which protrudes from individual sides of the seat chassis 924 10. Juxtaposed to its front end 925, the seat chassis 924 is pivotally connected to each side, and is pivotally connected to one end of a linear post 961 at a pivot point 952. The linear strut 961 is pivotally connected to a sliding table frame member (not shown) at the other end 962, and the member is connected to a support structure 910 located below the seat chassis 924. The sliding table frame member is movably mounted to the supporting structure 15 so that the sliding table frame member can be moved between an upper position corresponding to FIGS. 29A to 29C and a lower position corresponding to FIGS. 30A and 30B. . A suitable biasing member is configured, for example, such as a bomb, a gas pillar, or the like, for biasing the moon frame member into the upper position. A selectively releasable mechanical fixing device is usually provided at the same time for fixing the sliding table frame member 20 in its position. The βHai linear strut 961 is swingably mounted to the sliding table frame member so that it can lie forward in a generally upright position as shown in FIG. 29A, and as shown in FIG. 29C. Shake between positions. The lugs 937, which are spaced apart on the polygonal plate 932, mesh with the -curve 84 593064. Description of the invention The track 971 is fixedly fastened to the individual sides of the backrest 922. As can be seen from Figures 29A to 29C and 30A to 30C, the curved track 971 is conveniently formed in an elongated plate member 972 which is attached to the back side. The curve's execution path 971 has upper and lower ends 973 and 5 974, respectively. Related to FIG. 29A. When the seat 920 is arranged in the upright or "dining" position, the two-part linkage set 94o series Is in an extended form, so that the first and second members 941, 942 are substantially coplanar with each other, and the two first and second members 94 !, 942 are generally tied upward from the pivot point 10944 And extend forward. The plate 932 extends backward from the attachment point to the first link member 941 and is oriented so that the linear slit 934 extends upward and backward. The backrest portion 922 is in an upright position, and the spaced-apart lugs are arranged at the ends below the curved track 971. The direction of the seat chassis is generally horizontal '(during flight) and the lugs 951 are disposed at the end 954 above the linear slit state 15. The sliding table frame member (not shown) is disposed in the above position as described above, and the direction of the swingable linear support 961 is substantially vertical. The seat chassis 924 is thus tied rearwardly between the two passenger support members 912, 914 in the chamber 91-6. The seat chassis 924 has an upper surface 926, which is suitably fitted with a 20-piece and used as a seat element. Similarly, the backrest element 922 has a front surface 923, which is suitably mounted as a seat element. Preferably, the front surface 923 of the backrest element is decorated to cooperate with the upper surface 926 of the seat chassis 924. Among them, the passenger wing member 914 is arranged in front of the seat 920 'and used as a fixed legrest portion, which is similar to the description of the invention. The legrest portion 928 has an upper surface 929. «The linear pillar 961 is operatively and selectively operable with a fixed motor transmission (not shown) capable of driving the pillar 961, as described above, in the upright position in Figure 29A and Figure 29C The five forward tilted positions are shaken in relation to the upper end portion 962 thereof. A suitable user control (not shown) is provided in the seat assembly so that a passenger using the seat can operate the fixed transmission. The backrest portion 922 has a rear surface 921 which is substantially planar. When the seat system is upright as shown in FIG. 29A, the rear surface 921 is separated from the passenger support member 912 by a small gap 913. The rear surface 921 carries a mattress portion (not shown) for use as a part of the bed. The mattress P knife is attached to the rear surface 921 of the backrest portion 922 so that when the backrest is upright, it is not Remove the mattress part. The passenger support member 912 also has an upper surface 911 which supports a mattress portion. A movable-filled passenger support member 915 is pivotally connected to a front side of the passenger support member M " ^ Side 4: 917. The filling member 9 i 5 is generally linear and has an upper surface 918 that carries a mattress P knife (not shown). The filling member 91-5 is slidably connected to the back surface 921 of the backrest element M2. As shown in Figure 29A, in the upright position, the filling member 915 extends substantially upright between the fixed passenger support member 9 丨 2 and the backrest element 922 of the seat 920 in the gap 913. . In addition to the fixed transmission motor used to drive the linear strut 961, it is equipped with a selectively operable motorized transmission for swinging the second part of the two-part linkage set 940 in relation to a fixed pivot point 944. II 86 593064 发明, invention description link member 942. The second link member 942 includes a rearwardly extending connecting portion 945 (see the first pass) for connecting with another transmission motor (not shown). At the same time, the user control device can be used to operate the mechanical fixing device 5 and release the seat chassis from the upper position while operating the second transmission device. When the seat system is upright as shown in FIG. 29A, the seat system can use 2 operating ㈣ drive motors to correlate the other end portion and swing the linear support 961 forward to recline the seat, while A sliding table frame member (not shown) supports the linear post 961 in its upper position. By shaking the linear strut 961 forward, the seat chassis element 924 of the seat is pulled forward in the chamber system, and the lug 951 slides from the upper end 954 along the slit 934 toward the lower end 955 . The forward movement of the seat chassis at the same time caused the lower end of the scapegoat 922 to move forward. The backrest part is restricted and is in the curved U-line track 971. The two tracks are moved along a predetermined path by the stagnation of the lugs 937. The 97K is made in an appropriate shape to cause the backrest milk to move to the seat chassis. And gradually lean back. When the seat is tilted back, the lug 937 follows the curve 971, moves through a middle position as shown in Figure 29B, and the two lug milk 20 is close to the upper end of the curved track 971 973, at which point the seat cannot be moved any further, and the seat is in the position of one of the heirs or leaners as shown in Figure 29C. It should be noted that the fixed action of the fixed transmission motor allows the seat Stopped and fixed at any desired intermediate position between the two ends represented by Figures 29A and 29C. 87 593064 发明 Description of the invention When a passenger using the second seat assembly 900 of the present invention is a passenger It is hoped that the sleeper seat assembly can be converted into a bed. Passengers operate the user control device to release the seat chassis from its upper position and cause the first motorized actuator to be as shown in Fig. 30a. In relation to the pivot point 944 shown in the figure, the second link member 942 of the link group device 940 is rocked back 5 times. When the second link member 942 is rocked backward, it is between the first and second link members The knee joint between 94 J was interrupted, allowing the first link structure 941 is related to the knee joint member 943 and shakes to the back and down, so that the back of the seat 920 moves forward in the chamber 916 and pivots forward 10 times from its upright position. When When the backrest element 922 is pivoted forward, it is pushed downward on the seat chassis portion 924, and is thus induced to move downward on the sliding platform frame member (not shown) to resist the action of the biasing member. Second The continuous backward movement of the connecting rod group member 942 causes the polygonal plates 2 and the backing element π] to move downward toward the floor F of the vehicle until, as shown in FIG. 303, the rear surface 921 of the guilty element 922 It is arranged substantially horizontally (during flight) and is coplanar with the passenger support members 912 and 914. The link group member 940, the polygon plate 932, the curved track 971, and the lug 937 are arranged so that they are as shown in FIG. 30B In the form of bed shown, the upper end of the backrest element is abutted against the rear edge of the forward passenger support member 914 to form a continuous surface with it. Equipped with suitable, releasable fixing devices, For backrest 922 Moreover, as can be clearly seen in FIG. 3A, when the backrest element 922 is shaken in the cavity 916 and moved forward, the filling member 915 follows the backrest element. The surface 921 slides and is induced or allowed to pivot forward until 88 593064 发明, the description of the invention 'as shown in the 3GB diagram, when the backrest element is generally horizontally arranged, the filling member 915 is placed on the passenger support member 912 and the back The backing element is formed between the rear surface 921 and the bridging part so that the upper surface 911, 918, 921, the filling member 915 and the backing element 922 of the passenger wing member 912 are generally octahedral and constitute a continuous surface. It should be noted that the mattress portion carried by the passenger support member 912, the filling member 915, and the rear surface 921 of the backing element 922 constitute an elongated mattress for passengers to sleep on. In addition, the upper surface 929 of the passenger support member 914 in front of the seat 920 can simultaneously carry a quilt portion to further extend the bed composed of the seat in the form of a bed in FIG. 10. The seat assembly of the present invention is allowed to form a continuous bedding surface with a length of at least 78_80 inches (1. 98_ 2. 032 meters). In some cases, the bed formed by the upper surface 9U, 918, 921, 929, the filling member ... 5 of the passenger support member 9ΐ2, M #, and the rear surface 921 of the backrest element 922 may have a length exceeding 15 inches. (2. 16 meters). In order to return the seat assembly 900 to a seat form, the second motor transmission is actuated to swing the second link member of the two-part linkage set 940 forwardly in relation to the fixed pivot point 944 942, thereby causing the first link member 941 to swing backwards, and in turn, causing the polygonal plate 932 to swing backwards and upwards, and gradually returning the backrest element 922 to its upright position. When the backrest element 922 returns to the upright position, the seat chassis element 924 is allowed to return to a position above the load bearing member (not shown) under the influence of the biasing member (also not shown). When the seat chassis returns to its upper seat position, the mechanical fixing member is automatically re-engaged to hold the seat in its upper position. It can be seen from examining the figures 29A to 20C that the upper surface 911 of the passenger support member 912 and the upper surface 918 of the filling member 915, when the seat assembly is assembled in the form of a seat, constitutes a Convenient recess 5 of 98. The recess 980 is at least partially hidden from view by the backrest portion 922 of the seat 920. Therefore, the recess 98 may be used for storing bedding materials such as pillows, duvets, and the like, for example. When the seat assembly is moved to the bedding form in Fig. 30B, the passenger can easily take out bedding material and unfold the surface of the bedding composed of the components of the seat assembly as described above. Another advantage of the passenger seat assembly 900 described previously is that the front surface 923 of the Λ element 922 and the upper surface 926 of the seat chassis element 924 can be particularly cushioned and covered for use as a seat element. Therefore, for example, the accusation element and the chassis element 922, 924 can carry 15 layers of foamed plugs, which are specially shaped and used as seat members. The texture, pattern, and / or color design of the cushion, and the decorative material used to cover the front surface 923 of the backrest element and the upper surface 926 of the seat chassis element may be materials specifically selected for use as a seat. In contrast, the mattress portion, the filling member 915, and the back surface 921 of the backrest element 922 carried by the passenger support member 912 may be specifically designed for use as bedding materials. Therefore, the internal pop-up mattress part or foam cushion layer used is specially made in an appropriate shape, which brings maximum comfort to passengers when using the seat as a bed. In particular, the materials and fabrics used to decorate the mattress part are available in a variety of colors, textures, colors, etc., which are particularly suitable for use as bedding materials 90 593064, invention description. The bedding material used for the decoration part and the material used to decorate the seat assembly ^ The seat parts have quite different appearances from each other. However, it can be seen that when the seat is assembled and used as a seat, most of the bedding material is concealed by the backrest element 922, and only the seats of the seats constituting the intersecting part of the seat can be seen. section. Similarly, when the seat is reassembled and used as a bed, the front surface of the backrest element and the upper surface of the seat & melons 7G are generally hidden and cannot be seen, and only the bedding material can be seen. It includes a mattress section on a passenger support element 912, a filling member 915, and a rear surface 921 of the backrest element 922. 15 In a passenger inspection of a vehicle, for example, the installation of a plurality of passenger seat assemblies of the present invention on an aircraft can be used to bring the aircraft to a bed or seat configuration according to most of the seat assembly systems. Observe two different things: feel the appearance or atmosphere. Therefore, most of the passenger seat assemblies during the daytime flight, or during the daytime portion of a long-lasting flight, are configured as a seat, as shown in one of the WC diagrams. The bedding material is generally hidden so that only the seat surface of the assembly can be seen. Of course, the seat assembly can be decorated to any desired design, but, for example, the seat assembly is cushioned and brought to the recording room with a private club view. For example, the upper surface 926 of the seat chassis element 924 and the back surface element 923 may be fitted with leather dumplings. During the night flight, either in the night portion of a long-term flight, 'most or all of the seat assemblies are fitted in the form of beds, as shown in the figure below.' The upper part is hidden, and only the passenger support member 912, the upper surfaces 911, 918, 921, 929, the stuffing member 915, and the bedding material supported by the backrest 91 20 593064 玖, the invention description element 922 can be seen. The material used to decorate the mattress portion has a significantly "softer" appearance than the material used to decorate the seat side of the back of the backrest element 922, in order to give the passenger cabin an attractive fit for sleep , Laid-back atmosphere. Figures 31 and 32 respectively show two different seating systems, each of which includes a plurality of seating assemblies previously related to the type shown in Figures 29-30. In Figure 31, an aircraft cabin is formed in particular by two opposing curved walls 1001, 1002. It is well known to those skilled in the art that each of the walls 1001, 1002 is generally recessed 10 on its inner surface. A row 1029 of the 15 passenger seat assemblies 900 of the present invention is arranged in parallel with each of the walls 1001, 1002. Regarding the seat assembly 900 represented by one of them, each seat assembly 900 forms a series of abstract vertical axes indicated by a representative symbol 1012. The seat assembly 900 is oriented in a pair of acute angles with respect to the adjacent cabin walls 1001, 1002. Figure 31 also shows an abstract "forward" axis 1014 juxtaposed with the wall 1001. It should be noted that the "forward, axis 1014" facing the front of the aircraft is actually not precisely oriented forward in relation to the forward direction of the aircraft, but the direction is generally the forward and backward direction of the adjacent side wall 100i Parallel, while ignoring the slight bend on the side 11001. The direction of each seat assembly 900 is between the abstract longitudinal axis 1G12 of the seat assembly and the abstract "forward" axis 1014 of the aircraft passenger grab. An alpha angle of about 40 degrees is formed. Each seat assembly is configured so that the passenger support member 912 extends into a recess formed by the side wall surface 1002 and the characteristic of the side surface 1002. Seat 92_About the passenger inspection system configuration facing 隔板 and towards Θ W and the low privacy partition 927 constitutes the front end portion surrounding the passenger support member 914, and 俾 surrounds each seat to form 92 20 593064 发明, description of the invention Into a passenger personal space. By positioning each seat assembly so that the passenger support member 912 extends into the recess formed by the recessed sidewalls 1001 and 1002, the largest usable space is formed in the aircraft cabin. It can be seen that, when the seat is configured as a bed, the passenger support member 912 is only used by the passenger, so a full-height headroom is not required above the passenger support member 912. A suitable privacy partition is arranged between adjacent seats, and a space 1015 adjacent to the mother-seat assembly and located behind the passenger support member 912 of the adjacent seat assembly is shown in FIG. To provide a surface with a seat height of 10 degrees, use it as a cocktail table or similar device. Where the cabin space permits, in addition to 900 rows of seat assemblies juxtaposed with the cabin walls 001, 002, one or more seat assemblies 900 of the Central Bank of China 1030 can be installed. Figure 31 shows a cabin equipment, which is a seat assembly of 1030 Central Bank of China. Within each central bank 1030, as described above, the seat assembly 900 series is positioned at an acute angle to the forward and backward axis of the aircraft cabin. The seat assembly 900 is arranged in two rows at the same time. In each row, the seat assemblies are arranged back-to-back. Therefore, the passenger supporting members 912 adjacent to the seats in the same row are continuously arranged with each other, so they are in the same row. The passenger supporting members 912 connected to the seats are arranged continuously with each other, and when the seats are in the form of seats, they are generally hidden by the backrest elements of the side-by-side seats 920 so as not to be seen. Fig. 32 shows various types of seating systems applicable to a seat assembly 900 including three rows of 1129 and 1130, which includes two rows of 1129, juxtaposed with two longitudinal walls of the cabin 1101, 1102, and a single central bank. Compared to the arrangement shown in figure 93 593064 玖, description of the invention in Figure 31, the seat assembly 900 in each row 1129 juxtaposed with one of the cabin walls 1101, 1102 is oriented so that the seats are related to Guest grabbing is facing forward and inward. The seat assembly within 113 ° of the Central Bank is also configured to face forward and side to side. Each seat assembly is formed between the abstract longitudinal axis 1112 of the seat assembly 900 and the front and rear axis 14 of the cabin, forming a pair of acute angle β of approximately 49 degrees. Figures 33A to 33C show a third passenger seat assembly according to the present invention. The components of the third passenger seat assembly in FIGS. 33A to 33C are similar to the corresponding components 10 of the assembly in FIGS. 29A to 29C and FIGS. 30A and 30B, so corresponding symbols are used, but Add "12" before the symbol to replace "9". Therefore, the supporting structure 1210 of the third seat assembly in FIGS. 33A to 33C corresponds to the supporting structure 910 of the second seat assembly in FIGS. 29A to 29C. The third seat assembly in FIGS. 33A to 33C includes a support structure, generally designated 15 as a representative symbol 1210, for supporting the assembly to leave the floor F of a vehicle, such as the floor of an aircraft cabin, for example. Similar to the second seat assembly in Figures 29 and 30 above, the third seat assembly in Figures 33A to 33C includes two elevated, auxiliary passenger support elements 1212, 1214, which are spaced apart and opposed to each other. A cavity 1216 is formed in the supporting structure. The chamber 1216 2o accommodates a seat, which is generally designated by a representative symbol 1220. The seat includes a backrest element 1222 and a seat chassis 1224. The seat chassis 1224 has a 1J 'portion 1225 and a rear end portion 1223, and the rear end portion 1223 is pivotally connected to a lower end portion 1226, which is one of the crime elements 1222. The seat chassis 1224 is movably connected to the support structure 94 593064 through a seat moving mechanism (not shown). Invention description 1210 allows the seat chassis 1224 to be inside the chamber 1216, substantially as shown in FIG. 33A. The upper position shown moves vertically from the lower position shown in Figure 33C. Equipped with a suitable dust deflecting member (not shown) for biasing the seat chassis 1224 into the upper position, and equipped with a selective operation 5 fixing device for fixing the seat chassis 1224 in the upper position. The backrest element 1222 is tied to a fixed pivot point 1230 and is pivotally connected to the support structure 1210. The backrest element 1222 has a rear surface 1221, which includes an extension portion 1231 at an end portion 1226 below the backrest element 1222. When the backrest element 1222 is in an upright position, the extension portion 1231 extends downward 10 Cross the fixed pivot point 1230. The upper surface of the seat chassis element 1224 and the front surface of the backrest element 1222 are fitted and covered with a cushion specially designed for use as a material for the seat. The passenger support element 1214 is spaced apart from the square in front of the seat 1220 and can be used as a footrest element 1228 when the seat 1220 is in the upright position shown in FIG. 33A. The passenger support element 1212 is arranged behind the backrest element 1222 and is separated from it by a small gap 1213. The back surface 1221 of the backrest element 1222 is substantially flat and carries a first mattress portion (not shown), which is specifically designed and decorated for use as a bedding element. The passenger support element 1212 has an upper surface 2012U, which simultaneously carries a mattress portion. The backrest element 1222 and the passenger support element 1212 form a recess 1 280 behind the guilty element 1222 for storing bedding materials such as pillows, duvets, rugs, blankets, and the like. An advantage of the third passenger seat assembly of the present invention is that when the scapegoat is captured in an upright position as shown in FIG. 33A, the concave 128 胄 is hidden by 95 59306464, the invention description is not seen , So neatly hide any bedding material stored in the recess. The backrest element 1222 is related to the fixed pivot point 1230 from the upright position in FIG. 33A and pivoted to a bed position 5 in FIG. 33C. The backrest element 1222 and the pivot point 1230 are designed to use passenger support elements 1212 and 1214, so that in the bed position, the rear surface 1221 of the backrest element 1222 is configured to be continuous with the two passenger support elements 1212 and 1214. To form a surface that is generally flat and continuous. In the bed form in FIG. 33C, the second mattress portion carried by the passenger support element 1212 on the top surface 1011 and the first mattress portion carried by the backrest element 1222 and the rear surface 1221 are closely adjacent to each other. Or almost abutting to form an extended bed for sleeping passengers. The upper surface 1229 of the passenger support element 1214 also forms an extended surface as a bed. Compared with the first and second seat assemblies described above, according to the third 15-seat assembly, it can be used to form a bed, and its total point-to-point length is at least 78-80 inches (1. 98_2 · 032 meters), and in some cases, at least 85 inches (2. 16 meters). The movement of the backrest element 1222 between the upright position in Figures 33A and 33C and the bed position can be motorized (not shown) and can be adjacent to the seat. ^ Fine configuration. 20 Suitable user-operable control devices. Not shown at the time. ) To enable passengers to control the movement of the seat. When the seat system is in the upright position as shown in Fig. M, the system can remove the fixing mechanism to release the seat chassis from its upper position f, and actuate the motor transmission device to cause the backrest element to be related to the fixed system. Pivot point] 230 shake forward. When the backrest element 1222 is rocked forward 96 593064 玖, description of the invention ′ It is abutted against the seat chassis element 1224, and the seat chassis element 224 is pushed downward in the chamber 1216 to resist the function of the aforementioned biasing member. In the bed position shown in Fig. 33C, the seat chassis element 1224 is completely hidden by the backrest element 1222. Therefore, compared with the first and fifth seat assemblies described above, the front surface of the backrest element 1222 and the upper surface of the seat chassis element 1224 can be covered with a material, resulting in a visual appearance and an atmosphere of inspection, and used for decoration. The back surface 1221 of the backrest element 1222 and the bedding accessories of the bedding accessories 1212 on the top surface 1211 of the passenger support το 1212 are completely different from the visual and guest atmosphere. When the backrest element 1222 10 is upright, the seat surfaces of the backrest element 1222 and the seat chassis element 1224 can be seen, and the bedding surface system of the back surface 1221 of the backrest element 1222 and the upper surface 1211 of the passenger support element 1212 is hidden. . On the other hand, when the seat is in the bed form in FIG. 33C, the seat surfaces of the backrest element 1222 and the seat element 1224 are hidden, and the bedding surfaces 15 1221 and 1211 can be seen at the same time. According to a special point of view of the second and third seat assemblies described above, the backrest element 922; 1222 has a first seating surface 923; a seat that is part of the upper surface 926; a seat chassis 924; 1224 and-opposite bed surface milk; 1221 is used to form a passenger support element 912, 914; 1212, 1214 with 20 or more other auxiliary. The passenger seat assembly of the present invention is therefore particularly advantageous, as the basin allows the provision of a long bed for passengers in an aircraft cabin or other vehicle, and can even provide a height that is more than redundant at the smallest seat spacing 2. 032 meters) tall passengers ride comfortably. According to the present invention, by 97 59306464, invention description 10 15 20, a seat assembly is arranged side by side with a recessed bulkhead, and rear passenger support elements 912, 1212 are arranged adjacent to the bulkhead, so that the cabin can be used efficiently. Free space within. In a seat form, the 'backrest element 922; 1212 series. After the passenger support element 912 M212 constitutes a recess 980; 1280, which can be used to neatly hide bedding materials, such as small blankets, blankets, pillows, etc. The surface of the backrest element 922; 1212 and the surface of the scrap can respectively cause different visual appearance, so that in a passenger grabbing facility, including a plurality of seat assemblies of the present invention, when all or most of the seat assemblies are configured When in the seat form, a first cabin atmosphere can be achieved, and when all or most of the seat assemblies are configured in a bed form, a second, different guest atmosphere can be achieved. Furthermore, the seat and bedding surfaces can be used separately for their specific applications. So 'for example, the seat surface of the backrest element 922; 1212 can be equipped with foam cushions or the like, and is specially shaped to be used as a seat element, while the bedding surface of the backrest part can be equipped with -bed Partial or other comfort, elastic layers are specially made in suitable shapes for use as bed elements. Another advantage of the seat assembly of the present invention is that, in the form of a bed, the seat chassis element 924; 1224 is completely, or substantially hidden by the backrest element 922; 1212, so that the material used to cover the seat chassis element i The appearance 'does not damage the appearance and atmosphere provided by the bedding material. Preferably, the seat assembly according to the present invention includes a leg rest portion separated from the front of the seat 92 ′, and is extended on the surface of the bed in the form of the leg pieces. [The diagram is simple and clear.] Plane, rough plane The first figure is a cut of a front part of an aircraft fuselage 98 593064. The invention is an explanatory diagram showing a system of a plurality of individual seat sheets of the present invention. Yuan seat Figure 1A is an enlarged view of the part of Figure 1, showing the seating unit. Shown three adjacent 15 20 Figure 2 is an isometric view of the third adjacent seat unit of Figure ία. In Figure 2, one of the seating units is shown as an upright seat, the other is shown as a reclining seat, and the third is shown as a bed. Figure 2A shows a part of a building structure of an individual seating unit of the type shown in Figure 2 with the movable seating elements removed. Fig. 3 is a schematic side view of a first passenger seat assembly for a vehicle according to the present invention, showing an upright seat form. Figure 4 is another schematic side view of the first passenger seat assembly of Figure 3, showing a fully reclined seat form. Figure 5 is another schematic side view of the first seat assembly in Figures 3 and 4, showing a bed form. Fig. 6 is an isometric view of a part of the first-seat assembly in the form of an upright seat in Figs. 3 to 5 in which the seat cushion is removed. Figure 6A is a side view of an offending element of the seat assembly of Figure 6 of the component. Figure 6B is an isometric view of the backrest element of Figures 6 and 8. ^ The figure is another special view of the first seat assembly in the part shown in Fig. 6, in which the seat assembly is in the completed reading seat form. The paste system is another part of the seat assembly of Figs. 6 and 7-发明, description of the invention Angular view 'where the seat assembly is in the form of a bed. Fig. 9 is an isometric view of a seat moving mechanism of the first seat assembly in the parts of Figs. 3 to 8, which are shown in the form of a bed. Fig. 10 is a side view of the seat moving mechanism of #A # $ 丨 77, which is a part of Fig. 9, which shows the seat form. Fig. 11 is another side view of the seat moving mechanism of the kazakhstan production and production of the p-knife in Figs. 9 and 10, which shows a bed form. Figure 12 is an enlarged isometric view of the seat-moving mechanism of Figure 1-9. 10 Figure 13 is an isometric view of the rear reclining mechanism of the part of the first seat assembly in Figures 3 to 8. Fig. 14 is an isometric view of the seat changing sub-mechanism of the part of the first seat assembly of Figs. 3 to 8, which shows the form of a bed. 15 Figure 15 is another isometric view of the seat conversion sub-mechanism of the part of Figure 14, which shows the-seat form will be a worm (gift) from-the corresponding position (Li m gear) Remove to allow the seat change sub-mechanism to be manually moved between the seat and the bed form. Fig. 16 is an enlarged, cross-sectional side view of one of the seat changing sub-mechanisms of the parts of Figs. 14 and 15; The 20 buckle diagram is a cross-sectional, schematic plan view of another seat system of the present invention. FIG. 18 is a first isometric view of a passenger accommodating a single open + valley, Na Zaofan, which is a seat type. Figure 19 is an isometric view of the passenger accommodation unit of Figure 18 100 593064 64, description of the invention The figure shows a bed form. Figures 20A-20C are schematic side views showing the passenger accommodation units of Figures 18 and 19 switching between bed and seat formats. Fig. 21A is a schematic, isometric view of the passenger accommodation unit of Figs. 18 and 19, showing a passenger using a seat in a seat form. Figure 21B is a schematic, isometric view of the passenger accommodation unit of Figures 18 and 19, showing a passenger using a seat under a bed. Fig. 22 is an isometric view of another accommodating unit of the present invention, in which a seat form is shown. 10 Figure 23 is an isometric view of the passenger accommodating unit of Figure 22, shown in the form of a bunk. Figure 24A is a schematic, isometric view of the passenger accommodation unit of Figures 22 and 23, showing a passenger using a seat in a seat format. Figure 24B is a schematic, isometric 15 view of the passenger accommodation unit of Figures 22 and 23, showing a passenger using a seat under a bed. Fig. 25 is an isometric view of a variant of the passenger accommodation unit of Figs. 22 and 23 ', which includes a sliding seat chassis. Figures 26A-26C are side views schematically showing different positions of the sliding seat chassis. 20 Figure 27 is an isometric view of another variation of the passenger accommodation unit of Figures 22 and 23. Figure 28 is a schematic, cross-sectional plan view of the upper and lower decks of a front part of an aircraft fuselage, showing another seat system of the present invention applied to a Boeing 747-400⑧ aircraft and a main bow. 101 593064 (ii) Description of the invention Figure 29A is a schematic side view of a second passenger seat assembly according to the present invention, and the seat assembly shown therein is in a dining position. Figure 29B is Figure 29A-Gong Anguang "^ 1 ^. A heart-side view of a passenger seat assembly, shown in a central reclining position. 5 Figure 29C is a schematic side view of the second passenger seat assembly of Figures 29A and 29B, with the figure shown in a fully reclined position.

第30A圖係為第29A至29C圖之第二乘客座位總成的一概略側視圖，其中所示係處在另一中間轉換位置。第30B圖係為第29A至29C圖以及第30A圖之座位總成 10的一概略侧視圖，其中所示係處在床舖形式。第3 1圖係為包括本發明之複數的乘客總成的另一座位系統的一概略平面圖。第32圖係為包括本發明之複數的乘客座位總成的另一座位系統的一概略平面圖。 15 第W A圖係為本發明之第三乘客座位的一概略側視圖Fig. 30A is a schematic side view of the second passenger seat assembly of Figs. 29A to 29C, and the illustration is in another intermediate shift position. Fig. 30B is a schematic side view of the seat assembly 10 in Figs. 29A to 29C and Fig. 30A, which is shown in the form of a bed. Figure 31 is a schematic plan view of another seat system including a plurality of passenger assemblies of the present invention. Fig. 32 is a schematic plan view of another seat system including a plurality of passenger seat assemblies of the present invention. 15 Figure W A is a schematic side view of the third passenger seat of the present invention

’其中所示之座位總成係處在一座位形式。第33B圖係為第33A圖之第三座位總成的一概略侧視圖，其中所示係處在一中間位置。第3 3 C圖係為第3 3 a及3 3 b圖之第三總成的一概略正視 20圖，其中所示係處在一床舖形式。【圖式之主要元件代表符號表】 10…飛機機身 15.··鼻部分 Π···前端部 20…乘客客艙 12…刚端部部分 21…乘客客艙 102 593064 玖、發明說明 22…公用區域 23…廚房 24.. .乘客盥洗室 2 6…表面部分 27…間隙 28…表面部分 29···行 3 0...地板或甲板 32…座位執道 3 4...座位執道 36…空間 38…二隔開點 39.. .單一點 40…座位單元 4 2...支樓結構 43.. .座位外殼 44··.凹部 45.. .第一凹入橫向邊緣 46…點 47."三角形的表面 48.. .三角形的表面 49.. .第二橫向邊緣 5 0...轉動軸 51.. .前端部 5 2…後端部 53.. .相對側邊 54.. .相對側邊 60.. .拱形隔板 61.. .凸面的後部分 62.. .線性前部分 65.. .軟墊凳 66.. .上表面 67.. .坐墊 68…隱私隔板 71.. .座位底盤 72…背靠 73.. .前表面 74.. .後表面 75…臂靠 76.. .充填元件 80.. .座位模組 13 0...地板 140.. .第一乘客座位總成 142.. .支撐結構 143.. .座位外殼 144…凹部 147…第一上表面 148…第二上表面'The seat assembly shown therein is in the form of a seat. Fig. 33B is a schematic side view of the third seat assembly of Fig. 33A, with the middle position shown. Figure 3 3 C is a schematic front view of the third assembly of Figures 3 3 a and 3 3 b. The figure is in the form of a bunk. [Representative symbol table of main elements of the drawing] 10 ... Aircraft fuselage 15 .... Nose section Π ... Front section 20 ... Passenger cabin 12 ... Rear end section 21 ... Passenger cabin 102 593064 发明, Invention description 22 ... Area 23 ... Kitchen 24 ... Passenger toilet 2 6 ... Surface section 27 ... Gap 28 ... Surface section 29 ... Row 3 0 ... Floor or deck 32 ... Seat lane 3 4 ... Seat lane 36 ... space 38 ... two separated points 39 .. single point 40 ... seat unit 4 2 ... office structure 43 ... seat shell 44 ... recess 45 ... first concave lateral edge 46 ... point 47. "Triangular surface 48 .. Triangular surface 49 .. Second lateral edge 5 0 ... Rotary axis 51 .. Front end 5 2 ... Rear end 53 .. Opposite side 54. .. Opposite side 60 .. Arched partition 61 .. Convex rear portion 62 .. Linear front portion 65 .. Upholstered stool 66 .. Upper surface 67 .. Cushion 68 ... Privacy partition Plate 71 ... Seat chassis 72 ... Back 73 ... Front surface 74 ... Rear 75 ... Arm 76 ... Filling element 80 ... Seat module 13 0 ... Floor 140 ... First passenger seat assembly 142 ... support structure 143 ... outside the seat Recessed portions 144 ... 147 ... 148 ... second upper surface of the first upper surface

103 593064 玖、發明說明 151.. .前端部 152.. .後端部 153.. .相對側邊 154.. .相對側邊 165.. .軟墊凳 166.. .上表面 167.. .坐墊 169.. .平坦上表面 201.. .上端部 202.. .前端部 203.. .後端部 204…後壁 205.. .侧壁 206.. .側壁 221.. .耳軸 222.. .旋轉軸承 223.. .搖動板 224.. .第一邊緣 225.. .第二邊緣 226.. .面向夕卜之表面 227···内表面 228.. .上端部 229.. .下端部 230.. .第一扭力管 231.. .相對端部 232.. .相對端部 23 5…凹部 241.. .連桿 242.. .端部 243···端部 244.. .端部 245…搖臂 246···端部 250···扭力管 251.. .端部 252···端部 253.. .軸承 260.. .中空蝸輪外殼 261.. .底部表面 262.. .内腔室 263.. .上壁 265…凸耳 270…蜗桿 271.. .蝸輪 272·.·推力軸承 273.. .蝸桿外殼 275…心軸 280.. .電氣馬達 104 593064 玖、發明說明 281...馬達外殼 322…滑件部分 282...連桿 324...翼部分 283…連桿 3 2 5...外表面 284...端部 326...内表面 285···端部 329...水平自由接頭 286...第二端部 330...膜片 301···凹部 331...橫向側邊緣 302…下端部 332...橫向側邊緣 303…上端部 333...後端部 304...線性螺桿 334...前端部 305...上端部 341...上端部 306...下端部 342...懸垂桿 307...軸承 343...端部 308...轉動軸承 345...滑件 310...齒輪外殼 350…滑道 311...斜齒輪 351...上端部 312…傳動軸 352...下端部 313...端部 354...下端部 314…端部 355…拖曳支柱 315...小齒輪 356...上端部 316...小齒輪 360...拱形軌道 318...步進馬達 361...上端部 320…螺帽 362...下端部 321...主體 365...線性狹缝103 593064 发明, Description of the invention 151 ... Front end 152 ... Rear end 153 ... Opposite side 154 ... Opposite side 165 ... Upholstered stool 166 ... Upper surface 167 ... Cushion 169 .. Flat upper surface 201 ... Upper end 202 .. Front end 203 .. Rear end 204 .. Rear wall 205 .. Side wall 206 .. Side wall 221 .. Trunnion 222. .. Rotary bearing 223 .. Shaking plate 224 .. First edge 225 .. Second edge 226 .. Surface facing 227 .. Inner surface 228 .. Upper end 229 .. Lower end Portion 230 ... First torque tube 231 ... Opposite end portion 232 ... Opposite end portion 23 5 ... Recessed portion 241 ... Link rod 242 ... End portion 243 ... End portion 244 ... End Portion 245 ... rocker 246 ... end 250 ... torsion tube 251 ... end 252 ... end 253 ... bearing 260 ... hollow worm gear housing 261 ... bottom surface 262 ... .Inner chamber 263 .. Upper wall 265 ... Lut 270 ... Worm 271 .. Worm gear 272 ... Thrust bearing 273 .. Worm housing 275 ... Spindle 280 .. Electric motor 104 593064 Description 281 ... Motor housing 322 ... Slider part 282 ... Link 324 ... Wing part 283 ... Link 3 2 5 ... Outer surface 284 ... End 326 ... Inner surface 285 ... End 329 ... Horizontal free joint 286 ... Second end 330 ... Diaphragm 301 ... Recess 331 ... Lateral side edge 302 ... Lower end 332 ... transverse side edge 303 ... upper end 333 ... rear end 304 ... linear screw 334 ... front end 305 ... upper end 341 ... upper end 306 ... lower end 342 ... .Overhang rod 307 ... bearing 343 ... end 308 ... rotation bearing 345 ... slider 310 ... gear housing 350 ... slide 311 ... helical gear 351 ... upper end 312 ... Transmission shaft 352 ... lower end 313 ... end 354 ... lower end 314 ... end 355 ... towing strut 315 ... pinion 356 ... upper end 316 ... pinion 360 ... Arched track 318 ... Stepping motor 361 ... Upper end 320 ... Nut 362 ... Lower end 321 ... Main body 365 ... Linear slit

105 593064 玖、發明說明 366.. .上端部 367.. .下端部 371.. .摩擦塊件 372…夕卜表面 373.. .下側構件 374…下背靠元件 375.. .上端部 376.. .下端部 377.. .線性後邊緣 378·.·腳部分 379·.·鼻部分 380.. .蓋板 3 81...前邊緣 385.. .膜片 386…後方下凹部 387.. .前方下凹部 390.. .腔室 391.. .周圍側壁 392.. .搖桿 393.. .上翼件 394…上背靠元件 395.. .下翼件 396.. .鈍角頂點 397.. .插銷 398.. .凸耳 402.. .上側構件 403.. .上膜片 404.. .後邊緣 40 5...前邊緣 406.. .前上凹部 407.. .後上凹部 408.. .坐墊 409.. .上端部 410.. .樞轉點 411.. .下端部 412.. .腳部分 414.. .切除部分 420.. .無效運動裝置 431.. .凸耳 432.. .臂構件 433.. .端部 434.. .端部 440.. .充填膜片構件 442.. .坐墊 443.. .上表面 450.. .折線構件 451.. .樞轉點 452.. .第一翼件 106 593064 玖、發明說明 453…鉤 454…第二翼件 455.. .凸輪從動件 4 5 6...支稽插銷 457.. .停止插銷 460.. .凸輪 510.. .飛機機身 515…鼻部分 520.. .客艙 526.. .内部表面部分 528.. .内部表面部分 529···行 5 3 0...地板表面 532.. .座位軌道 5 3 4...座位軌道 536…空間 537.. .群組 538.. .群組 610.. .殼總成 610a...半殼 610b...半殼 610’…相鄰座位 611…底部邊緣 612.. .後隔板 614.. .前隔板 616.. .線性側壁 618.. .乘客空間 620…座位 622.. .座位底盤 623.. .前邊緣 624···背靠 625.. .下端部 626.. .下端部延伸部分 628…下座位底盤 629…開口 630…足箱 630’...足箱 632.. .側壁 634.. .側壁 636…上壁 638…平坦的部分 640.. .托架 652.. .床墊 710…殼 710a...半殼 710b...半殼 712.. .後隔板 714.. .前隔板105 593064 发明, Description of the invention 366.... Upper end portion 367... Lower end portion 371... Friction piece piece 372... Surface 373... Lower side member 374... ... Lower end 377... Linear rear edge 378... Foot portion 379... Nose portion 380... Cover 3 81 ... front edge 385... Diaphragm 386 ... rear recess 387. ... Front recess 390 .. Cavity 391 .. Surrounding side wall 392 .. Rocker 393 ... ... Latch 398................... The upper member 403... The upper diaphragm 404... The rear edge 40 5... The front edge 406... 408 ... seat 409 ... upper end 410 ... pivot point 411 ... lower end 412 ... foot part 414 ... cutout part 420 ... invalid motion device 431 ... lug 432 .. arm member 433 .. end 434 .. end 440 .. filling diaphragm member 442 .. cushion 443 .. upper surface 450 .. polyline member 451 .. pivot point 452 .. First wing 106 593064 玖, invention description 453 ... hook 454 ... second wing 455 ... cam follower 4 5 6 ... support latch 457 .. .Stop latch 460... Cam 510... Aircraft fuselage 515 ... nose section 520... Cabin 526... Inner surface section 528... Surface 532 ... Seat track 5 3 4 ... Seat track 536 ... Space 537 ... Group 538 ... Group 610 ... Shell assembly 610a ... Half shell 610b ... Half shell 610 '... adjacent seat 611 ... bottom edge 612 ... rear partition 614 ... front partition 616 ... linear side wall 618 ... passenger space 620 ... seat 622 ... seat cushion 623 ... front edge 624 ... Backrest 625 ... Lower end 626 ... Lower end extension 628 ... Lower seat chassis 629 ... Opening 630 ... Foot box 630 '... Foot box 632 ... Side wall 634 ... Side wall 636 ... upper wall 638 ... flat section 640 .... bracket 652 ... mattress 710 ... shell 710a ... half shell 710b ... half shell 712 ... rear partition 714 ... front partition

107 593064 玖、發明說明 716··· 側壁 718… .乘客個人空間 720··, .座位 722.. .座位底盤 723.· .後邊緣 724.. .背靠 725.· .前邊緣 729·· •開口 730·· .足箱 732.. .側壁 732, ...側壁 733, ...外凹部 735. ..座位延伸部分 735, ...擱板 736. ..上壁 738.. .水平部分 740.. .托架 752.. .突出部分 760.. .底座 762.. .下壁 763.. .直立的側壁 764.. .凹部 765.. .上邊緣 770.. .地板嵌板 i 772…底側 800.. .乘客容納單元 810…客艙側壁 830.. .空間 840.. .四邊形空間 900…第二乘客座位總成 910.. .支撐結構 911.. .上表面 912.. .乘客支撐構件 913.. .間隙 914.. .乘客支撐構件 915.. .乘客支撐構件 916.. .腔室 917.. .橫向邊緣 918____L表面 920.. .乘客座位 921.. .後表面 922.. .背靠元件 923.. .前表面 924.. .座位底盤元件 925.. .前端部 926.. .上表面 927…隱私隔板 928…腿靠部分 108 593064 玖、發明說明 929·.·上表面 980·.·凹部 930...座位移動機構 1001...曲線壁 932...多邊形板 1002…曲線壁 934...狹縫 1012·.·縱軸 935...邊緣 1014...向前軸 9 3 6...邊緣 1015...空間 937…凸耳 1029…行 939...邊緣 1030…中央行 940...連桿組裝置 1101...縱向壁 941…第一構件 1102...縱向壁 942…第二構件 1112...縱軸 943…膝部接頭 1114…前後向軸 944…樞轉點 1129···行 945…鉸接部分 1130··.行 951...凸耳構件 1210…支撐結構 952...樞轉點 1211...上表面 954...末端 1212...輔助的乘客支撐元件 955···末端 1213...間隙 961...線性支柱 1214...輔助的乘客支撐元件 962...端部 1216...腔室 971...曲線的軌道 1220...座位 972...板構件 1221...後表面 973...上末端 1222…背靠元件 974...下末端 1223...前端部 109 593064 玖、發明說明 1224.. .座位底盤 1225.. .後端部 1226.. .下端部 1228.. .搁腳部分元件 1229.. .上表面 1230.. .樞轉點 1231.. .延伸部分 1280.. .凹部 F...地板107 593064, Description of invention 716 ... Side wall 718 ... Passenger personal space 720 ..., Seat 722 ... Seat chassis 723 ... Rear edge 724 ... Back 725 ... Front edge 729 ... • Opening 730 ... Foot box 732 ... Side wall 732, ... Side wall 733, ... Outer recess 735 ... Seat extension 735, ... Shelf 736 ... Upper wall 738 ... Horizontal section 740 ... bracket 752 ... protruding section 760 ... base 762 ... lower wall 763 ... upright side wall 764 ... recess 765 ... upper edge 770 ... floor panel i 772… bottom side 800 .. passenger accommodation unit 810. cabin side wall 830 .. space 840 .. quadrilateral space 900 .. second passenger seat assembly 910 .. support structure 911 .. upper surface 912 .. Passenger support member 913 .. Clearance 914 .. Passenger support member 915 .. Passenger support member 916 .. Cavity 917 .. Lateral edge 918____L surface 920 .. Passenger seat 921 .. Rear surface 922. .. Backrest element 923 .. Front surface 924 .. Seat chassis element 925 .. Front end 926 .. Upper surface 927 ... Privacy partition 928 ... Legrest portion 108 593064 玖, Invention description 929 ... · Top surface 980 ··· Recess 930 ... Seat moving mechanism 1001 ... Curved wall 932 ... Polygon plate 1002 ... Curved wall 934 ... Slot 1012 ... Vertical axis 935 ... Edge 1014 ... Forward Axis 9 3 6 ... edge 1015 ... space 937 ... lug 1029 ... row 939 ... edge 1030 ... central bank 940 ... link set device 1101 ... longitudinal wall 941 ... first member 1102. .. longitudinal wall 942 ... second member 1112 ... longitudinal axis 943 ... knee joint 1114 ... forward and backward axis 944 ... pivot point 1129 ... line 945 ... hinged portion 1130 ... line 951 ... lug Member 1210 ... Support structure 952 ... Pivot point 1211 ... Upper surface 954 ... End 1212 ... Auxiliary passenger support element 955 ... End 1213 ... Gap 961 ... Linear pillar 1214. .. auxiliary passenger support element 962 ... end 1216 ... chamber 971 ... curved track 1220 ... seat 972 ... plate member 1221 ... rear surface 973 ... upper end 1222 ... backrest element 974 ... lower end 1223 ... front end 109 593064 玖, invention description 1224 ... seat base 1225 ... rear end 1226 ... lower end 1228 ... footrest element 1229 ... upper surface 1230 ... pivot point 1231 ... extension Div. 1280: recess F ... floor

110110

Claims

Patent application scope No. 092101637 Patent application patent application scope amendment May 1993 A passenger accommodation unit for vehicles, especially for aircraft, which is used to provide passengers with their own, individual seats and sleep For berths, the seat assembly includes: a support structure, which is a unit for supporting the floor leaving the vehicle, or more movable passenger support, structural elements; to the structure, and for Mobile, structural element connected components so that the element is optionally in the form of a seat, where multiple passenger support surfaces or the I structure are located on the one or more structural, movable elements Composition-passenger seat, and-bed form, wherein a plurality of the support surfaces are substantially coplanar and are continuously arranged to form a passenger bed, moving between them; it is characterized by at least one of the movable elements It is double-sided and includes a first and second opposite sides, wherein one of the sides has a first-seat surface attached to the seat-form towel component, And further - the side having - a second bed surface of the bed in the form of lines constituting the portion of the bed. For example, the passenger accommodating unit of the scope of application for patent item i, wherein the at least-bilateral movable element is a back-to-back element. For example, the passenger accommodation unit of the scope of patent application, wherein the backrest element system can be connected with the pushing structure, so that it can optionally be pivoted between a first substantially upright position and a second inclined position The first-substantially upright position where the first-surface system is configured to form the seat of the section and the second inclined position where the second surface is configured and the scope of the patent application is set to form the bed of the section. Shi claimed that the passenger accommodation unit of item 3 of the patented dry enclosure, wherein the surface of the first bed with the element leaning back, is generally horizontal in the second inclined position. ^ Declares that the passenger accommodation unit of the patent dry enclosure item 3 or 4, in which the 4 times each support surface system includes a seat chassis, and its / month A element system can be connected to the structure so that in the second inclined position The sin component covers the seat chassis. 6 ·: Passenger accommodating unit under the scope of application for patent No. 5, wherein the seat chassis includes one or more of the movable elements, which are connected with the structure for having between an upper unfolded position and a lower storage position One vertical = one side moves upwards, and the seat chassis moving member is configured to move the seat chassis from the upper unfolded position to the lower Jianzang position when Tian Yue Gui 7G is moved from an upright position to an inclined position. 7. The passenger accommodating unit according to item 3 of the patent application scope, wherein the one or more passenger supporting surfaces include a bed extension surface. In the type of seat 2, the bed extension surface is configured or expandable to Seats are placed forward or backward. & The passenger accommodating unit as claimed in claim 7, wherein the backrest element can be connected to the structure so that in the inclined position, the second bed surface and the bed extension surface constitute a substantially continuous surface. 9. If the passenger accommodating unit of item 7 or 8 of the patent application scope, wherein the bed extension surface is configurable or expandable to place the seat chassis element into the front chisel seat form, the bed extension surface can be used to pick up 2. The scope of patent application: T-hooks on one side. 10. If the passenger accommodation unit No. 3 of the scope of the patent application, the-or even 4 times each support surface wraps one, the back extended surface on the back of the back element, and + + 土一 " The moon component can be connected to the structure so that, in the inclined position, the first bed surface and the extended surface are substantially coplanar. 11. According to the scope of the patent application, item 10 is not all inclusive, in which the back element is in the inclined position Λ-you are separated from the front surface of the extended surface of the Haiyue surface, and it is possible to configure Qin—Private moving filling elements, which are connected to the structure so as to be movable between a healthy position and an unfolded position. When the filling element is unfolded, the stomach fills 711. The pieces include-passenger support filling surface, Extends between the β-helium element and the back surface extension surface, so that the back surface extension surface, the filling surface, and the second bed surface structure are substantially continuous surfaces, and wherein the configurable member stands upright as a backing element When the position is moved to the inclined position, it is used to move the filling element from the storage position to the unfolded position. 12. The passenger accommodating unit according to item 3 of the patent application, wherein the backrest element system is structurally connected for selective movement between an upright position and a fully reclined position, wherein the backrest element system is relatively upright Shake the position backwards. One or more of the movable element systems may include a seat chassis that is connected to the support structure such that it is pivotable relative to the support structure between a first and a stern position, and the configuration member acts as a backrest element It is used to gradually pivot the seat chassis from the first position to the second position to apply for special fiber placement when it is turned back from the upright position to the fully reclined position. [3] If Yin requested the passenger accommodation unit in item 2 of the patent, the one or more of the movable components may include a seat chassis, and the supporting structure is connected so that it can be connected to a first position with- The first position is pivoted relative to the backrest cymbal, and the configuration member is used to gradually rotate the seat chassis from the _ position when the backrest element is pivoted rearward from the upright position to the fully reclined position. To the second position. 10 14 · If the passenger accommodating unit of item 1 of the patent scope, please claim that the one side of the two-sided movable element bears a foamed padding layer and the temple surface is made in an appropriate shape. 'Use as a The seat element, and the other side carries a foamed padding layer having a substantially flat surface, used as a part of the bed. 15 15. ^ Passenger seat assemblies for passenger vehicles, especially for machines. The assembly is used to provide passenger seats and sleeping facilities. The unit includes a cut structure that is used to support leaving the vehicle floor. Assembly; a plurality of seat elements, including a seat chassis element and;-a backrest element, the backrest element includes first and second opposite side edges, /, the side of the royal j has a first seat Surface, and the other side has a substantially flat second bed surface; 20 or more auxiliary receiving elements, which are connected to or constitute part of the supporting structure, and can be configured or Deployably juxtaposed with the seat, the or each auxiliary accommodating element has an auxiliary, substantially flat passenger support surface, and a seat moving mechanism for connecting the seat element to a support 4 "Fan Qi 7 Structure" Hai seat moving mechanism includes _ seat conversion sub-mechanism, which is to allow and control the movement of the seat element, so that the seat element can be selectively in the seat used to provide passenger seats Form, can be moved in the form of bedding to provide passenger beds, the seat conversion sub-mechanism is used to control the movement of the backrest element, so that the backrest element system can be The first and second side cooperate with the seat chassis element to form a seat, and pivot to = the second inclined position, where the surface of the second bed is generally configured to be coplanar or continuous with the supporting surface of the auxiliary passenger support Use 10 to make the bed. 16. The passenger seat assembly of claim 15 in which the seat moving mechanism is used to control the seat chassis element and the backrest element to move relative to each other. 17 · Russian #Patent 粑乘客 15 or 16 passenger seat assembly, wherein the 15 纟 position conversion sub-mechanism can be used to control the movement of the backrest element: ;; When the backrest element is from the first position When moving to the second position, the backrest element pivots forward to cover the seat chassis element, and the backrest element in the first inclined position overlaps and covers the seat chassis element. 18. The passenger seat assembly of item 17 in the scope of patent application No. 4, wherein the seat ## changer mechanism can be used to control the movement of the seat chassis element, so that when the backrest element moves from the first upright position to the second In the second inclined position, the seat chassis elements are moved downward relative to the support structure by being induced. 19. If you apply for a passenger seat assembly in item 15 of the scope of patent application, the seat in # 5 593064, the scope of the patent application and the moving mechanism further include a seat backrest mechanism, which is used to allow the seat to be selected From the upright position to a fully reclined position, the seat reclining mechanism is used to control the movement of the backrest element so that when the seat is reclined from the upright position to the fully reclined position 5 hearts * 70 The piece swung backwards from the first upright position to the third fully reclined position. 20. If the passenger seat assembly of item 19 of the scope of patent application, the rear seat = mechanism is used to control the movement of the seat chassis element, so that the Tianyue sin component is shaken backward from the first upright position to the third completely The 10 I tilt position causes the seat chassis element to tilt backwards. 21. The passenger seat assembly according to item 15 of the patent application, wherein the one or more auxiliary components are arranged or expandably arranged in front of or behind the seat. 22. The passenger seat assembly according to claim 21, wherein the auxiliary receiving element on one or more nights includes a footrest, which is configured in front of the n-seat or 17 unfolded, and which is in the first The surface of the second bed of the two mid-crime elements is generally configured to be coplanar and continuous with the footrest. 2 () 23. If the passenger seat assembly of item 21 of the patent is requested, the one or more auxiliary components include a fixed extension surface on the rear side, which is arranged behind the seat. 'As in the patent, the passenger seat assembly of item 23 of the patent, wherein the seat includes a movable filling element, and the seat conversion sub-mechanism can be used to store the filling element in a lower, storage position and a raised, accessible position. 6 Pick up the extension of the scope of the patent application # Modular extension: On the second inclined position, the filling element is substantially coplanar with the second surface of the backing element and is connected in parallel: The back extends the surface so as to constitute-a substantially flat, = bed surface, and in which the seat changer mechanism is tied in-the step: π controls the movement of the filling element, so that when the backing element system -... the upright position moves to the In the second inclined position, the filling pieces are moved from the storage position to the unfolded position upon being induced. The filling element is pivotally connected to the lower end of the backrest element, so that when the Λ element is moved from the first position to the second position, the filling element is moved from the storage position to the unfolded position. 25. The passenger seat assembly of claim 15 in which the side of the backrest member carries a foamed congestion layer with a hemp-compatible first surface, which is used to form a -back The backrest or part of a seat is backed, and the other side bears—a foamed padded layer with a generally flat, twisted second surface, which is used to form part of the bed. 26. The passenger seat assembly of claim 15 in which the seat conversion sub-mechanism includes-a seat support rack, which is pivotally connected to the support structure 'for a first seat position and a second When the bed position is shaken, the backrest element system can be installed on the supporting structure, so that the backrest element system can be moved from the first position to the second position by shaking the support device from the first position to the second position. The upright position is pivoted to the second inclined position, and a releasable fixing device is used to selectively fix the gift device in the first and second positions. 27. If the passenger seat assembly of item 26 of the patent application, wherein the seat pick-up and patent application chassis components are pivotably mounted on the support device, the arrangement is such that the backup support device is in the first position When it is shaken to the second position, the seat chassis element is induced to move downward from an upper unfolded position to a lower storage position 'and the backrest element is shaken to cover the seat chassis element forward, so that in the second inclined position, the The components cover the components of the seat chassis. 28. If the passenger seat assembly of item 27 of the application for a patent, wherein the seat chassis element includes a front end portion and a rear end portion relative to the backrest element, the far seat chassis element may be at the rear end portion or Finger support is provided towards the rear end, and wherein the seat moving mechanism further comprises a seat chassis support means for supporting a front end portion of the seat chassis element. And if the application for the related item is completed, the seat chassis support device includes a slideway, which is arranged below the seat chassis element, the foot member has two opposite ends, and one of the ends may be Pivotally connected to the front end of the seat chassis element, and the other end is slidably engaged in the slideway, > a 丄 and a tow post connect the other end of the foot member to the supporting device; the configuration So that when the optional device is shaken from the first position to the second position, the moving tow post is used to induce or allow the other end of the foot member to slide on the slideway, and the slideway has an outer shape so that When the branch device is moved from the first position to the second position, the 'foot member system moves downwards, thereby causing confusion. The front end of the chassis element of the afternoon seat is progressively downward # ^ After the passenger seat assembly, such as the scope of patent application No. 25, which includes the seat, the scope of patent application: :: several: further includes a seat back When the support device is arranged in the first seat position, the mechanism allows the seat element to selectively move between the upright position and the fully reclined position. 10 31. If the passenger seat assembly of the patent application No. 3G, the seat reclining mechanism of the seat includes-a curved track, which is attached to the support device, and has two opposite track ends, and A plurality of spaced-apart track followers are attached to the backrest element, and the track followers are used to spray and slide along 2 tracks. The track is assembled so that the track followers slide along the track from the end to At the other end, the backrest element is gradually shaken backward to the third upright position to a third fully reclined position. 15 32. The passenger seat assembly according to item 31 of the application for a patent, wherein the seat reclining sub-mechanism may further include a selectively operable two-way transmission device for translating the backrest element in translation. Moving relative to the support structure, the configuration causes the transmission device to act to slide the track follower along the curved track, thereby causing the backrest element to gradually swing between the first and third positions. The passenger seat assembly of claim 32, wherein the transmission 20 device includes a linear actuator connected between the backrest element and the support device. Q Λ • The passenger seat assembly of claim 33, wherein the linear actuation includes a linear screw fixedly secured to the supporting device, a screw engaging device pivotally connected to the backrest element, and a The supporting device carries a selectively operable bi-directional motor for rotating the linear screw and applying for a patent to drive the linear screw. For example, the passenger seat assembly of the patent application No. 33 or 34, wherein the seat chassis element may have a front end portion and a rear side relative to the backrest element, and the linear actuator may be pivoted at The supporting device 连接 4 is connected between the seat chassis elements, and the linear actuator is attached to the seat chassis element toward the rear end portion or toward the rear end portion, and is used to drive down gradually relative to the support structure. The seat chassis element is from a first upper position 10 when the Tianyue element element is positioned in the first upright position to a first lower position when the backrest element is positioned in the third fully reclined position 'and wherein The seat moving mechanism further includes a seat chassis supporting device, which is used to drive the rear end of the seat chassis element to the lower end and the front end of the seat chassis element of the branch building, thereby causing the seat chassis to swing backward when the f lean element Tilt backwards gradually. 15 36 · If the passenger seat assembly of the patent application is applied for, the linear device can be connected to 70 cases of the crime by an invalid motion device (1 post motion device), which is allowed in the seat chassis and the backrest element. Relatively small lateral shift. 37. The passenger seat assembly according to the scope of application for patent No. 26, wherein the seat 20 transfer mechanism further includes a -selectable two-way actuator for fixing the pushing device to the -seat Shake between the position and the first bed position. (linkage) It is considered that the 37th slave passenger Yu «, where the actuator includes-a four-rod double-rocking link set σ brie, such as doubIe_rocker, includes a rocker and a connector link attached to the branch]. The patent application scope support device is connected to the rocker in the middle, and the two-way square-reading transmission device with selective operation can be used to actuate the rocker. This configuration causes the rocker to act and cause the gift device to 9. The passenger seat assembly of item 38 in the first and second positions as described in the patent claim 38, wherein the rotary transmission device may include a motor, an worm wheel (w_ state and a worm wheel (a Whee1), wherein the worm wheel (worm wheel) is fixedly fixed to the rocker. 4 Application. The passenger seat assembly of the 39th aspect of the patent view, wherein the worm wheel (㈣ ^ is from the worm wheel ⑽ 啦, she called out of permission) The support device is manually rocked between the first and second positions. For example, the passenger seat assembly of item 37 of the Shengu patent scope, wherein the actuation is attached to the support structure under the seat element 42 ·: Passenger Seat for Patent Application No. 26 The assembly, wherein the supporting device includes two spaced apart side members, which are respectively arranged on opposite sides of the backrest element. 43. The passenger seat assembly according to item 42 of the patent application, wherein the connection The connecting rod system can be connected to the side members, and is located under the frame axis between the support device and the support structure. 44. A seat system for each vehicle, especially for aircraft, which includes a plurality of seat units, each A seating unit defines an abstract longitudinal axis of the seat and includes a support structure for attaching the seating unit to a floor of a vehicle, a molded member, or a configuration configured to form a Features of the seat; the feature is that the seat unit 593064 is patented and is configured to constitute—the line's n) definition—the abstract vertical axis. In this line, the seat unit is in a vertical offset relationship with轴 The shafts are arranged side by side at an acute angle to form the back space of each seat, and each seating unit further includes formed members or is configured to form-substantially flat The main part of the bed is arranged in the front of the seating position. The bed extends backward into the space to stretch the bed. Ίο 45. If the seat system of the 44th area of the patent application is characterized by the acute angle system In the range of 30-60 degrees, it is preferably 40-50 degrees. 46. The seat system according to item 44 of the patent application range is characterized in that the acute angle system is in the range of 30-60 degrees, preferably 47. If the seat system of patent application No. 44 or 45 is characterized in that the vehicle includes a passenger space, the cabin defines an abstract passenger ship longitudinal 15 axis, and the abstract line The shaft may be substantially parallel to the guest pump, or may form a pair of acute angles. 48. The seat system according to item 44 of the patent application, which is characterized in that the seat unit is arranged adjacent to one side wall of the vehicle and faces inward. 49. The seat m according to claim 44 is characterized in that the mother-seat unit further includes a footrest portion which is arranged in front of the seat. 50. The seat system of claim 49 is characterized in that each seat unit further includes a footrest portion which is arranged in front of the seat. 12 593064 Patent application scope 51. The seat system of the 44th patent scope is characterized in that the seat forming member and the bed forming member may include one or more movable passenger supporting elements, and the attachment options are It is configured to be at least part of the passenger seat in the form of a seat, or at least part of the flat bed in the form of a bed, and the flat bed in the form of a bed is configured. At substantially the same height as the seat chassis in the seat form. ίο A If the seat system of the scope of application for the item 51 of the patent application, each of the seat units in the material space of the seat includes the _th_passenger-removed element. When the movable element is assembled into a bed, the -The passenger support element is generally configured to be coplanar with the one or more movable elements and is a flat bed used to form the portion. 53. The seat system of claim 52, wherein the 15-per-seat unit further includes a second passenger support element fixed to the side of each seat. The second passenger selection element is substantially The upper configuration is coplanar with the first passenger support element, and is used to form the flat bed of the portion when the movable element is assembled under the bed form, thereby extending the flat bed laterally. 20 54. If the seat system according to item 53 of the patent application scope, wherein the first fixed element of the one seat unit is generally configured to be continuous with the second fixed element of the adjacent seat unit, and the first The components can be separated from each other by a privacy barrier. -A kind of reclining seat assembly, which is especially used on a cutting tool, 1 series includes-a fixed support part to support the floor leaving the vehicle 13 55. 593064 A reclining seat part including a seat chassis and a backrest, and a seat connecting device for connecting the seat part with the branch part, the connecting device including a seat reclining mechanism for allowing and controlling The movement of the seat portion between a first upright position and a first fully reclined position, and a selectively operable bidirectional motor are used to drive the seat portion in the first and second positions; wherein the The seat reclining mechanism includes an irreversible linear actuator connected between the motor device and the seat portion. · 56 · —A kind of reclining seat assembly, which is specially used on an airplane, which includes-a fixed saluting part, an assembly for the floor to leave the vehicle,-a reclining seat part It includes a seat chassis and a month A and a seat connection device for connecting the seat part to the A support 4 ′ knife. The connection device includes a seat reclining mechanism for allowing and controlling the seat part in a first The movement between the upright position and a first fully reclined position, and a selectively operable reversing motor 'are used to drive the seat to hold the points in the first and second positions; The reclining mechanism includes an irreversible linear actuator connected between the motor device and the seat part. The reclining seat assembly is applied after the 55th of the patent scope. The irreversible linear actuator may include a lead screw drive or -Ball screw drive. Shishen ° Monthly Patent Offense 57th reclining seat assembly, where the linear motion includes-linear screw or ball screw, attached to the branch ... one of the xuan seat parts-part (or- Partial connection), with 14 593064, patent application scope and a screw spraying system attached to the seat part and the supporting part, or another part (or part of the connection). 59. For example, Shen Shiyue's patent scope 55, 57 or 58 reclining seat assembly, wherein a money actuator can be connected to the seat chassis for being located in a first position relative to the supporting portion A predetermined linear path from a second position drives the seat chassis. ίο 15 6〇 · If you apply for the 59th scope of the patent application, you can recline the seat assembly, where the seat bottom i has a front end and a rear end, and the line actuation system can be at the rear end. The frame is connected to the seat chassis at or towards the rear portion, and is configured to drive the rear portion of the seat chassis downward when the seat chassis is moved from the first position to the second position. The reclining mechanism further includes a support device for supporting the front end of the seat chassis when the rear end of the seat Z chassis is driven downward, thereby causing the seat chassis to tilt backward when the backrest is swung back. 61. The reclining seat assembly according to item 55 of the patent application scope, wherein the linear actuator is connected to the backrest and is used for translational transmission between a first upright position and a second reclining position In the backrest, the seat reclining mechanism further includes a guide device for gradually and backwardly swinging the backrest relative to the support portion when the backrest is moved from the first upright position to the second fully reclined position. 62. If the reclining seat assembly of item 61 of the patent application scope, wherein the guide device includes a curved track, which is attached to the support part or a part is connected to the support part, and a plurality of spaced track followers, It is attached to the backrest, and the follower follower is used to engage and slide along the track 15 20 593064, patent application scope. 63. If the patent application scope item 61 or 62 reclining seat assembly, wherein the linear actuator can be pivotally connected to the seat chassis, and can be hung to the backrest via two surplus: motion device, allowing the Relative rotation and translation between the seat chassis and the backrest 1. ίο 15 64.-A seat with a reclining backrest, the seat including a fixed support portion for supporting the seat off the floor, a seat portion including a reclining backrest and a seat connection Component 1 is used to connect the seat part with the support part, and the connection component includes a backstab mechanism which is used to allow and control the backrest in a f-th upright position and a second complete rear A movement between a supine position; wherein the backrest comprises a first lower backrest member having an upper end portion, and a second upper backrest member 'which is superposed on the backrest member and is connected to the end portion Or it is pivoted towards the upper end to facilitate its movement, and wherein the back-to-back mechanism includes first and second extensions attached to a support = or a part connected to the support part. The track has Two opposite track ends and a plurality of separated one-way track coupling driven members are attached to the 20-way support member and used to mesh and slide in the _ month one U track, and the ^ track Sialic follower member 'which is attached to the A part of the backrest member is connected to the backrest member, and the first track is curved so that when the first track slaves the driven member from one end to the other end along the first track, the first ― ” Between the first position and the second fully reclined position, the component is gradually retracted relative to the supporting part, the scope of the patent application, and the movement of the stopper is also caused by the shape of the second track. The affected part slides along the second lane, causing the first-month member A to gradually swing in relation to the _ backrest member. 10 15 • If there is a seat with a backrest that can be reclined, Its: the back-to-back mechanism includes a rocker system having a pair of obtuse angles :: the rocker system is pivotally connected to the sin component at a position in the middle of the two arms, and one of the arms carries the The second beveled toothed follower member, and a-link with two opposite ends, one of which is: pivotally connected to the other arm of the rocker, and the other end is fixed to the dungeon = to the first month # 机构； This configuration causes when the second driven member is subject to "" mouthing the first When the track slides, the rocker system is affected by its pivot axis to the first backrest member, which causes the pivot of the link to pivot to the other arm of the rocker, thereby causing the second backrest The component is pivoted to the first backrest component in relation to its pivot. 66. A seat having a reclining backrest, such as a patent application No. 64 or 65, wherein the seat connection component further includes an optional At first glance, the linear actuation benefit is connected between the support part or a part connected with the support part and the backrest for moving the backrest in translation relative to 20. The configuration is such that when the backrest is induced to move translationally relative to the support portion, the first driven member located on the first backrest member is induced to slide along the first track gradually, thereby causing the backrest Shake progressively between this first upright position and the second full-backward position. 67 • If there is a seat in the scope of the patent application, which can be reclined back, 17 593064, the scope of the patent application, where the far seat part includes a seat chassis, and the linear actuator is connected to the far seat chassis. The seat chassis is moved between a first position and a second position along a predetermined linear road control. 68. The seat having a reclining backrest as claimed in item 67 of the patent application scope, wherein the linear actuator is pivotally connected to the seat chassis. 69. The seat having a reclining backrest as claimed in item 66 of the patent application scope, wherein the linear actuator is pivotally connected to the backrest by an invalid motion device. 70 · —A seat module for a passenger vehicle, the seat module comprising a seat portion of 10 minutes, a footrest portion, a single support structure for supporting the seat portion and a footrest portion leaving the vehicle floor, and The attachment member is used for attaching the support structure to a pair of seats in the floor of the vehicle, and is characterized in that the attachment member includes two spaced-apart fixing portions 15 for attaching the support structure to the two-spaced structure. The opening point is fixed to one of the pair of tracks-the track, and a third fixing part is used to fix the support structure to the other track, so as to provide the seat between the seat module and the seat track. The modules are connected to the seat track one by one to form a plurality of seat sheets 7L. Each seat sheet A includes a seat portion of one module and a footrest portion of another adjacent module. 71. The passenger seat assembly of item 4 or item 39 (4) of claim 4, which is characterized in that in the first position, the rocker and the connector link form a diagonal of-stiffness' to form a pillar to thereby The force applied to the support device is transmitted linearly via the joystick to the worm without rotation. 18 20 593064 Pick up and apply for patent scope 72. For the passenger seat assembly of the scope of application for patent No. 40, wherein the worm-gear is combined with the worm-wheel via an interrupt link device, the The device is used to prevent the worm-gear from inadvertently disengaging from the worm-wheel, but can be selectively actuated to allow the worm-gear to disengage from the worm-wheel. 19