M413652 100年05月20日修正替換百 五、新型說明： ^ 【新型所屬之技術領域】 本創作主要係揭示-種具有降落裝置之飛行器，尤复 是指-種降落裝置設於飛行器之機腹，當飛行器降落時， 機腹能夠朝向天空之飛行器。 【先前技術】M413652 Modified on May 20th, 100th, the new type of explanation: ^ [New technical field] This creation mainly reveals an aircraft with a landing gear, especially the landing device is set on the belly of the aircraft. When the aircraft is landing, the belly can face the sky. [Prior Art]
飛打器藉由飛行於天空而能夠進行許多在陸地上所益 法進行的X作，飛行齡了錢旅客與貨物之外，更且有、 勘測地形、進行空拍.·.等等進行t集龍的X作，也常使 用於氣輯_隸，更具有能夠從空中施放或投擲物品 之功效，例如：施放敎、嘴灑農藥…等等。除此 飛行器最常應祕軍彻途，其能夠進行探純 武器發射。 J運仃 飛行料行⑽蕙制卫作時，飛行器的機腹内 有記錄器，記錄器能夠完錢集資料的工作。 9〇 。飛行器的操控分為兩種，其—為人為駕馱，另 人駕駛。以人為駕駛而言’飛行器能夠透過機 ^By flying in the sky, the flying sprinter can carry out a lot of X work done on the land, flying the money passengers and goods, and more, surveying the terrain, making aerial shots, etc. The dragon's X is also often used in the gas series, and it has the effect of being able to cast or throw objects from the air, such as: spraying cockroaches, sprinkling pesticides, etc. In addition to this, the aircraft is most often secretly attacked by the military, and it is capable of detecting the launch of weapons. J Yun 仃 Flight material line (10) When the squad is made, there is a recorder in the belly of the aircraft, and the recorder can complete the work of collecting money. 9〇. There are two kinds of control of the aircraft, which are artificially controlled and driven by others. In terms of human driving, the aircraft can pass through the aircraft ^
If/無人駕駛而言，控制人員在地面上的控制室^ k控裳置進讀控無人飛行H轉飛、飛行與降落。 無人飛行器的降落搭载有降落傘而進行降落 降落傘設《行器機柄购。當麟^欲進 = :=關閉飛行動力，且讓位於機尾的降落伞脫離二 幾身，降洛傘在適當時機會展開，藉由降落傘展開而 100年05月20日修正替換頁 讓飛行器能夠完成著陸的目的。 傳統的設計將降落傘設在機尾，因此，飛行器降落時， 機尾會朝向天空，而機鼻會朝向地面。當飛行器落地時， 顯然的機鼻與機腹會先落地，雖然飛行器受到降落伞的保 護而不會發生嚴重的損傷’但是機鼻、機腹與地面接觸時， 收藏在機腹内的精密設備，如記錄器，其稍受揸擊即可能 發生記錄器内的硬碟資料損壞之情事，而無法將記錄器所 記錄的重要資料提供給使用者。 因此本創作想排除或至少減輕先前技藝所遭遇的問 題。 【新型内容】 本創作欲提供-種『具有降落裝置之飛行器』，以解決 先前技術存在的問題。 本創作首要解決的技術問題是，飛行器降落時，該降 落裝置緩慢落下，該機腹朝向天空，該飛行器落地時，該 機鼻與該兩個垂直尾翼與地面接觸，因此能夠保護該機腹 不會與地面接觸’進一步保護收藏於機腹内之記錄器或其 他精密設備不會受到損傷。 本創作次要解決的技術問題是，當該飛行器失去動力 時，該飛行器藉由拋出該降落裝置而能夠控制該飛行器在 預定區域内下降著陸，該降落裝置展開時，其能夠延緩該 飛行器往下墜落。 其他目的、優點和本創作的新穎特性將從以下詳細的 100年05月20日修正替換頁 描述與相關的附圖更加 顯明 【實施方式】 有關本創作所採用之技術、手段及其功效，茲舉一較 佳貫施例並配合圖式詳述如後，此僅供說明之用，在專利 申上並不受此種結構之限制。 一。參照圖一、圖二與圖三，為本創作具有降落裝置之飛 仃盗之立體外觀圖與前視圖。本創作之飛行器1包括有一 個機腹11、一個機鼻12、-個機背13、兩個垂直尾翼14 與一個機尾15。該飛行器1飛行時，該機腹11朝向地面， 該機鼻12朝向前方，兮擔择] 介料尸… 3與該垂直尾翼14朝向天 工’ _尾15朝向後方，該機鼻12與 該飛行器1相對的兩端。 刀職於 該飛行器1之機腹u内收藏 其他精密設備，當着H i飛行圖巾未見）或 11内的記錄器或其他精密設備能夠空日土，收藏在該機腹 該飛行器1之機腹n包括，仃策集資料的工作。 體112’該容納空間ln鄰近該機尸，空間Hi與一個蓋 該蓋體112封閉該容納空間Ul。毛15而遠離該機鼻12， 該機腹11之容納空間Ul内 其能夠設為降落傘，該蓋體社人職個降落裝置16， 降落裝置16包括數個連接線161 ^於该降落裝置丨6。該 線161的兩端分別連接於該容訥空個傘面162 ’該連接 162。該蓋體112更設有一個連接 Ul的底部與該傘面 ' ，其相反於該蓋體If/unmanned, the control personnel in the control room on the ground control the unmanned flight H flight, flight and landing. The landing of the unmanned aerial vehicle is carried out with a parachute for landing. The parachute is designed to be purchased. When Lin wants to enter = := to turn off the flight power, and let the parachute at the tail of the machine break away from the two bodies, the Luo Luo umbrella will be deployed at the appropriate time, and the parachute will be unfolded and the replacement page will be amended on May 20, 100. Can complete the purpose of landing. The traditional design places the parachute at the tail, so when the aircraft is landing, the tail will face the sky and the nose will face the ground. When the aircraft is landing, the apparent nose and belly will land first. Although the aircraft is protected by a parachute without serious damage, but the nose and belly are in contact with the ground, the precision equipment collected in the belly of the machine. For example, if the recorder is slightly attacked, the hard disk data in the recorder may be damaged, and the important data recorded by the recorder cannot be provided to the user. Therefore, this creation wants to eliminate or at least alleviate the problems encountered in prior art. [New content] This creation is intended to provide an "aircraft with landing gear" to solve the problems of the prior art. The technical problem that this creation solves first is that when the aircraft is landing, the landing device slowly falls, the belly of the machine is facing the sky, and when the aircraft is landing, the nose and the two vertical tails are in contact with the ground, so that the belly can be protected. Will be in contact with the ground' to further protect the recorder or other precision equipment stored in the belly of the machine from damage. The technical problem to be solved by the present invention is that when the aircraft loses power, the aircraft can control the aircraft to descend and land in a predetermined area by throwing the landing device, and when the landing device is deployed, it can delay the aircraft to Fall down. Other purposes, advantages, and novel features of the present invention will be more apparent from the following detailed description of the replacement page description of the 20th of May, 100, and the related drawings. [Embodiment] The techniques, means, and effects of the present invention are used. The preferred embodiment is described in detail with reference to the drawings, and this is for illustrative purposes only and is not limited by the structure. One. Referring to Figure 1, Figure 2 and Figure 3, the three-dimensional appearance and front view of the flying bandit with the landing gear are created. The aircraft 1 of the present invention comprises a belly 11, a nose 12, a machine back 13, two vertical tails 14 and a tail 15. When the aircraft 1 is flying, the belly 11 is facing the ground, the nose 12 is facing forward, and the body is squeezing] 3 and the vertical tail 14 is facing the Tiangong' _ tail 15 toward the rear, the nose 12 and the nose 12 The opposite ends of the aircraft 1. The knives are located in the belly of the aircraft 1 and collect other precision equipment. When the H i flight chart is not seen, or the recorder or other precision equipment in the 11 can be empty, the aircraft is stored in the belly of the aircraft. The belly n includes the work of collecting information. The body 112' is adjacent to the body, and the space Hi and a cover 112 close the receiving space U1. The hair 15 is away from the nose 12, and the space U1 of the belly 11 can be set as a parachute. The cover body has a landing device 16, and the landing device 16 includes a plurality of connecting lines 161. 6. Both ends of the line 161 are respectively connected to the space 162' of the container 162. The cover body 112 is further provided with a bottom portion connecting the Ul and the umbrella surface ', which is opposite to the cover body
112的一端連接於該傘面162 ^ 參照圖四與圖五，為本創作之飛行器 該飛行器1藉由地面人為操控而進行降落的動作，One end of 112 is connected to the umbrella surface 162. Referring to FIG. 4 and FIG. 5, the aircraft of the present invention is a landing motion of the aircraft 1 by artificial manipulation of the ground.
著該蓋體112而被拋出於該飛行器1之機腹u a 脫離 袭置16隨 之外，該降 落裝置16脫離該容納空間1U時’該飛行器丨隨即佟止牛 力源。此時，該降落裝置16承受風阻，該飛行器丨因= 性移動的影響而持續往前飛，該飛行器丨並受到重力的= 響而會往下墜。該降落裝置16隨著該飛行器1往前飛與S 下墜，該降落裝置16承受相反該飛行器丨方向之風阻，2 該降落裝置16隨即展開。 7 當該飛行器1減速的往前飛且往下墜時，展開後的降 落裝置16承受風阻而緩慢的下墜，因為該飛行器1的下堅 速度大於該降落裴置丨6，因此該飛行器1會位於該降落裝 置16的下方，此時’該飛行器1已完全失去往前飛的動力。 該飛行器1之容納空間U1連接著該降落裝置16之連接線 161 ’該伞面162因為受到該飛行器1的牽制而往下移動， 因此該傘面162往下移動時會受風而展開，同時，該連接 線161結合於該容納空間m，而能夠避免該飛行器1因 為失去動力而完全受到重力影響往下墜落，該降落裝置16 進一步提供下墜時的空氣阻力，使該飛行器丨下墜速度緩 慢，能夠保證在空中下墜的飛行器丨之安全。 參照圖六與圖七，為本創作飛行器著陸之示意圖。當 100年05月20日修正替換頁 該飛行器1失去動力時，該飛行器1藉由拋出該降落裝置 16而能夠控制該飛行器1在預定區域内下降著陸，該降落 裝置16展開時，其能夠延緩該飛行器1往下墜落的速度。 該降落裝置16缓慢落下時，此時，該飛行器1之機腹 11受到該降落裝置16之連接線161的牽制而朝向天空， 該飛行器1降落時，該飛行器1以該機鼻12與該兩個垂直 尾翼14與地面接觸，因此能夠保護該機腹11不會與地面 接觸’該機腹11朝向天空，令收藏於該機腹11内之記錄 器或其他精密設備不會受到損傷。 就以上所述可以歸納出本創作具有以下之優點： 1.本創作『具有降落裝置之飛行器』，其降落時，該降 落裝置緩慢落下，該機腹朝向天空，該飛行器落地時，該 機鼻與該兩個垂直尾翼與地面接觸，因此能夠保護該機腹 不會與地面接觸，進一步保護收藏於機腹内之記錄器或其 他精密設備不會受到損傷。 2.本創作『具有降落裝置之飛行器』，當該飛行器失去 =時，該飛行器藉由拋出該降落裝置而能夠控制該飛行 ^:定區域内下降著陸’該降落裝置展開時，其能夠延 緩邊飛行1§往下墜落。 以之P卩定敉侄貫施例而已，當不能 件==?之範圍’故舉凡數值之變更或等效元 置奐或依本創作申請專利範圍所 飾’皆應㈣本新料细蓋之料。化與修 M413652 100年05月20日修正替換頁 【圖式簡單說明】 圖一：為本創作具有降落裝置之飛行器之立體外觀圖。 圖二：為本創作具有降落裝置之飛行器拋出降落裝置之立 體外觀圖。 圖三：為本創作具有降落裝置之飛行器之側視圖。 圖四：為本創作之飛行器降落之動作圖，表飛行器往前飛 且往下墜之示意圖。 圖五：為本創作之飛行器降落之動作圖，表降落裝置牽制 飛行器下墜之示意圖。 圖六：為本創作飛行器著陸之側視圖。 圖七：為本創作飛行器著陸之前視圖。 【主要元件符號說明】 1 飛行為 11 機腹 111 容納空間 112 蓋體 113 連接線 12 機鼻 13 機背 14 垂直尾翼 15 機尾 16 降落裝置 161 連接線 162 傘面 8When the cover 112 is thrown out of the belly of the aircraft 1 and the detachment of the aircraft is removed, the landing gear 16 is detached from the accommodating space 1U. At this time, the landing device 16 is subjected to the wind resistance, and the aircraft continually flies forward due to the influence of the sexual movement, and the aircraft is slammed by the gravity = and will fall. The landing gear 16 ascends forward and descends with the aircraft 1 and the landing gear 16 is subjected to wind resistance in the opposite direction of the aircraft, 2 and the landing device 16 is deployed. 7 When the aircraft 1 flies forward and descends, the deployed landing gear 16 is subjected to wind resistance and slowly falls, because the lowering speed of the aircraft 1 is greater than the landing gear 丨 6, so the aircraft 1 will be located Below the landing gear 16, at this point the aircraft 1 has completely lost the power to fly forward. The accommodation space U1 of the aircraft 1 is connected to the connection line 161 ′ of the landing device 16 . The umbrella surface 162 is moved downward by the restriction of the aircraft 1 , so that the umbrella surface 162 is exposed to wind when moving downward, and at the same time The connecting wire 161 is coupled to the accommodating space m, and can prevent the aircraft 1 from falling down completely due to the loss of power. The landing device 16 further provides the air resistance at the time of falling, so that the aircraft squats slowly. It can guarantee the safety of the aircraft falling in the air. Referring to Figure 6 and Figure 7, a schematic diagram of the landing of the author aircraft. When the aircraft 1 loses power in the correction replacement page on May 20, 100, the aircraft 1 can control the aircraft 1 to descend and land in a predetermined area by throwing the landing device 16, and when the landing device 16 is deployed, it can Delay the speed at which the aircraft 1 falls down. When the landing device 16 is slowly falling, at this time, the belly 11 of the aircraft 1 is pinched by the connecting line 161 of the landing device 16 and faces the sky. When the aircraft 1 is lowered, the aircraft 1 uses the nose 12 and the two. The vertical tail 14 is in contact with the ground, so that the belly 11 can be protected from contact with the ground. The belly 11 faces the sky, so that the recorder or other precision equipment stored in the belly 11 is not damaged. As far as the above is concerned, it can be concluded that the creation has the following advantages: 1. The creation "an aircraft with a landing gear", when landing, the landing device slowly falls, the belly of the machine faces the sky, and the nose of the aircraft when the aircraft is landing The two vertical tails are in contact with the ground, so that the belly can be protected from contact with the ground, and the recorder or other precision equipment stored in the belly can be further protected from damage. 2. The present invention "an aircraft having a landing gear", when the aircraft loses =, the aircraft can control the flight by throwing the landing device ^: landing in a fixed area" when the landing device is deployed, it can be delayed Fly 1 § and fall down. P 卩 敉侄 敉侄 施 施 , , , , , , , , , , , , , , = = = = = = = = = = = = ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' ' 凡The material. M413652 Correction and replacement page on May 20th, 100th [Simplified illustration of the drawing] Figure 1: This is a three-dimensional appearance of the aircraft with the landing gear. Figure 2: The exterior view of the aircraft throwing the landing gear with the landing gear. Figure 3: A side view of an aircraft with a landing gear for this creation. Figure 4: The action diagram of the landing of the aircraft of this creation, the schematic diagram of the flight of the aircraft flying forward and falling. Figure 5: The action diagram of the landing of the aircraft for this creation, the table landing device is a schematic diagram of the aircraft falling. Figure 6: Side view of the landing of the creative aircraft. Figure 7: Front view of the landing of the creative aircraft. [Main component symbol description] 1 Flight is 11 belly 111 accommodating space 112 cover 113 connecting wire 12 nose 13 back 14 vertical tail 15 tail 16 landing gear 161 connecting line 162 umbrella 8