CN101014496B - Arrangement of the upper part of an aircraft cabin - Google Patents
Arrangement of the upper part of an aircraft cabin Download PDFInfo
- Publication number
- CN101014496B CN101014496B CN200580025430.8A CN200580025430A CN101014496B CN 101014496 B CN101014496 B CN 101014496B CN 200580025430 A CN200580025430 A CN 200580025430A CN 101014496 B CN101014496 B CN 101014496B
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- Prior art keywords
- main cabin
- passageway
- cabin
- sleeping berth
- deck
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- 230000000630 rising effect Effects 0.000 claims description 4
- 239000000470 constituent Substances 0.000 claims description 3
- 108010066278 cabin-4 Proteins 0.000 description 9
- 239000003795 chemical substances by application Substances 0.000 description 9
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 8
- 238000000034 method Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000002459 sustained effect Effects 0.000 description 3
- 239000011229 interlayer Substances 0.000 description 2
- 230000007306 turnover Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 238000009428 plumbing Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0601—Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
- B64C2001/0027—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D2011/0069—Rest berths, beds or the like
- B64D2011/0084—Bed units for passengers attached to the ceiling of the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Seats For Vehicles (AREA)
Abstract
The arrangement relates to an aircraft cabin (4) comprising a main structure corresponding to the aircraft structure and enveloping the cabin (4), a deck (20) forming a flat surface provided with seats (12, 42) mounted thereon, a passage (32) which longitudinally extends along the cabin (4) and is raised with respect to the deck (20) and with berths (14) which are serviced by said passage (32) and disposed above the seats (12, 42) of the deck (20) transversally with respect to the passage (32) on both sides thereof.
Description
Technical field
The present invention relates to the layout on an aircraft cabin top.
Technical field of the present invention is the passenger traffic in aerocraft.In a given volume of aircraft cabin, under the situation that maximal comfort is provided for the passenger, settle passenger as much as possible proper.Usually provide three kinds of freight spaces: cabin saloon, business class and tourist class.In first and business class, offering passenger's seat tool modal is convertible seat tool, and said convertible seat tool offers passenger one seat of having a rest in primary importance, and the position that couches is provided in another position, couch described in the business class position what tilt to some extent.Known kinds of schemes from prior art, it provides the position that couches also for the passenger of tourist class.For example proposed to use a plurality of tools so that convert them to stack bed.The sleeping berth quantity that is obtained is less than the quantity of the seat of having a rest usually.In known solutions, generally two seats of having a rest are calculated as a sleeping berth.
Original thinking of the present invention is to use the upper space of aircraft cabin so that settle sleeping berth therein.Problem is to want to place the sleeping berth of larger amt.
Background technology
Some documents of prior art have proposed to use the upper space of aircraft cabin.Therefore, document EP-0901964 proposes in said upper space, to place some via the sensible sleeping berth of a gallery.Like what in the diagram of said document, seen, sleeping berth quantity is very limited.Therefore the use of said sleeping berth more properly is to keep for the aircrew.The document of another renewal, promptly document US-6619589 also proposes a similar configuration.
Summary of the invention
Thereby the objective of the invention is in the upper space of aircraft cabin, provide the sleeping berth of larger amt.
For this reason, the present invention propose one be used for the aerocraft of passenger traffic the main cabin, it has:
-one agent structure, its structure and envelope corresponding to said aerocraft is enclosed said main cabin,
-one deck, it forms a flat surface, and a seat tool is fixed on the said flat surface,
-one passageway, it is longitudinal extension in said main cabin, and said relatively deck high rise and
-sleeping berth, it is sensible via said passageway, and is placed in the seat tool top on said deck.
According to the present invention, laterally settle in both sides, said passageway and with respect to said passageway via the sensible said sleeping berth in passageway that said height rises.
Compare with the layout of similar sleeping berth in the prior art, because this configuration then can be placed more sleeping berth on the top in main cabin.
The present invention also proposes one preferred embodiment, and in said embodiment, sleeping berth is in the agent structure in a side mounting to the said main cabin of central aisle, and the opposite side in said passageway is connected to said same agent structure.Thereby the element that supports said sleeping berth can be also very firm when presenting a light and handy structure, because they are to link to each other with the agent structure in main cabin.In said embodiment; Can consider that for example said sleeping berth is by L-shaped structural member supports; One first branch of L shaped body is roughly parallel to ground, deck and extends; And appear one be substantially equal to a sleeping berth length length, and another branch of L shaped body is approximately perpendicular to said first branch ground and extends, and the free end of L shaped structural constituent is fixed on the agent structure in main cabin.
In order can bootlessly not increase the suspension load on aerocraft agent structure top, high passageway of rising is advantageously supported by the deck in main cabin.Here can not cause big overload for saloon deck.In fact, high passageway of rising may replace a row seat tool, and the weight that allows to realize a high element that plays the passageway should be greater than the weight of a row seat tool, even what relate to is the seat tool of tourist class.
Can consider: stair allow to enter each end in the passageway that said height rises.Said stair can be vertically or be laterally orientation in the main cabin.Under the situation of horizontal stair, said stair can be two pass type (thereby get into from the left side with from the right passageway).Also can design the stair of a bending.One ladder also can allow to lead to into passageway.But, though said method is feasible also lower than stair implementation cost, be not preferable methods according to reason, because it can not realize the sleeping berth outside that passenger's rapid evacuation is sensible to the passageway of rising via height.
In one embodiment, the high passageway end wise that rises is divided into two longitudinal part sections with the main cabin.Thereby see that in said aerocraft an end wise is with main cabin " wall " divided into two parts.This allow to form the passageway with a relatively large height, thereby the passenger that must get into sleeping berth can be bent over and is standing and walking.In the said configuration that has two longitudinal part sections, and when said main cabin had the seat tool that for example is convertible into sleeping berth and is not convertible into the seat tool of sleeping berth, a tool that is convertible into sleeping berth for example all was arranged in same longitudinal part section.
Give and to be located in the passenger on the sleeping berth in order to reserve a maximum space, advantageously the passage used of airline and pipeline is laid in the structure of support deck.
Preferred enforcement in the modification, parking space be disposed in passageway that said height rises below.This makes to have the baggage rack that some are easy to touch.In addition, one place the baggage rack on the pedestal also to place traditional baggage rack weight of eminence little than one.Owing to below the passageway that height rises, have a lot of spaces, said space also to can be used for to place the crew member to be used for providing the go-cart (English is trolleys) of service for the passenger.Can be used to admit the element that is known as (monument) between the chamber that is fixed in pedestal equally.For example can relate to and (be called " galleys " usually) between the kitchen that is used for cabin service or also relate to as taking in the wardrobe (said wardrobe is called as " coatstowage " usually at English) of passenger's overcoat and overcoat.
Disengage maximum space for be present tool place and sleeping berth place and be used for the passenger, the zone above sleeping berth is positioned at a tool, the top board on deck preferably is roughly parallel to the deck.
Description of drawings
Details of the present invention and advantage will from hereinafter, through embodying better the description of doing with reference to appended scheme drawing, in the accompanying drawings:
Fig. 1 be one be equipped with according to the birds-eye view in the main cabin of the aircraft of layout of the present invention and
Fig. 2 is the view corresponding to the cross-sectional plane of Fig. 1 aircraft in different configurations to Fig. 4.
The specific embodiment
Can see an aircraft among Fig. 1, its have one be positioned at aircraft forward driving compartment 2 and extend in the main cabin 4 on this aircraft major part.
In the front portion in said main cabin 4 one first cabin 6 is arranged, be furnished with the individual modules 8 that the passenger uses in said first cabin.In the individual modules 8 that said each passenger uses, there is one convertible tool, no matter this tool receivability is the sitting posture or the passenger of prone position.Other daily life equipment in said module, is equipped with equally.Therefore said cabin 6 is known as the cabin of cabin saloon.
There are one second cabin 10, this second cabin to have a tool 12 (can not convert bed to) on the one hand in the back in said first cabin 6, and have sleeping berth 14 on the other hand.Said seat tool 12 is arranged in the different height place with said sleeping berth 14.Therefore, said sleeping berth 14 is positioned at the top of said seat tool 12, and all said seat tools 12 all are positioned at sustained height, the individual modules 8 residing height that this height is used corresponding to the passenger.More detailed description will be done hereinafter in said second cabin 10.
There is one the 3rd cabin 16 at 4 the rear portion in the main cabin at last, places the seat tool 12 of seat tool in similar second cabin 10 in said the 3rd cabin.The individual modules 8 that seat tool 12 in the said seat tool 12 and second cabin 10 and the passenger in first cabin 6 use is positioned at sustained height.
Fig. 2 is corresponding to a section-drawing of airframe among Fig. 1, and said section is implemented at 10 places, second cabin.
To Fig. 4, an agent structure 18 of aircraft is enclosed by a pair of lines schematically illustrated on the limit, main cabin at Fig. 2.Here can relate to well-known to those skilled in the art one traditional aircaft configuration.Traditionally, one a main cabin 4 and a cargo hold 22 are separated with respect to the longitudinally extending deck 20 of said aircraft.Said deck 20 is supported by a structure 24, and this structure is formed by the beam that is fixed on the agent structure 18 especially.Said cargo hold 22 has a substrate 26, and is used for taking in standardized freight container 28 in its part that is arranged in the section place.
In ensuing description, can imagine, said deck 20 be level and whole length that extend in aircraft at grade and width on.Also can imagine, said main cabin is positioned at the top on said deck and said cargo hold is positioned at the below on said deck.
Said main cabin 4, sleeping berth 14 is arranged at the top in second cabin 10 or rather.Said sleeping berth is a horizontal positioned, promptly is parallel to placement of 20 ground, said deck and said relatively main cabin and laterally is orientated.As can see especially in Fig. 1 that two row's sleeping berths 14 are arranged here.Said two row's sleeping berths are arranged on the both sides of a central aisle 32.
Said sleeping berth 14 is supported by L shaped supporting member 34.Said supporting member 34 is to place like this: branch's horizontal-extending of L shaped body and another branch extends to the upper vertical in main cabin 4.The free end of the said branch of L shaped body links to each other with the agent structure 18 in said main cabin separately.Therefore obtain the interlayer (mezzanine) of two longitudinal extensions in the both sides of aircraft.Said passageway 32 allows the said interlayer of turnover.There is a pedestal 36 in said passageway, and this pedestal 36 is similar to the gangway ladder (passerelle) that is fixed on the deck 20.Therefore can obtain one in the centre in said main cabin 4 with respect to the said deck 20 high passages that rise.The turnover of said passage realizes that through two stair 38 wherein each end of 32 respectively has stair in the passageway.One sidewall 40 is connected to said sleeping berth 14 in the both sides in said passageway 32 with the pedestal 36 in said passageway 32.Therefore, other part in the said passageway 32 and second cabin 10 is kept apart.
Said pedestal 36 preferably rests on the storage box.Said storage box can be used for taking in the passenger's in second cabin 10 luggage.Bring the acceptable upperlimit of the luggage in main cabin into if consider common permission travelling, have enough spaces to lay below the pedestal 36 to ride in all luggage of the passenger who travels in said second cabin.Even also having enough spaces to be used for still below pedestal 36, placing go-cart (between the kitchen), said go-cart is generally used for supplying crew member (personnel navigant commercial; Cabin crew) service is provided aboard.The existence of said parking space can allow to cancel the baggage container that is usually located at top, main cabin.Thereby on the top in main cabin, more free space is just arranged, and said space is with regard to the comfort level that increases the passenger in the sleeping berth 14 capable of using.
Disengage more spaces again for the top in said main cabin 4, the said structure 24 that supports said deck 20 is arranged to allow said various plumbing system and pipeline to pass through.Therefore below deck 20, in said structure 24, for example letting, wirning harness, conduit under fluid pressure and air-pressure duct pass through.Airline as for being used for the main cabin ventilation then is located in said cargo hold 22, just in time below the said structure 24 of support deck 20 and near the aircraft outer wall.The position that receives said airline is indicated with reference marker 41.Said airline thereby between structure connecting rod (bielle de structure) and airplane skin, pass through.In order to give the overdraught in said main cabin 4, can set some pipelines along the transversary element that is known as framework, so that air is provided for the said part in said main cabin 4.
Fig. 3 illustrates one of Fig. 2 and implements modification.The difference here is: each side that said deck 20 is in said central aisle 32 has three positive front stall tools, and being seen as in the drawings, each side at central aisle in the configuration of Fig. 2 has four positive front stall tools.
The originality of the configuration shown on Fig. 4 is that convertible seat tool 42 is placed on a side of said central aisle 32, and the opposite side of said central aisle then has a tool 12, and said seat tool is corresponding to the seat tool of in the cabin of tourist class, seeing usually.Usually, have only in the aircraft on unique deck one, the seat tool of corresponding tourist class places the rear portion in main cabin, and first and business class then leans on the front portion in main cabin to arrange.Here the passenger of first and business class is positioned in the right (being the left side among Fig. 4) of aircraft with respect to the aircraft direct of travel, and the passenger of tourist class then sits in the left side of aircraft.Therefore, in the process of boarding, the passenger of tourist class just need not pass the cabin of first and business class again, but is directly led to the cabin of tourist class.
Above being used for of proposing allows for a large amount of passengers in the tourist class first in the scheme that aerocraft is placed sleeping berth and provides with prone position and travel.Certainly the sleeping berth Bueche seat that in tourist class, provides is few, but for example can consider that tourist class has two kinds of different regulation prices: sleeping berth is arranged or do not have sleeping berth.
The scheme that described proposition is used to realize sleeping berth can not cause bigger overweight to aircraft.In fact, mentioned as top, the said scheme that provides causes cancelling all and arranges pinnacled baggage rack.Said baggage rack has a relatively large quality.With being positioned on the deck and replacing the said baggage rack that is usually placed in eminence, alleviated weight quite significantly as the chest of the support of central aisle 32 pedestals 36.
The said scheme that provides allows to have a passageway 32, and the passenger can bend over just can walk about in this passageway.Therefore just can in the time period of aircraft industry prescribed by standard, realize evacuating out aerocraft.
Cancel the baggage rack that is usually placed in eminence and also can vacate the space on top, main cabin.Therefore said sleeping berth 14 can with the deck segment distance ground layout of being separated by, said distance just exceeds a people height.Therefore, for the sleeping berth that is positioned at aircraft cabin top of the prior art, the height of these sleeping berths can obviously reduce.The reduction of said sleeping berth height is special to allow to obtain at the sleeping berth place a bigger width, and allows the passenger and a central aisle that on sustained height, can have two directions of advancing with respect to aerocraft laterally to stretch on top, main cabin.
The present invention is not limited to the above embodiment of describing with non-limiting way.It also relates in all enforcement modification that those skilled in the art grasped in the scope described in the appended claims subsequently.
Claims (7)
1. be used for the main cabin (4) of the aerocraft of passenger traffic, said aircraft cabin has:
-one agent structure (18), its structure and envelope corresponding to said aerocraft is enclosed said main cabin (4),
-one deck (20), it forms a flat surface, and a seat tool (12,42) is fixed on the said flat surface,
-one passageway (32), they are longitudinal extension in said main cabin (4), and said relatively deck (20) high rise and
-sleeping berth (14), it is sensible via said passageway (32), and is placed in seat tool (12, the 42) top on said deck (20), and laterally settles in (32) both sides, said passageway and with respect to said passageway (32);
It is characterized in that in the agent structure (18) of said main cabin (4), and the opposite side in said passageway is connected to this identical agent structure (18) to said sleeping berth (14) in the side mounting in the passageway (32) of central authorities;
And high passageway (32) of rising is supported by the deck (20) in said main cabin.
2. according to the main cabin (4) of the described aerocraft of claim 1; It is characterized in that; Said sleeping berth (14) is supported by L-shaped structural constituent (34); One first branch of said L shaped body is roughly parallel to said deck extends (20), and have one be substantially equal to a sleeping berth (14) length length, and another branch of said L shaped body is approximately perpendicular to said first branch ground and extends; And the free end of said L shaped structural constituent (34) is fixed on the agent structure (18) of said main cabin (4).
3. according to the main cabin (4) of claim 1 or 2 described aerocrafts, it is characterized in that each end in the passageway (32) that the approaching said height of stair (38) permission rises.
4. according to the main cabin (4) of claim 1 or 2 described aerocrafts, it is characterized in that the passageway that said height rises (32) are divided into two longitudinal part sections with said main cabin (4) end wise.
5. according to the main cabin (4) of the described aerocraft of claim 4, it is characterized in that said main cabin (4) have the seat tool (42) that is convertible into sleeping berth and can not convert the seat tool (12) of sleeping berth to; And the said seat tool (42) that is convertible into sleeping berth all is arranged in same longitudinal part section.
6. according to the main cabin (4) of claim 1 or 2 described aerocrafts, it is characterized in that, be provided in the structure (24) that supports said deck (20) for airline and the used passage of pipeline.
7. according to the main cabin (4) of claim 1 or 2 described aerocrafts, it is characterized in that parking space is disposed in below the passageway (32) that said height rises.
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0408239A FR2873349B1 (en) | 2004-07-26 | 2004-07-26 | ARRANGEMENT OF THE UPPER PART OF THE CABIN OF AN AIRCRAFT |
| FR0408239 | 2004-07-26 | ||
| US60652204P | 2004-09-02 | 2004-09-02 | |
| US60/606,522 | 2004-09-02 | ||
| PCT/FR2005/001824 WO2006021646A1 (en) | 2004-07-26 | 2005-07-18 | Arrangement of the upper part of an aircraft cabin |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101014496A CN101014496A (en) | 2007-08-08 |
| CN101014496B true CN101014496B (en) | 2012-01-18 |
Family
ID=34947476
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200580025430.8A Active CN101014496B (en) | 2004-07-26 | 2005-07-18 | Arrangement of the upper part of an aircraft cabin |
Country Status (3)
| Country | Link |
|---|---|
| JP (1) | JP4870668B2 (en) |
| CN (1) | CN101014496B (en) |
| FR (1) | FR2873349B1 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2903664B1 (en) * | 2006-07-12 | 2008-09-26 | Airbus France Sas | AIRCRAFT CABIN ARRANGEMENT HAVING BUCKETS IN THE UPPER PART OF THE CABIN. |
| DE102009008355A1 (en) | 2009-02-11 | 2010-08-19 | Airbus Deutschland Gmbh | Workspace in an aircraft |
| JP2014520728A (en) * | 2011-11-01 | 2014-08-25 | シーアンドディー ゾディアック，インコーポレイティド | Airliner cabin array with high privacy |
| US9475583B2 (en) * | 2013-06-18 | 2016-10-25 | B/E Aerospace, Inc. | Location and support system for aircraft galley appliance inserts |
| EP3148874A2 (en) * | 2014-05-30 | 2017-04-05 | Zodiac Aerospace | Lower deck commercial cabin |
| US10800531B2 (en) | 2015-04-08 | 2020-10-13 | Safran Seats Usa Llc | Passenger accommodation systems including partition walls |
| FR3035072B1 (en) * | 2015-04-20 | 2020-09-18 | Airbus Operations Sas | AIRCRAFT WITH IMPROVED UNDER CABIN SPACE ARCHITECTURE |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0901964A2 (en) * | 1997-09-10 | 1999-03-17 | The Boeing Company | Aircraft overhead rest areas |
| US20020033432A1 (en) * | 2000-07-14 | 2002-03-21 | Mikosza Olgierd Stanislaw | Vehicle seating arrangement |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2630210C3 (en) * | 1976-07-05 | 1979-10-18 | Hans Guido Dr. 8000 Muenchen Mutke | Device for the horizontal transport of people, in particular in aircraft |
| US4066227A (en) * | 1976-07-16 | 1978-01-03 | Buchsel Christian K E | Mezzanine structure for wide-bodied passenger aircraft |
| DE4116524A1 (en) * | 1991-05-21 | 1992-11-26 | Airbus Gmbh | AIRCRAFT WITH WING AND A FUSELAGE |
| US6464169B1 (en) * | 2001-07-27 | 2002-10-15 | The Boeing Company | Overhead galley/crew rest facility |
| US6616098B2 (en) * | 2001-08-13 | 2003-09-09 | The Boeing Company | Mid-level deck for passenger aircraft |
| US6619589B2 (en) | 2002-01-28 | 2003-09-16 | The Boeing Company | Flight crew and attendant rest environmental control system |
| US6536710B1 (en) * | 2002-02-06 | 2003-03-25 | The Boeing Company | Overhead lattice support structure |
| US7077360B2 (en) * | 2004-07-01 | 2006-07-18 | Emil Jacob | Passenger sitting/sleeping arrangement |
-
2004
- 2004-07-26 FR FR0408239A patent/FR2873349B1/en not_active Expired - Fee Related
-
2005
- 2005-07-18 CN CN200580025430.8A patent/CN101014496B/en active Active
- 2005-07-18 JP JP2007523104A patent/JP4870668B2/en not_active Expired - Fee Related
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0901964A2 (en) * | 1997-09-10 | 1999-03-17 | The Boeing Company | Aircraft overhead rest areas |
| US20020033432A1 (en) * | 2000-07-14 | 2002-03-21 | Mikosza Olgierd Stanislaw | Vehicle seating arrangement |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2008507448A (en) | 2008-03-13 |
| FR2873349A1 (en) | 2006-01-27 |
| JP4870668B2 (en) | 2012-02-08 |
| CN101014496A (en) | 2007-08-08 |
| FR2873349B1 (en) | 2006-10-27 |
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