[go: up one dir, main page]

CN111994285B - Aerospace seat - Google Patents

Aerospace seat Download PDF

Info

Publication number
CN111994285B
CN111994285B CN202010909123.2A CN202010909123A CN111994285B CN 111994285 B CN111994285 B CN 111994285B CN 202010909123 A CN202010909123 A CN 202010909123A CN 111994285 B CN111994285 B CN 111994285B
Authority
CN
China
Prior art keywords
seat
plate
positioning
contact piece
dining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202010909123.2A
Other languages
Chinese (zh)
Other versions
CN111994285A (en
Inventor
何锦霞
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mango Airlines Group Co ltd
Original Assignee
Nanjing Yusheng Robot Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nanjing Yusheng Robot Technology Co Ltd filed Critical Nanjing Yusheng Robot Technology Co Ltd
Priority to CN202010909123.2A priority Critical patent/CN111994285B/en
Publication of CN111994285A publication Critical patent/CN111994285A/en
Application granted granted Critical
Publication of CN111994285B publication Critical patent/CN111994285B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0602Seat modules, i.e. seat systems including furniture separate from the seat itself
    • B64D11/0605Seat modules, i.e. seat systems including furniture separate from the seat itself including tables or desks

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Seats For Vehicles (AREA)

Abstract

The invention relates to the technical field of aviation and aircraft accessories and discloses a seat for aerospace, which comprises a seat body, wherein a carrying handle is movably connected to one side of the top end of a seat plate of the seat body, a supporting seat is fixedly connected to the bottom end of the seat plate of the seat body, a sliding rail is fixedly connected to the bottom end of the supporting seat, a reset tension spring is fixedly connected to one end of an inner cavity of a bottom plate of the supporting seat, the other end of the reset tension spring is fixedly connected with one end of a carrying plate, an anti-falling plate is fixedly sleeved on the outer wall of the carrying plate, which is located in the supporting seat, and a stop block is fixedly mounted on the inner wall of the supporting seat and on one side of the anti-falling plate. This seat for aerospace through setting up movable contact and static contact, can judge whether to accomplish the lock with meal board and button device by whether movable contact and static contact to whether light up to help the crew to confirm fast that the crew does not accomplish with meal board and pack up the action in the cabin by the warning light, thereby be convenient for the crew to carry out going on of the safety inspection work before the aircraft takes off.

Description

一种航空航天用座椅An aerospace seat

技术领域technical field

本发明涉及航空飞机配件技术领域,具体为一种航空航天用座椅。The invention relates to the technical field of aerospace aircraft accessories, in particular to an aerospace seat.

背景技术Background technique

民用飞机座椅主要由椅座、椅背、扶手架以及椅背后部的用餐板组成,分别具备椅背的倚靠角度可调节、扶手架可收起伸展、用餐板可收纳折叠的功能,在乘机体验过程中,飞机上升和下降过程均需要将用餐板收起,以免飞机上升或下降过程中惯性导致用餐板戳伤乘客的事故发生,同时,要求无法放置在机舱行李架上的行李物品放置在前排乘客座椅的下方,防止飞机在飞行过程中行李散落的情况发生。A civil aircraft seat is mainly composed of a seat, a seat back, an armrest frame and a dining board on the back of the chair. It has the functions of adjustable backrest angle, retractable armrest, and retractable dining board. During the experience, the dining board needs to be stowed away during the ascent and descent of the aircraft to avoid the accident that the dining board may hurt passengers due to inertia during the ascent or descent of the aircraft. Below the front passenger seat to prevent luggage from being scattered during the flight.

当前,民用飞机的座椅用餐板均不具有提示收纳警示功能,乘务员要求旅客收纳桌板时,常存在部分旅客不遵守使用规定的情况,需要乘务员依次检查,不仅占用飞机起飞前的准备时间,而且易发生漏检的情况,另一方面,由于飞机座椅前后排的间距空间有限,在将物品放置在前排座椅下方时,取拿均不便,且飞机起飞与下降过程中,依然易发生物品散落的情况,因此,提出一种航空航天用座椅。At present, the seat dining boards of civil aircraft do not have the function of prompting storage and storage. When the flight attendants ask passengers to store the table boards, there are often cases where some passengers do not comply with the use regulations. In addition, it is prone to missed inspections. On the other hand, due to the limited space between the front and rear rows of aircraft seats, it is inconvenient to take items when they are placed under the front seats, and during the take-off and descent of the aircraft, it is still easy to Since items are scattered, an aerospace seat has been proposed.

发明内容SUMMARY OF THE INVENTION

(一)解决的技术问题(1) Technical problems solved

针对现有技术的不足,本发明提供了一种航空航天用座椅,具备便于乘务员检查各座椅桌板收纳情况、座椅下方物品取拿便利等优点,解决了民用飞机的座椅用餐板均不具有提示收纳警示功能,乘务员要求旅客收纳桌板时,常存在部分旅客不遵守使用规定的情况,需要乘务员依次检查,不仅占用飞机起飞前的准备时间,而且易发生漏检的情况,另一方面,由于飞机座椅前后排的间距空间有限,在将物品放置在前排座椅下方时,取拿均不便,且飞机起飞与下降过程中,依然易发生物品散落情况的问题。In view of the deficiencies of the prior art, the present invention provides an aerospace seat, which has the advantages of being convenient for flight attendants to check the storage condition of each seat table board, convenient for taking items under the seat, etc., and solves the problem of seat dining boards in civil aircraft None of them have the function of prompting and storing. When the flight attendant asks passengers to store the desk board, there are often cases where some passengers do not comply with the use regulations, and the flight attendants need to check in sequence, which not only takes up the preparation time before the plane takes off, but also is prone to missed inspections. On the one hand, due to the limited space between the front and rear rows of aircraft seats, it is inconvenient to take items when placing them under the front seats, and during the take-off and descent of the aircraft, the problem of scattered items is still prone to occur.

(二)技术方案(2) Technical solutions

为实现上述便于乘务员检查各座椅桌板收纳情况和座椅下方物品取拿便利的目的,本发明提供如下技术方案:一种航空航天用座椅,包括座椅本体,所述座椅本体座板顶端的一侧活动连接有搭手把,所述座椅本体座板的底端固定连接有支撑座,所述支撑座的底端固定连接有滑轨,所述支撑座底板内腔的一端固定连接有复位拉簧,所述复位拉簧的另一端与载物板的一端固定连接,所述载物板位于支撑座内的外壁固定套接有防脱板,所述支撑座的内壁且位于防脱板的一侧固定安装有挡块,所述载物板的正面固定安装有滑条,所述滑条的外部与支撑座内壁滑动连接,所述载物板顶端的一侧且位于支撑座的背面固定连接有前挡板,所述前挡板正面的顶端铰接有侧撑杆,所述侧撑杆的另一端与载物板顶端的另一侧铰接,所述侧撑杆正面的中部铰接有斜撑杆,所述斜撑杆的另一端与载物板顶端的中部固定连接,所述载物板的一端铰接有后挡板,所述后挡板正面的顶部铰接有启闭装置,所述座椅本体一侧的底部固定安装有挂钩,所述座椅本体座板与椅背的连接轴的正面活动连接有餐板架,所述餐板架的另一端铰接有用餐板,所述用餐板的一端固定安装有定位板,所述用餐板正面顶端的中部开设有固定槽,所述固定槽的内底嵌设有动触片,所述座椅本体一侧的顶端固定安装有纽扣装置,所述纽扣装置的内侧嵌设有静触片,所述座椅本体的顶端固定安装有警示灯。In order to achieve the above-mentioned purpose of facilitating the flight attendants to check the storage conditions of each seat table and the convenience of taking items under the seat, the present invention provides the following technical solution: an aerospace seat, comprising a seat body, the seat body seat A handlebar is movably connected to one side of the top of the board, a support seat is fixedly connected to the bottom end of the seat plate of the seat body, a slide rail is fixedly connected to the bottom end of the support seat, and one end of the inner cavity of the bottom plate of the support seat is fixedly connected. A reset tension spring is fixedly connected, and the other end of the reset tension spring is fixedly connected with one end of the carrier plate. A stopper is fixedly installed on one side of the anti-separation plate, a slide bar is fixedly installed on the front of the object carrier, and the outside of the slider is slidably connected to the inner wall of the support seat, and one side of the top of the object carrier is located at The back of the support base is fixedly connected with a front baffle, the top of the front of the front baffle is hinged with a side strut, the other end of the side strut is hinged with the other side of the top of the load board, and the front of the side strut is hinged. A diagonal strut is hinged in the middle of the slanted strut, the other end of the diagonal strut is fixedly connected with the middle of the top end of the load board, a tailgate is hinged at one end of the load board, and the top of the front of the tailgate is hinged with a starter. A hook is fixedly installed at the bottom of one side of the seat body, a dining plate rack is movably connected to the front of the connecting shaft of the seat plate of the seat body and the seat back, and the other end of the dining plate rack is hinged with a dining plate frame One end of the dining plate is fixedly installed with a positioning plate, the middle of the top of the front of the dining plate is provided with a fixing groove, the inner bottom of the fixing groove is embedded with a moving contact piece, and the top of the seat body is on one side. A button device is fixedly installed, the inner side of the button device is embedded with a static contact piece, and a warning light is fixedly installed on the top of the seat body.

优选的,所述启闭装置包括固定支杆,所述固定支杆的底端与支撑座背面的中部铰接,所述固定支杆的顶端与连轴的外部活动套接,所述连轴的外部且位于固定支杆的背面活动套接有活动支杆,所述活动支杆的底端与后挡板正面的顶部铰接,所述连轴的外部且位于活动支杆的背面活动套接有安装套筒,所述安装套筒的外壁固定连接有固定套筒,所述固定套筒的内部活动套接有固定套杆,所述固定套杆的底端固定连接有紧固拉簧,所述紧固拉簧的底端与固定套筒的内底固定连接,所述固定套杆一侧的顶部开设有定位挂孔,所述定位挂孔与挂钩扣合。Preferably, the opening and closing device includes a fixed support rod, the bottom end of the fixed support rod is hinged with the middle part of the back of the support seat, the top end of the fixed support rod is movably sleeved with the outside of the connecting shaft, and the A movable support rod is movably sleeved outside and located on the back of the fixed support rod, the bottom end of the movable support rod is hinged with the top of the front of the tailgate, and the outer part of the connecting shaft is movably sleeved on the back of the movable support rod. an installation sleeve, the outer wall of the installation sleeve is fixedly connected with a fixed sleeve, the inner of the fixed sleeve is movably sleeved with a fixed sleeve rod, and the bottom end of the fixed sleeve rod is fixedly connected with a fastening tension spring, so The bottom end of the tightening tension spring is fixedly connected with the inner bottom of the fixing sleeve, the top of one side of the fixing sleeve rod is provided with a positioning hanging hole, and the positioning hanging hole is fastened with the hook.

优选的,所述纽扣装置包括锁扣条,所述锁扣条一侧的底部嵌设有静触片,所述锁扣条一侧的中部固定连接有定位轴,所述定位轴的外部活动套接有定位套筒,所述定位套筒的另一端与座椅本体的一侧固定连接,所述定位轴的外壁固定安装有限位块,所述定位套筒的内壁固定安装有定位块。Preferably, the button device includes a locking bar, a bottom of one side of the locking bar is embedded with a static contact piece, a middle part of one side of the locking bar is fixedly connected with a positioning shaft, and the outside of the positioning shaft is movable A positioning sleeve is sleeved, the other end of the positioning sleeve is fixedly connected with one side of the seat body, the outer wall of the positioning shaft is fixedly installed with a limit block, and the inner wall of the positioning sleeve is fixedly installed with a positioning block.

优选的,所述固定支杆和活动支杆的总长度与后挡板和载物板的总长度相同,所述载物板的背面伸出支撑座的背面。Preferably, the total length of the fixed support rod and the movable support rod is the same as the total length of the tailgate and the object board, and the back of the object board protrudes from the back of the support base.

优选的,所述限位块和定位块的数量均设有两个,且两个限位块和两个定位块分别以定位轴的中心轴成对称布置。Preferably, the number of the limit blocks and the positioning blocks is two, and the two limit blocks and the two positioning blocks are respectively arranged symmetrically with respect to the central axis of the positioning shaft.

优选的,所述固定槽与纽扣装置的布置位置以餐板架折叠收起位置为参考相适配布置,且固定槽内嵌设动触片的位置与纽扣装置一侧嵌设静触片的位置相适配布置。Preferably, the arrangement position of the fixing slot and the button device is adapted to be arranged with reference to the folded and retracted position of the plate rack, and the position where the movable contact piece is embedded in the fixing slot is the same as the position where the stationary contact piece is embedded on one side of the button device. position to match.

优选的,所述动触片的一侧与分压电阻的输出端电连接,所述分压电阻的输入端和输出端分别电连接总开关的输出端和警示灯的输入端,所述总开关的输入端与电源的输出端电连接,所述电源的输入端分别与静触片的一侧和警示灯的输出端电连接。Preferably, one side of the moving contact piece is electrically connected to the output end of the voltage dividing resistor, and the input end and the output end of the voltage dividing resistor are electrically connected to the output end of the main switch and the input end of the warning light respectively, and the The input end of the switch is electrically connected with the output end of the power source, and the input end of the power source is electrically connected with one side of the static contact piece and the output end of the warning light respectively.

优选的,所述总开关的安装位置位于机舱乘务员专用座的位置。Preferably, the installation position of the master switch is located at the position of the special seat for the cabin crew.

优选的,所述动触片的导电线由用餐板的内部经用餐板与定位板连接轴的内部转至餐板架的内部,再由餐板架的内部经餐板架与座椅本体连接轴的内部进入座椅本体的内部。Preferably, the conductive wire of the movable contact piece is transferred from the inside of the dining plate to the inside of the dining plate frame through the inside of the connecting shaft of the dining plate and the positioning plate, and then connected to the seat body from the inside of the dining plate frame through the dining plate frame The inside of the shaft enters the inside of the seat body.

优选的,所述静触片的导电线有锁扣条的内部经定位轴和定位套筒进入座椅本体的内部。Preferably, the conductive wire of the static contact piece has the inner portion of the locking strip and enters the interior of the seat body through the positioning shaft and the positioning sleeve.

(三)有益效果(3) Beneficial effects

与现有技术相比,本发明提供了一种航空航天用座椅,具备以下有益效果:Compared with the prior art, the present invention provides an aerospace seat, which has the following beneficial effects:

1、该航空航天用座椅,通过设置动触片和静触片,可由动触片与静触片是否接触来判定用餐板与纽扣装置是否完成扣合,从而由警示灯点亮与否来辅助乘务员快速确认机舱内何处用餐板未完成收起动作,从而便于乘务员进行飞机起飞前的安全检查工作的进行。1. In this aerospace seat, by setting the moving contact piece and the static contact piece, it can be determined whether the dining plate and the button device are fully buckled by whether the moving contact piece and the static contact piece are in contact, so that the warning light is lit or not. The auxiliary flight attendant can quickly confirm where the dining board has not been stowed away in the cabin, so that it is convenient for the flight attendant to carry out the safety inspection before the plane takes off.

2、该航空航天用座椅,通过载物板、前挡板和后挡板,由载物板、前挡板和后挡板组成的座椅下方行李架可对无法置于机舱上方行李架的物品进行存放,同时配合侧撑杆和斜撑杆的侧挡机构以及复位拉簧的拉力回弹机构,可实现稳定存放物品的目的,有效避免飞机起飞或下降时物品散落的情况发生。2. This aerospace seat, through the cargo plate, the front baffle and the rear baffle, the luggage rack under the seat composed of the cargo plate, the front baffle and the rear baffle can be used for the luggage rack that cannot be placed above the cabin. Items are stored in a stable manner, and at the same time, it cooperates with the side stop mechanism of the side struts and diagonal struts and the tension rebound mechanism of the reset tension spring to achieve the purpose of stably storing items and effectively avoid the occurrence of scattered items when the aircraft takes off or descends.

3、该航空航天用座椅,通过设置启闭装置,由旅客按压固定套筒,使得活动支杆撑开后挡板,再由后挡板拉动载物板从支撑座的下方伸出,完成取拿物品动作后,将定位挂孔与挂钩扣接,并在复位拉簧的拉力回弹作用下,将载物板收回至支撑座的下方,从而便于旅客直接取拿物品,使用方便快捷。3. For the aerospace seat, by setting the opening and closing device, the passenger presses the fixed sleeve, so that the movable support rod supports the rear baffle, and then the rear baffle pulls the loading plate to extend from the bottom of the support seat, and the completion is completed. After taking the object, the positioning hanging hole is fastened to the hook, and the loading plate is retracted to the bottom of the support seat under the rebounding force of the reset tension spring, so that the passenger can directly take the object, which is convenient and quick to use.

附图说明Description of drawings

图1为本发明结构示意图;Fig. 1 is the structural representation of the present invention;

图2为本发明图1的启闭装置处局部放大示意图;Fig. 2 is the partial enlarged schematic diagram of the opening and closing device of Fig. 1 of the present invention;

图3为本发明用餐板侧视图;Fig. 3 is the side view of the dining board of the present invention;

图4为本发明启闭装置侧视图;Figure 4 is a side view of the opening and closing device of the present invention;

图5为本发明图1的A处放大示意图;Fig. 5 is the enlarged schematic diagram of the place A of Fig. 1 of the present invention;

图6为本发明纽扣装置剖视图;6 is a sectional view of the button device of the present invention;

图7为本发明动触片与静触片电路连接示意图。7 is a schematic diagram of the circuit connection between the moving contact piece and the static contact piece of the present invention.

图中:1、座椅本体;2、搭手把;3、支撑座;4、滑轨;5、复位拉簧;6、载物板;7、防脱板;8、挡块;9、滑条;10、前挡板;11、侧撑杆;12、斜撑杆;13、后挡板;14、启闭装置;141、固定支杆;142、连轴;143、活动支杆;144、安装套筒;145、固定套筒;146、固定套杆;147、紧固拉簧;148、定位挂孔;15、挂钩;16、餐板架;17、用餐板;18、定位板;19、固定槽;20、动触片;21、纽扣装置;211、锁扣条;212、定位轴;213、定位套筒;214、限位块;215、定位块;22、静触片;23、警示灯;24、分压电阻;25、总开关;26、电源。In the picture: 1. Seat body; 2. Handlebar; 3. Support seat; 4. Slide rail; 5. Return tension spring; 6. Load plate; 7. Anti-drop plate; Slider; 10. Front baffle; 11. Side strut; 12. Diagonal strut; 13. Back baffle; 14. Opening and closing device; 141, Fixed strut; 142, Connecting shaft; 143, Active strut; 144, installation sleeve; 145, fixed sleeve; 146, fixed sleeve rod; 147, tightening tension spring; 148, positioning hanging hole; 15, hook; 16, dining plate rack; 17, dining plate; 18, positioning plate ;19, fixed slot; 20, moving contact piece; 21, button device; 211, locking strip; 212, positioning shaft; 213, positioning sleeve; 214, limit block; 215, positioning block; 22, static contact piece ; 23, warning light; 24, divider resistor; 25, main switch; 26, power supply.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

请参阅图1-7,一种航空航天用座椅,包括座椅本体1,座椅本体1座板顶端的一侧活动连接有搭手把2,座椅本体1座板的底端固定连接有支撑座3,支撑座3的底端固定连接有滑轨4,滑轨4与机舱地板的滑道固定连接,连接方式采用现有技术中的锚栓固定,支撑座3底板内腔的一端固定连接有复位拉簧5,复位拉簧5的另一端与载物板6的一端固定连接,载物板6位于支撑座3内的外壁固定套接有防脱板7,支撑座3的内壁且位于防脱板7的一侧固定安装有挡块8,载物板6的正面固定安装有滑条9,滑条9的外部与支撑座3内壁滑动连接,载物板6顶端的一侧且位于支撑座3的背面固定连接有前挡板10,前挡板10正面的顶端铰接有侧撑杆11,侧撑杆11的另一端与载物板6顶端的另一侧铰接,侧撑杆11正面的中部铰接有斜撑杆12,斜撑杆12的另一端与载物板6顶端的中部固定连接,载物板6的一端铰接有后挡板13,后挡板13正面的顶部铰接有启闭装置14,启闭装置14包括固定支杆141,固定支杆141的底端与支撑座3背面的中部铰接,固定支杆141的顶端与连轴142的外部活动套接,连轴142的外部且位于固定支杆141的背面活动套接有活动支杆143,固定支杆141和活动支杆143的总长度与后挡板13和载物板6的总长度相同,载物板6的背面伸出支撑座3的背面,支撑座3的背面开设有与载物板6的厚度相适配的滑槽,且防脱板7的高度大于支撑座3背面开设的滑槽宽度,以此保证载物板6与支撑座3背面的滑动连接,且防脱板7不会脱离支撑座3的内部,活动支杆143的底端与后挡板13正面的顶部铰接,连轴142的外部且位于活动支杆143的背面活动套接有安装套筒144,安装套筒144的外壁固定连接有固定套筒145,固定套筒145的内部活动套接有固定套杆146,固定套杆146的底端固定连接有紧固拉簧147,紧固拉簧147的底端与固定套筒145的内底固定连接,固定套杆146一侧的顶部开设有定位挂孔148,定位挂孔148与挂钩15扣合,座椅本体1一侧的底部固定安装有挂钩15,座椅本体1座板与椅背的连接轴的正面活动连接有餐板架16,餐板架16与座椅本体1的安装方式采用现已公开的座椅安装方式,将餐板架16与座椅本体1的不动轴端活动连接,餐板架16的另一端铰接有用餐板17,用餐板17的一端固定安装有定位板18,定位板18与餐板架16一端的伸出板形成限位机构,防止用餐板17在餐板架16的一端过度转动,保证用餐板17转动最大限度处的水平,用餐板17正面顶端的中部开设有固定槽19,固定槽19与纽扣装置21的布置位置以餐板架16折叠收起位置为参考相适配布置,且固定槽19内嵌设动触片20的位置与纽扣装置21一侧嵌设静触片22的位置相适配布置,餐板架16收起,并将用餐板17收起,使得锁扣条211恰好能够对用餐板17处的固定槽19进行扣合,同时,动触片20与静触片22接触,固定槽19的内底嵌设有动触片20,动触片20的一侧与分压电阻24的输出端电连接,分压电阻24的输入端和输出端分别电连接总开关25的输出端和警示灯23的输入端,总开关25的安装位置位于机舱乘务员专用座的位置,由乘务员确定并开始进行安全检查,总开关25的输入端与电源26的输出端电连接,电源26的输入端分别与静触片22的一侧和警示灯23的输出端电连接,动触片20的导电线由用餐板17的内部经用餐板17与定位板18连接轴的内部转至餐板架16的内部,再由餐板架16的内部经餐板架16与座椅本体1连接轴的内部进入座椅本体1的内部,静触片22的导电线有锁扣条211的内部经定位轴212和定位套筒213进入座椅本体1的内部,座椅本体1一侧的顶端固定安装有纽扣装置21,纽扣装置21包括锁扣条211,锁扣条211一侧的底部嵌设有静触片22,锁扣条211一侧的中部固定连接有定位轴212,定位轴212的外部活动套接有定位套筒213,定位套筒213的另一端与座椅本体1的一侧固定连接,定位轴212的外壁固定安装有限位块214,定位套筒213的内壁固定安装有定位块215,限位块214和定位块215的数量均设有两个,且两个限位块214和两个定位块215分别以定位轴212的中心轴成对称布置,通过设置限位块214和定位块215,由限位块214和定位块215限制定位轴212相对定位套筒213的转动角度,从而将锁扣条211的转动角度限制在180°内,防止静触片22的导电线在锁扣条211内被过度扭转而脱落,纽扣装置21的内侧嵌设有静触片22,座椅本体1的顶端固定安装有警示灯23。1-7, an aerospace seat includes a seat body 1, a handle 2 is movably connected to one side of the top of the seat plate of the seat body 1, and the bottom end of the seat plate of the seat body 1 is fixedly connected There is a support base 3, the bottom end of the support base 3 is fixedly connected with a slide rail 4, and the slide rail 4 is fixedly connected with the slideway of the engine room floor. A reset tension spring 5 is fixedly connected, and the other end of the reset tension spring 5 is fixedly connected with one end of the object carrier 6 . And a stopper 8 is fixedly installed on one side of the anti-separation plate 7, a sliding bar 9 is fixedly installed on the front of the object carrying plate 6, the outer part of the sliding bar 9 is slidably connected with the inner wall of the support base 3, and one side of the top of the object carrying plate 6 is slidably connected. And the front baffle 10 is fixedly connected to the back of the support base 3, the top of the front baffle 10 is hinged with a side strut 11, and the other end of the side strut 11 is hinged with the other side of the top of the load board 6, and the side brace A diagonal strut 12 is hinged to the middle of the front of the rod 11 , and the other end of the diagonal strut 12 is fixedly connected to the middle of the top of the object carrier 6 , and one end of the object carrier 6 is hinged with a rear baffle 13 , and the top of the front of the rear baffle 13 is hinged. The opening and closing device 14 is hingedly connected. The opening and closing device 14 includes a fixed support rod 141. The bottom end of the fixed support rod 141 is hinged with the middle part of the back of the support base 3. A movable strut 143 is movably sleeved on the outside of the shaft 142 and located on the back of the fixed strut 141. The total length of the fixed strut 141 and the movable strut 143 is the same as the total length of the rear baffle 13 and the load board 6. The back of the plate 6 protrudes from the back of the support seat 3, the back of the support seat 3 is provided with a chute that is adapted to the thickness of the carrier plate 6, and the height of the anti-detachment plate 7 is greater than the width of the chute opened on the back of the support seat 3 , so as to ensure the sliding connection between the loading plate 6 and the back of the support base 3, and the anti-detachment plate 7 will not be separated from the interior of the support base 3, and the bottom end of the movable support rod 143 is hinged with the top of the front of the rear baffle 13, and the connecting shaft An installation sleeve 144 is movably sleeved on the outside of the 142 and located on the back of the movable strut 143, the outer wall of the installation sleeve 144 is fixedly connected with a fixed sleeve 145, and the inner part of the fixed sleeve 145 is movably sleeved with a fixed sleeve rod 146. The bottom end of the sleeve rod 146 is fixedly connected with a tightening tension spring 147, and the bottom end of the tightening tension spring 147 is fixedly connected with the inner bottom of the fixed sleeve 145. The top of one side of the fixed sleeve rod 146 is provided with a positioning hanging hole 148 for positioning The hanging hole 148 is buckled with the hook 15, the bottom of one side of the seat body 1 is fixedly installed with the hook 15, and the front side of the connecting shaft of the seat plate and the seat back of the seat body 1 is movably connected with a dining plate frame 16, and the dining plate frame 16 is connected to the front side of the connecting shaft. The installation method of the seat body 1 adopts the disclosed seat installation method. The dining plate frame 16 is movably connected with the fixed shaft end of the seat body 1. The other end of the dining plate frame 16 is hinged with a dining plate 17. The dining plate One end of the 17 is fixedly installed with a positioning plate 18, and the positioning plate 18 and the protruding plate at one end of the meal plate rack 16 form a limiting mechanism to prevent the meal plate 17 from being in the position of the meal plate rack 16. One end is over-rotated to ensure the level of the maximum rotation of the dining plate 17. A fixing groove 19 is provided in the middle of the front top of the dining plate 17. The arrangement position of the fixing groove 19 and the button device 21 is based on the folded and retracted position of the dining plate frame 16 as a reference. The arrangement is adapted, and the position where the movable contact piece 20 is embedded in the fixing groove 19 is adapted to the position where the static contact piece 22 is embedded on one side of the button device 21 , the dining plate rack 16 is retracted, and the dining plate 17 is retracted , so that the locking bar 211 can just snap the fixing groove 19 at the dining board 17, and at the same time, the moving contact piece 20 contacts the static contact piece 22, and the inner bottom of the fixing groove 19 is embedded with the moving contact piece 20. One side of the chip 20 is electrically connected to the output end of the voltage dividing resistor 24, and the input end and the output end of the voltage dividing resistor 24 are respectively electrically connected to the output end of the main switch 25 and the input end of the warning light 23, and the installation position of the main switch 25 is located at The position of the special seat for the cabin crew is determined by the flight attendant and the safety inspection is started. The input end of the main switch 25 is electrically connected to the output end of the power supply 26, and the input end of the power supply 26 is respectively connected to one side of the static contact piece 22 and the side of the warning light 23. The output end is electrically connected, and the conductive wire of the movable contact piece 20 is transferred from the inside of the dining plate 17 through the inside of the connecting shaft of the dining plate 17 and the positioning plate 18 to the inside of the dining plate rack 16, and then from the inside of the dining plate rack 16 through the dining plate The inside of the connecting shaft of the frame 16 and the seat body 1 enters the interior of the seat body 1, the conductive wire of the static contact piece 22 and the interior of the locking strip 211 enter the interior of the seat body 1 through the positioning shaft 212 and the positioning sleeve 213, A button device 21 is fixedly installed on the top of one side of the seat body 1 . The button device 21 includes a locking bar 211 . The bottom of one side of the locking bar 211 is embedded with a static contact piece 22 . There is a positioning shaft 212, a positioning sleeve 213 is movably sleeved on the outside of the positioning shaft 212, the other end of the positioning sleeve 213 is fixedly connected to one side of the seat body 1, and the outer wall of the positioning shaft 212 is fixedly installed with a limit block 214, positioning A positioning block 215 is fixedly installed on the inner wall of the sleeve 213 , the number of the limit block 214 and the positioning block 215 is two, and the two limit blocks 214 and the two positioning blocks 215 are respectively formed by the central axis of the positioning shaft 212 . Symmetrical arrangement, by setting the limit block 214 and the positioning block 215, the limit block 214 and the positioning block 215 limit the rotation angle of the positioning shaft 212 relative to the positioning sleeve 213, thereby limiting the rotation angle of the locking bar 211 within 180° , to prevent the conductive wire of the static contact piece 22 from being excessively twisted and falling off in the locking bar 211 .

工作时,由乘务员闭合总开关25,警示灯23点亮的位置即为用餐板17与纽扣装置21未扣合收起的位置,而用餐板17与纽扣装置21扣合收起的位置,动触片20与静触片22接触,警示灯23短路熄灭,存取支撑座3下方的行李物品时,拔开定位挂孔148与挂钩15的扣合状态,按压固定套筒145,在固定支杆141的定点支撑作用下,活动支杆143将后挡板13撑开并转动,由后挡板13带动载物板6从支撑座3内滑出,同时拉伸复位拉簧5,将行李放置或取出载物板6后,松开固定套筒145,在复位拉簧5的拉力回弹作用下,载物板6滑入支撑座3内,并使得活动支杆143升起,带动后挡板13转变为垂直状态,然后拉伸固定套杆146,使得定位挂孔148与挂钩15再次扣合。When working, the main switch 25 is closed by the flight attendant, and the position where the warning light 23 is lit is the position where the dining board 17 and the button device 21 are not buckled and stowed, and the position where the dining board 17 and the button device 21 are buckled and stowed. The contact piece 20 is in contact with the static contact piece 22, and the warning light 23 is short-circuited and extinguished. When accessing the luggage under the support base 3, pull out the buckled state between the positioning hole 148 and the hook 15, and press the fixing sleeve 145. Under the fixed-point support of the rod 141, the movable support rod 143 spreads and rotates the tailgate 13, and the tailgate 13 drives the loading board 6 to slide out from the support seat 3, and at the same time stretches the reset tension spring 5, so that the luggage can be moved. After placing or taking out the loading plate 6, loosen the fixing sleeve 145, and under the rebounding action of the tension spring 5, the loading plate 6 slides into the support base 3, and makes the movable support rod 143 rise, driving the rear The baffle 13 is transformed into a vertical state, and then the fixing sleeve rod 146 is stretched, so that the positioning hanging hole 148 is engaged with the hook 15 again.

综上所述,该航空航天用座椅,通过设置动触片20和静触片22,可由动触片20与静触片22是否接触来判定用餐板17与纽扣装置21是否完成扣合,从而由警示灯23点亮与否来辅助乘务员快速确认机舱内何处用餐板未完成收起动作,从而便于乘务员进行飞机起飞前的安全检查工作的进行;通过载物板6、前挡板10和后挡板13,由载物板6、前挡板10和后挡板13组成的座椅下方行李架可对无法置于机舱上方行李架的物品进行存放,同时配合侧撑杆11和斜撑杆12的侧挡机构以及复位拉簧5的拉力回弹机构,可实现稳定存放物品的目的,有效避免飞机起飞或下降时物品散落的情况发生;通过设置启闭装置14,由旅客按压固定套筒145,使得活动支杆143撑开后挡板13,再由后挡板13拉动载物板6从支撑座3的下方伸出,完成取拿物品动作后,将定位挂孔148与挂钩15扣接,并在复位拉簧5的拉力回弹作用下,将载物板6收回至支撑座3的下方,从而便于旅客直接取拿物品,使用方便快捷;解决了民用飞机的座椅用餐板17均不具有提示收纳警示功能,乘务员要求旅客收纳桌板时,常存在部分旅客不遵守使用规定的情况,需要乘务员依次检查,不仅占用飞机起飞前的准备时间,而且易发生漏检的情况,另一方面,由于飞机座椅前后排的间距空间有限,在将物品放置在前排座椅下方时,取拿均不便,且飞机起飞与下降过程中,依然易发生物品散落情况的问题。To sum up, in this aerospace seat, by arranging the movable contact piece 20 and the static contact piece 22, it can be determined whether the dining plate 17 and the button device 21 are fully buckled by whether the movable contact piece 20 and the static contact piece 22 are in contact. Therefore, whether the warning light 23 is lit or not assists the flight attendant to quickly confirm where the dining board has not completed the retraction action in the cabin, so as to facilitate the flight attendant to carry out the safety inspection work before the aircraft takes off; And the tailgate 13, the luggage rack under the seat composed of the cargo plate 6, the front baffle 10 and the tailgate 13 can store the items that cannot be placed in the luggage rack above the cabin, and at the same time cooperate with the side struts 11 and the inclined The side stop mechanism of the strut 12 and the tension rebound mechanism of the reset tension spring 5 can achieve the purpose of stably storing items and effectively avoid the occurrence of scattered items when the aircraft takes off or descends; by setting the opening and closing device 14, it is pressed and fixed by passengers The sleeve 145 makes the movable strut 143 support the rear baffle 13, and then the rear baffle 13 pulls the object carrier 6 to extend from the bottom of the support base 3. After the action of picking up the object is completed, the positioning hanging hole 148 is connected to the hook. 15 is buckled, and under the action of the tension and rebound of the reset tension spring 5, the loading plate 6 is retracted to the bottom of the support base 3, so that it is convenient for passengers to directly take the items, which is convenient and quick to use; it solves the problem of seat dining in civil aircraft. The board 17 does not have the function of prompting storage and warning. When the flight attendant asks passengers to store the table board, there are often cases that some passengers do not comply with the use regulations. The flight attendants need to check in sequence, which not only takes up the preparation time before the plane takes off, but also easily misses the situation. On the other hand, due to the limited space between the front and rear rows of aircraft seats, it is inconvenient to take items when placing them under the front seats, and during the take-off and descent of the aircraft, the problem of scattered items is still prone to occur.

需要说明的是,在本文中,诸如第一和第二等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来,而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且,术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含,从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素,而且还包括没有明确列出的其他要素,或者是还包括为这种过程、方法、物品或者设备所固有的要素。It should be noted that, in this document, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any relationship between these entities or operations. any such actual relationship or sequence exists. Moreover, the terms "comprising", "comprising" or any other variation thereof are intended to encompass non-exclusive inclusion such that a process, method, article or device comprising a list of elements includes not only those elements, but also includes not explicitly listed or other elements inherent to such a process, method, article or apparatus.

尽管已经示出和描述了本发明的实施例,对于本领域的普通技术人员而言,可以理解在不脱离本发明的原理和精神的情况下可以对这些实施例进行多种变化、修改、替换和变型,本发明的范围由所附权利要求及其等同物限定。Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, and substitutions can be made in these embodiments without departing from the principle and spirit of the invention and modifications, the scope of the present invention is defined by the appended claims and their equivalents.

Claims (1)

1.一种航空航天用座椅,其特征在于:包括座椅本体(1),所述座椅本体(1)座板顶端的一侧活动连接有搭手把(2),所述座椅本体(1)座板的底端固定连接有支撑座(3),所述支撑座(3)的底端固定连接有滑轨(4),所述支撑座(3)底板内腔的一端固定连接有复位拉簧(5),所述复位拉簧(5)的另一端与载物板(6)的一端固定连接,所述载物板(6)位于支撑座(3)内的外壁固定套接有防脱板(7),所述支撑座(3)的内壁且位于防脱板(7)的一侧固定安装有挡块(8),所述载物板(6)的正面固定安装有滑条(9),所述滑条(9)的外部与支撑座(3)内壁滑动连接,所述载物板(6)顶端的一侧且位于支撑座(3)的背面固定连接有前挡板(10),所述前挡板(10)正面的顶端铰接有侧撑杆(11),所述侧撑杆(11)的另一端与载物板(6)顶端的另一侧铰接,所述侧撑杆(11)正面的中部铰接有斜撑杆(12),所述斜撑杆(12)的另一端与载物板(6)顶端的中部固定连接,所述载物板(6)的一端铰接有后挡板(13),所述后挡板(13)正面的顶部铰接有启闭装置(14),所述座椅本体(1)一侧的底部固定安装有挂钩(15),所述座椅本体(1)座板与椅背的连接轴的正面活动连接有餐板架(16),所述餐板架(16)的另一端铰接有用餐板(17),所述用餐板(17)的一端固定安装有定位板(18),所述用餐板(17)正面顶端的中部开设有固定槽(19),所述固定槽(19)的内底嵌设有动触片(20),所述座椅本体(1)一侧的顶端固定安装有纽扣装置(21),所述纽扣装置(21)的内侧嵌设有静触片(22),所述座椅本体(1)的顶端固定安装有警示灯(23);1. An aerospace seat, characterized by comprising a seat body (1), a handlebar (2) is movably connected to one side of the top of the seat plate of the seat body (1), and the seat is The bottom end of the base plate of the main body (1) is fixedly connected with a support seat (3), the bottom end of the support seat (3) is fixedly connected with a slide rail (4), and one end of the inner cavity of the bottom plate of the support seat (3) is fixed A reset tension spring (5) is connected, the other end of the reset tension spring (5) is fixedly connected with one end of the object carrier (6), and the outer wall of the object carrier (6) located in the support seat (3) is fixed An anti-separation plate (7) is sleeved, and a stopper (8) is fixedly installed on the inner wall of the support seat (3) and located on one side of the anti-separation plate (7), and the front of the object carrying plate (6) is fixed A slider (9) is installed, the outside of the slider (9) is slidably connected to the inner wall of the support seat (3), and one side of the top end of the object carrier (6) is fixedly connected to the back of the support seat (3) There is a front baffle (10), the top of the front of the front baffle (10) is hinged with a side strut (11), and the other end of the side strut (11) is connected to the other end of the top of the load board (6). Side hinge, the middle part of the front side of the side strut (11) is hinged with a diagonal strut (12), the other end of the diagonal strut (12) is fixedly connected with the middle part of the top end of the object carrier (6), the carrier One end of the object board (6) is hinged with a tailgate (13), the top of the front of the tailgate (13) is hinged with an opening and closing device (14), and the bottom of one side of the seat body (1) is fixedly installed There is a hook (15), a dining plate frame (16) is movably connected to the front of the connecting shaft of the seat plate and the seat back of the seat body (1), and a dining plate (16) is hinged at the other end of the dining plate frame (16). 17), a positioning plate (18) is fixedly installed at one end of the dining board (17), a fixing groove (19) is opened in the middle of the top of the front of the dining board (17), and the inner bottom of the fixing groove (19) is A moving contact piece (20) is embedded, a button device (21) is fixedly installed on the top end of one side of the seat body (1), and a static contact piece (22) is embedded in the inner side of the button device (21). A warning light (23) is fixedly installed on the top of the seat body (1); 所述启闭装置(14)包括固定支杆(141),所述固定支杆(141)的底端与支撑座(3)背面的中部铰接,所述固定支杆(141)的顶端与连轴(142)的外部活动套接,所述连轴(142)的外部且位于固定支杆(141)的背面活动套接有活动支杆(143),所述活动支杆(143)的底端与后挡板(13)正面的顶部铰接,所述连轴(142)的外部且位于活动支杆(143)的背面活动套接有安装套筒(144),所述安装套筒(144)的外壁固定连接有固定套筒(145),所述固定套筒(145)的内部活动套接有固定套杆(146),所述固定套杆(146)的底端固定连接有紧固拉簧(147),所述紧固拉簧(147)的底端与固定套筒(145)的内底固定连接,所述固定套杆(146)一侧的顶部开设有定位挂孔(148),所述定位挂孔(148)与挂钩(15)扣合;The opening and closing device (14) includes a fixed support rod (141), the bottom end of the fixed support rod (141) is hinged with the middle part of the back of the support seat (3), and the top end of the fixed support rod (141) is connected to the A movable support rod (143) is movably sleeved on the outside of the shaft (142) and located on the back of the fixed support rod (141), and the bottom of the movable support rod (143) is movably sleeved on the outside of the shaft (142). The end is hinged to the top of the front of the rear baffle (13), and a mounting sleeve (144) is movably sleeved on the outside of the connecting shaft (142) and located at the back of the movable strut (143), and the mounting sleeve (144) A fixing sleeve (145) is fixedly connected to the outer wall of the A tension spring (147), the bottom end of the tightening tension spring (147) is fixedly connected with the inner bottom of the fixing sleeve (145), and the top of one side of the fixing sleeve rod (146) is provided with a positioning hanging hole (148) ), the positioning hanging hole (148) is engaged with the hook (15); 所述纽扣装置(21)包括锁扣条(211),所述锁扣条(211)一侧的底部嵌设有静触片(22),所述锁扣条(211)一侧的中部固定连接有定位轴(212),所述定位轴(212)的外部活动套接有定位套筒(213),所述定位套筒(213)的另一端与座椅本体(1)的一侧固定连接,所述定位轴(212)的外壁固定安装有限位块(214),所述定位套筒(213)的内壁固定安装有定位块(215);The button device (21) includes a locking bar (211), a static contact piece (22) is embedded in the bottom of one side of the locking bar (211), and a middle part of one side of the locking bar (211) is fixed A positioning shaft (212) is connected, and a positioning sleeve (213) is movably sleeved on the outside of the positioning shaft (212), and the other end of the positioning sleeve (213) is fixed to one side of the seat body (1). connection, the outer wall of the positioning shaft (212) is fixedly installed with a limiting block (214), and the inner wall of the positioning sleeve (213) is fixedly installed with a positioning block (215); 所述固定支杆(141)和活动支杆(143)的总长度与后挡板(13)和载物板(6)的总长度相同,所述载物板(6)的背面伸出支撑座(3)的背面;The total length of the fixed support rod (141) and the movable support rod (143) is the same as the total length of the rear baffle (13) and the load board (6), and the back of the load board (6) protrudes to support the back of the seat (3); 所述限位块(214)和定位块(215)的数量均设有两个,且两个限位块(214)和两个定位块(215)分别以定位轴(212)的中心轴成对称布置;The number of the limit blocks (214) and the positioning blocks (215) is two, and the two limit blocks (214) and the two positioning blocks (215) are respectively formed by the central axis of the positioning shaft (212). symmetrical arrangement; 所述固定槽(19)与纽扣装置(21)的布置位置以餐板架(16)折叠收起位置为参考相适配布置,且固定槽(19)内嵌设动触片(20)的位置与纽扣装置(21)一侧嵌设静触片(22)的位置相适配布置;The arrangement position of the fixing groove (19) and the button device (21) is adapted and arranged with reference to the folded and retracted position of the plate rack (16), and the fixing groove (19) is embedded with the movable contact piece (20). The position is adapted to the position where the static contact piece (22) is embedded on one side of the button device (21); 所述动触片(20)的一侧与分压电阻(24)的输出端电连接,所述分压电阻(24)的输入端和输出端分别电连接总开关(25)的输出端和警示灯(23)的输入端,所述总开关(25)的输入端与电源(26)的输出端电连接,所述电源(26)的输入端分别与静触片(22)的一侧和警示灯(23)的输出端电连接;所述总开关(25)的安装位置位于机舱乘务员专用座的位置;One side of the movable contact piece (20) is electrically connected to the output end of the voltage dividing resistor (24), and the input end and the output end of the voltage dividing resistor (24) are respectively electrically connected to the output end and the output end of the main switch (25). The input end of the warning light (23), the input end of the main switch (25) is electrically connected with the output end of the power supply (26), and the input end of the power supply (26) is respectively connected to one side of the static contact piece (22) is electrically connected with the output end of the warning light (23); the installation position of the main switch (25) is located at the position of the special seat for the cabin crew; 所述动触片(20)的导电线由用餐板(17)的内部经用餐板(17)与定位板(18)连接轴的内部转至餐板架(16)的内部,再由餐板架(16)的内部经餐板架(16)与座椅本体(1)连接轴的内部进入座椅本体(1)的内部;The conductive wire of the movable contact piece (20) is transferred from the inside of the dining plate (17) through the inside of the connecting shaft of the dining plate (17) and the positioning plate (18) to the inside of the dining plate frame (16), and then from the dining plate (17) to the inside of the dining plate frame (16). The interior of the frame (16) enters the interior of the seat body (1) through the interior of the connecting shaft between the meal plate frame (16) and the seat body (1); 所述静触片(22)的导电线有锁扣条(211)的内部经定位轴(212)和定位套筒(213)进入座椅本体(1)的内部;The conductive wire of the static contact piece (22) has a locking bar (211) inside the seat body (1) through a positioning shaft (212) and a positioning sleeve (213); 乘务员闭合总开关,警示灯点亮的位置即为用餐板与纽扣装置未扣合收起的位置,而用餐板与纽扣装置扣合收起的位置,动触片与静触片接触,警示灯短路熄灭,存取支撑座下方的行李物品时,拔开定位挂孔与挂钩的扣合状态,按压固定套筒,在固定支杆的定点支撑作用下,活动支杆将后挡板撑开并转动,由后挡板带动载物板从支撑座内滑出,同时拉伸复位拉簧,将行李放置或取出载物板后,松开固定套筒,在复位拉簧的拉力回弹作用下,载物板滑入支撑座内,并使得活动支杆升起,带动后挡板转变为垂直状态,然后拉伸固定套杆,使得定位挂孔与挂钩再次扣合。When the flight attendant closes the main switch, the position where the warning light is lit is the position where the dining board and the button device are not buckled and stowed, and the position where the dining board and the button device are buckled and stowed, the moving contact piece is in contact with the static contact piece, and the warning light The short circuit is extinguished. When accessing the luggage under the support seat, pull out the buckled state between the positioning hanging hole and the hook, press the fixed sleeve, and under the fixed-point support of the fixed support rod, the movable support rod will support the tailgate and open it. Rotate, the tailgate will drive the loading board to slide out from the support seat, and at the same time stretch the reset tension spring, after placing the luggage or taking out the loading board, release the fixed sleeve, under the rebound effect of the reset tension spring , the loading board slides into the support seat, and the movable support rod is raised, which drives the tailgate to change to a vertical state, and then stretches the fixed sleeve rod, so that the positioning hanging hole and the hook are buckled again.
CN202010909123.2A 2020-09-02 2020-09-02 Aerospace seat Active CN111994285B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010909123.2A CN111994285B (en) 2020-09-02 2020-09-02 Aerospace seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010909123.2A CN111994285B (en) 2020-09-02 2020-09-02 Aerospace seat

Publications (2)

Publication Number Publication Date
CN111994285A CN111994285A (en) 2020-11-27
CN111994285B true CN111994285B (en) 2022-07-19

Family

ID=73465130

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010909123.2A Active CN111994285B (en) 2020-09-02 2020-09-02 Aerospace seat

Country Status (1)

Country Link
CN (1) CN111994285B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2464569Y (en) * 2001-02-19 2001-12-12 财团法人工业技术研究院 A movable luggage lever seat
CN101575006A (en) * 2009-06-05 2009-11-11 吴速 Media and communication system integrated by a dining board in front of aircraft passenger seats
CN204055707U (en) * 2014-05-06 2014-12-31 王庚启 With the seat belt apparatus of annunciator or display lamp on a kind of aircraft
CN204496670U (en) * 2015-04-18 2015-07-22 李俊楠 A kind of tableware uses alarm set
CN106114870A (en) * 2010-10-18 2016-11-16 祖迪雅克座椅法国公司 Passenger seat component and many aspects thereof
CN107117317A (en) * 2017-05-04 2017-09-01 中国航空工业集团公司西安飞机设计研究所 A kind of luggage bracket component under aircraft seat
CN208530859U (en) * 2018-06-22 2019-02-22 苏州昊信精密机械有限公司 A kind of preceding leg device of aircraft seat

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8826830B2 (en) * 2011-10-13 2014-09-09 Nick Pajic Tray table with rotatable inner tray for electronic device docking

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2464569Y (en) * 2001-02-19 2001-12-12 财团法人工业技术研究院 A movable luggage lever seat
CN101575006A (en) * 2009-06-05 2009-11-11 吴速 Media and communication system integrated by a dining board in front of aircraft passenger seats
CN106114870A (en) * 2010-10-18 2016-11-16 祖迪雅克座椅法国公司 Passenger seat component and many aspects thereof
CN204055707U (en) * 2014-05-06 2014-12-31 王庚启 With the seat belt apparatus of annunciator or display lamp on a kind of aircraft
CN204496670U (en) * 2015-04-18 2015-07-22 李俊楠 A kind of tableware uses alarm set
CN107117317A (en) * 2017-05-04 2017-09-01 中国航空工业集团公司西安飞机设计研究所 A kind of luggage bracket component under aircraft seat
CN208530859U (en) * 2018-06-22 2019-02-22 苏州昊信精密机械有限公司 A kind of preceding leg device of aircraft seat

Also Published As

Publication number Publication date
CN111994285A (en) 2020-11-27

Similar Documents

Publication Publication Date Title
US10875652B2 (en) Passenger tray table
US3632161A (en) Side arm stowable table
US8770659B2 (en) Self-stowing jumpseat for aircraft
US10689120B2 (en) Stowable reversible seat
US9573687B2 (en) Laterally-expanding tray table
US7708327B2 (en) Vehicle cargo floor organizer
GB2473927A (en) A folding golf cart
CN115891792A (en) Chair armrest integrated with table plate and touch screen
CN111994285B (en) Aerospace seat
US2352721A (en) Parachute and automatic opening device therefor
CN208216613U (en) One kind can plug-type passenger car luggage rack
CN206664389U (en) A kind of automobile rear seat table plate with folding hand rail
CN108454519A (en) One kind can plug-type passenger car luggage rack
CN205553959U (en) a vehicle
US2585742A (en) Collapsible table mountable on automobile seat
CN110481737B (en) Flexible foldable wing device applied to underwater robot
CN210455228U (en) Rest facility for crew members on a civil aviation passenger plane
CN218777688U (en) An aircraft seat and an aircraft
US2861624A (en) Seats for aircraft cabins and other vehicles
CN111391760A (en) Automatic retractable landing ladder
CN110450959A (en) Crew's rest facility and its application method on a kind of civil aviation passenger transport aircraft
US11912186B2 (en) Modular tray table with rotational displacement mechanism
CN105715201A (en) A built-in foldable pull ladder
US5791014A (en) Handle for carry-on luggage
CN201712501U (en) Vehicular combined seat

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right

Effective date of registration: 20220630

Address after: 211100 two, B unit 300, Zhihui Road, Qilin science and Technology Innovation Park, Nanjing, Jiangsu.

Applicant after: NANJING YUSHENG ROBOT TECHNOLOGY Co.,Ltd.

Address before: 310000 Tianbao building, No. 588, Shixin Road, Xiaoshan District, Hangzhou City, Zhejiang Province

Applicant before: Hangzhou car acceleration Service Co.,Ltd.

TA01 Transfer of patent application right
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20250422

Address after: 337000 Tanhua Village, Shangli County, Pingxiang City, Jiangxi Province

Patentee after: Jiangxi Zhongjin Electric Power Manufacturing Co.,Ltd.

Country or region after: China

Patentee after: Wannian County Rongrong Industrial Co.,Ltd.

Address before: 211100 two, B unit 300, Zhihui Road, Qilin science and Technology Innovation Park, Nanjing, Jiangsu.

Patentee before: NANJING YUSHENG ROBOT TECHNOLOGY Co.,Ltd.

Country or region before: China

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20250603

Address after: 330001, No. 66 Fota Road, Qingyunpu District, Nanchang City, Jiangxi Province, Room HD-1013, Aggregation Space

Patentee after: Mango Airlines Group Co.,Ltd.

Country or region after: China

Address before: 337000 Tanhua Village, Shangli County, Pingxiang City, Jiangxi Province

Patentee before: Jiangxi Zhongjin Electric Power Manufacturing Co.,Ltd.

Country or region before: China

Patentee before: Wannian County Rongrong Industrial Co.,Ltd.

TR01 Transfer of patent right