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CN118597426A - A shock absorbing and buffering mechanism for ejection seat - Google Patents

A shock absorbing and buffering mechanism for ejection seat Download PDF

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Publication number
CN118597426A
CN118597426A CN202410991714.7A CN202410991714A CN118597426A CN 118597426 A CN118597426 A CN 118597426A CN 202410991714 A CN202410991714 A CN 202410991714A CN 118597426 A CN118597426 A CN 118597426A
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China
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shaped
flip
ejection seat
sleeve
frame
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CN202410991714.7A
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CN118597426B (en
Inventor
施锦寿
李林杰
曲鸣飞
马超
李亚萍
闫紫光
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Beijing Polytechnic
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Beijing Polytechnic
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    • 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
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • B64D25/08Ejecting or escaping means
    • B64D25/10Ejector seats

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  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Seats For Vehicles (AREA)

Abstract

The application discloses a damping buffer mechanism for an ejection seat, and belongs to the technical field of ejection seats. The damping buffer mechanism comprises an ejection seat, an adjustable plug structure, a neck protection module and a linkage tensioning mechanism, wherein the neck protection module and the linkage tensioning mechanism are sequentially arranged from bottom to top. According to the application, the upper and lower linkage tensioning mechanism and the neck protection module which are configured through the adjustable plug structure can utilize the characteristics similar to the lever principle, after the ejection seat is ejected, the body of the ejection seat is clung to the first protection cushion block under the action of reaction force, the second protection cushion blocks on the two sides of the top are pulled down to support the head, so that the head is effectively damped and buffered, when the head or the helmet is leaned against the surface of the head, the second protection cushion blocks on the two sides are tightened from the two sides to the middle, and the inner damping spring sleeve is matched to counteract huge load in the ejection process, and the neck vertebra of a pilot is stabilized, so that the damping and buffering effects of the head or the helmet are further improved.

Description

一种用于弹射座椅的减震缓冲机构A shock absorbing and buffering mechanism for ejection seat

技术领域Technical Field

本发明涉及弹射座椅技术领域,更具体地说,涉及一种用于弹射座椅的减震缓冲机构。The present invention relates to the technical field of ejection seats, and more particularly to a shock absorbing and buffering mechanism for an ejection seat.

背景技术Background Art

弹射座椅顾名思义就是能够向外弹射的座椅,可依靠座椅下的动力装置将其弹射出舱,然后配合张开的降落伞使飞行员安全降落的座椅型救生装置,随着科学技术的不断进步,弹射座椅发展及至现代,其已为全自动程序装置,飞行员只要拉动弹射手柄,从座椅弹出至乘降落伞着陆全都会按程序自动完成。As the name suggests, an ejection seat is a seat that can be ejected outwards. It can be ejected out of the cabin by relying on the power device under the seat, and then cooperate with the open parachute to allow the pilot to land safely. It is a seat-type life-saving device. With the continuous advancement of science and technology, the ejection seat has developed into a fully automatic program device in modern times. The pilot only needs to pull the ejection handle, and everything from ejecting from the seat to landing by parachute will be automatically completed according to the program.

现有技术中的全自动弹射座椅组成一般包括抛盖装置、弹射装置等,结构比较复杂,不仅有弹射动力系统,为了进一步保证飞行员的安全,还配置有应急供氧系统以及减震缓冲系统等,其中减震缓冲模块用于托住飞行员的腰部与胯部,以抵消弹射过程中产生的载荷。The components of the fully automatic ejection seat in the prior art generally include a cover ejection device, an ejection device, etc., and the structure is relatively complex. It not only has an ejection power system, but also is equipped with an emergency oxygen supply system and a shock absorbing and buffering system to further ensure the safety of the pilot. The shock absorbing and buffering module is used to support the pilot's waist and hips to offset the load generated during the ejection process.

但是,在座椅被弹射出去以后,实际上受力的不仅仅是腰部与胯部,还有颈部,并且颈椎是离头最近的脊柱部分,活动度比较大,其牵扯到中枢神经系统的最高位的神经中枢,因此更为脆弱,但是现有技术中对于颈椎的缓冲防护大多数仅仅能够依靠颈部护枕,在向外弹射时高强度的冲击力会使颈椎直接撞向护枕,并由于惯性其颈椎会向外抬高,使头部直接上仰,而上仰的头部并没有对应的防护端,故并不能够对其起到很好的减震缓冲作用。However, after the seat is ejected, it is not only the waist and hips that are actually under force, but also the neck. The cervical vertebra is the part of the spine closest to the head and has a relatively large range of motion. It involves the highest nerve center of the central nervous system and is therefore more fragile. However, in the prior art, most of the cushioning protection for the cervical vertebra can only rely on a neck pillow. When ejected outward, the high-intensity impact force will cause the cervical vertebra to directly hit the pillow, and due to inertia, the cervical vertebra will be lifted outward, causing the head to tilt directly upward, and the tilted head does not have a corresponding protective end, so it cannot provide a good shock-absorbing and buffering effect.

因此,有必要提供一种用于弹射座椅的减震缓冲机构。Therefore, it is necessary to provide a shock absorbing and buffering mechanism for an ejection seat.

发明内容Summary of the invention

针对现有技术中弹射座椅并不能够对飞行员的颈部起到很好的减震缓冲作用的问题,本发明的目的在于提供一种用于弹射座椅的减震缓冲机构。In view of the problem that the ejection seat in the prior art cannot provide a good shock absorbing and buffering effect on the pilot's neck, an object of the present invention is to provide a shock absorbing and buffering mechanism for the ejection seat.

为解决上述问题,本发明采用如下的技术方案。To solve the above problems, the present invention adopts the following technical solutions.

一种用于弹射座椅的减震缓冲机构,包括弹射座椅;所述弹射座椅的背部上侧位置处安装有可调插拔结构,所述可调插拔结构的外侧延伸至弹射座椅的前侧;在所述可调插拔结构上且自下往而上依次配置颈部防护模块和联动拉紧机构;A shock absorbing and buffering mechanism for an ejection seat, comprising an ejection seat; an adjustable plug-in structure is installed at the upper side of the back of the ejection seat, and the outer side of the adjustable plug-in structure extends to the front side of the ejection seat; a neck protection module and a linkage tensioning mechanism are sequentially arranged on the adjustable plug-in structure from bottom to top;

所述弹射座椅的顶端的中间位置处开设有U形开口,所述可调插拔结构包括插口套框和插拔板,所述插口套框设置在所述U形开口的背侧且与所述U形开口固定连接,所述插拔板插入所述插口套框内,所述颈部防护模块包括设置于插拔板前端下侧位置处的U形敞口架,所述联动拉紧机构包括设置于插拔板前端上侧位置处的导轨槽口架;A U-shaped opening is provided at the middle position of the top of the ejection seat, the adjustable plug-in structure comprises a socket sleeve frame and a plug-in plate, the socket sleeve frame is arranged at the back side of the U-shaped opening and is fixedly connected to the U-shaped opening, the plug-in plate is inserted into the socket sleeve frame, the neck protection module comprises a U-shaped open frame arranged at the lower side of the front end of the plug-in plate, and the linkage tensioning mechanism comprises a guide rail slot frame arranged at the upper side of the front end of the plug-in plate;

其中,所述导轨槽口架的两侧均配置有相对称的第二防护垫块,所述U形敞口架的外侧配置有第一防护垫块,所述第一防护垫块贴合颈部被向后推动过程中带动上部两侧的第二防护垫块向中间收紧托住头部进行减震缓冲。Among them, symmetrical second protective pads are arranged on both sides of the guide rail slot frame, and a first protective pad is arranged on the outer side of the U-shaped open frame. When the first protective pad fits the neck and is pushed backward, it drives the second protective pads on both sides of the upper part to tighten toward the middle to support the head for shock absorption and buffering.

可选地,所述插拔板的表面从上往下依次开设多个开口,所述插口套框的侧壁上设置有插口,所述插拔板的开口与所述插口套框的插口通过插入安定位插销固定,所述插拔板的顶部活动铰接有U形外翻板。Optionally, a plurality of openings are sequentially provided on the surface of the plug plate from top to bottom, a socket is provided on the side wall of the socket frame, the opening of the plug plate and the socket of the socket frame are fixed by inserting positioning pins, and a U-shaped outer flap is movably hinged on the top of the plug plate.

可选地,所述U形外翻板的外侧U形开口端内活动铰接有翻转块;所述翻转块的铰接端侧面转动安装有用收紧螺栓,所述收紧螺栓用于控制所述翻转块的松紧状态,所述翻转块的上下两侧分别固定安装有电动伸缩杆。Optionally, a flip block is movably hinged inside the outer U-shaped opening end of the U-shaped outer flap; a tightening bolt is rotatably installed on the side of the hinged end of the flip block, and the tightening bolt is used to control the tightness of the flip block. Electric telescopic rods are respectively fixedly installed on the upper and lower sides of the flip block.

可选地,所述U形敞口架固定连接于所述翻转块下侧的电动伸缩杆上,所述U形敞口架的外敞口端上固定连接有第一防护垫块,所述第一防护垫块表面中间位置处开设有开口;所述第一防护垫块的开口固定连接有纱网层。Optionally, the U-shaped open frame is fixedly connected to the electric telescopic rod on the lower side of the flip block, and a first protective pad is fixedly connected to the outer open end of the U-shaped open frame, and an opening is provided in the middle position of the surface of the first protective pad; the opening of the first protective pad is fixedly connected to a mesh layer.

可选地,所述第一防护垫块的内侧面上固定安装有吸附风机,所述吸附风机的吸附端与所述纱网层贴合,所述U形敞口架的后表面中间位置处固定安装有透气槽口架,所述透气槽口架的两侧端均固定安装有气囊块。Optionally, an adsorption fan is fixedly installed on the inner side surface of the first protective pad block, the adsorption end of the adsorption fan is in contact with the mesh layer, a breathable slot frame is fixedly installed at the middle position of the rear surface of the U-shaped open frame, and airbag blocks are fixedly installed on both side ends of the breathable slot frame.

可选地,所述导轨槽口架固定连接于所述翻转块上侧的电动伸缩杆上,所述导轨槽口架的内部中间位置处活动水平安装有双向螺纹杆,所述双向螺纹杆一侧贯穿伸出导轨槽口架的侧壁且所述双向螺杆的同侧端部固定连接有调节转扣,所述导轨槽口架的内槽口两端相对称的位置处均通过双向螺纹杆啮合安装有螺母U形套块。Optionally, the guide rail slot frame is fixedly connected to the electric telescopic rod on the upper side of the flip block, and a two-way threaded rod is movably installed horizontally at the inner middle position of the guide rail slot frame, one side of the two-way threaded rod penetrates through the side wall of the guide rail slot frame and the same side end of the two-way screw rod is fixedly connected with an adjustment buckle, and nut U-shaped sleeve blocks are installed at symmetrical positions at both ends of the inner slot of the guide rail slot frame through the engagement of the two-way threaded rod.

可选地,所述螺母U形套块的外侧U形槽口内均活动铰接有一个向外倾斜敞开的弧形翻转板,所述弧形翻转板的外表面上侧两端位置处均固定安装有翻转接头,所述弧形翻转板的外表面通过两侧的翻转接头活动安装有第二防护垫块。Optionally, an arc-shaped flip plate that is tilted outward and opened is movably hinged in the outer U-shaped groove of the nut U-shaped sleeve block, and flip joints are fixedly installed at both ends of the upper side of the outer surface of the arc-shaped flip plate. The outer surface of the arc-shaped flip plate is movably installed with a second protective pad via the flip joints on both sides.

可选地,所述第二防护垫块的内侧两端位置处均固定安装有与弧形翻转板外表面贴合对应的减震弹簧套,所述第二防护垫块整体为自上而下向背面凹陷的圆弧块结构。Optionally, shock-absorbing spring sleeves corresponding to the outer surface of the arc-shaped flip plate are fixedly installed at both ends of the inner side of the second protective pad block, and the second protective pad block as a whole is an arc block structure that is concave from top to bottom toward the back.

可选地,所述弧形翻转板远离螺母U形套块铰接的一端均固定连接有翻转套筒,所述导轨槽口架的背面中间位置处固定连接有两根限位杆,所述限位杆外表面滑动套有套口支架。Optionally, one end of the arc-shaped flip plate away from the hinged end of the nut U-shaped sleeve block is fixedly connected to a flip sleeve, two limit rods are fixedly connected to the middle position of the back side of the guide rail slot frame, and a sleeve bracket is slidably sleeved on the outer surface of the limit rod.

可选地,所述套口支架整体为H形结构,所述套口支架的内侧与导轨槽口架背面之间均固定连接有复位弹簧,所述复位弹簧的一端与所述导轨槽口架背面连接,所述复位弹簧的另一端与所述套口支架连接,所述套口支架的两侧均活动安装有与翻转套筒连接的铰接板。Optionally, the sleeve bracket is an H-shaped structure as a whole, and a return spring is fixedly connected between the inner side of the sleeve bracket and the back side of the guide rail slot bracket, one end of the return spring is connected to the back side of the guide rail slot bracket, and the other end of the return spring is connected to the sleeve bracket, and hinged plates connected to the flip sleeve are movably installed on both sides of the sleeve bracket.

本发明提供的技术方案与现有技术相比,至少具有如下有益效果:Compared with the prior art, the technical solution provided by the present invention has at least the following beneficial effects:

上述方案中,通过可调插拔结构配置的一上一下联动拉紧机构与颈部防护模块,其两端的第一防护垫块与第二防护垫块可利用类似于杠杆原理的特性,在弹射座椅被弹射出去之后,其身体在反作用力的作用下,颈部会紧贴在第一防护垫块上,并拉下顶部两侧的第二防护垫块托住头部,进行有效的减震缓冲;In the above scheme, the upper and lower linkage tensioning mechanism and the neck protection module are configured through the adjustable plug-in structure. The first protection pads and the second protection pads at both ends can utilize the characteristics similar to the lever principle. After the ejection seat is ejected, the body will be tightly attached to the first protection pad under the action of the reaction force, and the second protection pads on both sides of the top will be pulled down to support the head, so as to effectively reduce shock and buffer.

通过联动拉紧机构中由螺母U形套块铰接的弧形翻转板的翻转作用,在头部或者头盔靠于其表面时,两侧的第二防护垫块会从两侧向中间收紧,并配合内侧的减震弹簧套去抵消弹射过程中的巨大荷载,并稳住飞行员的颈部脊椎,进一步提高其减震缓冲效果;Through the flipping action of the arc-shaped flip plate hinged by the nut U-shaped sleeve in the linkage tensioning mechanism, when the head or helmet is against its surface, the second protective pads on both sides will be tightened from both sides to the middle, and cooperate with the shock-absorbing spring sleeve on the inside to offset the huge load during the ejection process and stabilize the pilot's cervical spine, further improving its shock-absorbing and buffering effect;

通过颈部防护模块、联动拉紧机构之间的翻转块,利用其上下表面上单独配置的电动伸缩杆,在实际使用过程中可根据不同环境以及不同体型的飞行员,去改变两侧防护端的间隔,进一步的,还可配合双向螺纹杆的调节作用去改变两侧第二防护垫块的间隔,增加减震端整体的适配性能与可控效果,在减震缓冲过程中能够更精准地控制其荷载力抵消端的位置;Through the flip block between the neck protection module and the linkage tensioning mechanism, and using the electric telescopic rods separately configured on the upper and lower surfaces, the interval between the protection ends on both sides can be changed according to different environments and pilots of different body shapes during actual use. Furthermore, the interval between the second protection pads on both sides can be changed by adjusting the bidirectional threaded rod, thereby increasing the overall adaptability and controllable effect of the shock absorbing end, and more accurately controlling the position of the load force offsetting end during the shock absorbing and buffering process.

通过第一防护垫块表面纱网层的设计,不仅可根据其圆弧状的块使其防护面以一个相对绷紧状态的弹性层去托住颈部,区别于传统的海绵块能够更有效卸去冲击力,并配合吸附风机稳稳地吸附住后颈,进一步提高其减震缓冲效果。Through the design of the mesh layer on the surface of the first protective pad block, not only can the arc-shaped block make its protective surface support the neck with a relatively taut elastic layer, which is different from the traditional sponge block and can more effectively remove the impact force, but it can also cooperate with the adsorption fan to stably adsorb the back of the neck, further improving its shock-absorbing and buffering effect.

附图说明BRIEF DESCRIPTION OF THE DRAWINGS

并入本文中并且构成说明书的部分的附图示出了本发明的实施例,并且与说明书一起进一步用来对本发明的原理进行解释,并且使相关领域技术人员能够实施和使用本发明。The accompanying drawings, which are incorporated herein and constitute a part of the specification, illustrate embodiments of the invention and, together with the description, further serve to explain the principles of the invention and to enable those skilled in the relevant art to make and use the invention.

图1为本发明的立体结构示意图;FIG1 is a schematic diagram of a three-dimensional structure of the present invention;

图2为本发明后侧面结构示意图;FIG2 is a schematic diagram of the rear side structure of the present invention;

图3为本发明颈部防护模块、联动拉紧机构整体的结构示意图;FIG3 is a schematic diagram of the overall structure of the neck protection module and the linkage tensioning mechanism of the present invention;

图4为本发明可调插拔结构拆分状态的结构示意图;FIG4 is a schematic diagram of the structure of the adjustable plug-in structure of the present invention in a disassembled state;

图5为本发明颈部防护模块拆分状态的结构示意图;FIG5 is a schematic structural diagram of a neck protection module of the present invention in a disassembled state;

图6为本发明联动拉紧机构的结构示意图;FIG6 is a schematic structural diagram of a linkage tensioning mechanism of the present invention;

图7为本发明单个弧形翻转板的结构示意图;FIG7 is a schematic diagram of the structure of a single arc-shaped flip plate of the present invention;

图8为本发明套口支架的结构示意图。FIG. 8 is a schematic structural diagram of the sleeve bracket of the present invention.

[附图标记][Reference Symbols]

1、弹射座椅;1. Ejection seat;

2、可调插拔结构;21、插口套框;22、插拔板;23、定位插销;24、U形外翻板;25、翻转块;26、收紧螺栓;27、电动伸缩杆;2. Adjustable plug-in structure; 21. Socket frame; 22. Plug-in plate; 23. Positioning pin; 24. U-shaped outer flap; 25. Flip block; 26. Tightening bolt; 27. Electric telescopic rod;

3、颈部防护模块;31、U形敞口架;32、第一防护垫块;33、纱网层;34、吸附风机;35、透气槽口架;36、气囊块;3. Neck protection module; 31. U-shaped open frame; 32. First protection pad; 33. Gauze layer; 34. Adsorption fan; 35. Breathable slot frame; 36. Airbag block;

4、联动拉紧机构;41、导轨槽口架;42、双向螺纹杆;43、调节转扣;44、螺母U形套块;45、弧形翻转板;46、翻转接头;47、第二防护垫块;48、减震弹簧套;49、翻转套筒;410、限位杆;411、套口支架;412、复位弹簧;413、铰接板。4. Linkage tensioning mechanism; 41. Guide rail slot frame; 42. Bidirectional threaded rod; 43. Adjustment buckle; 44. Nut U-shaped sleeve; 45. Arc-shaped flip plate; 46. Flip joint; 47. Second protective pad; 48. Shock-absorbing spring sleeve; 49. Flip sleeve; 410. Limit rod; 411. Sleeve bracket; 412. Reset spring; 413. Hinge plate.

如图所示,为了能明确实现本发明的实施例的结构,在图中标注了特定的结构和器件,但这仅为示意需要,并非意图将本发明限定在该特定结构、器件和环境中,根据具体需要,本领域的普通技术人员可以将这些器件和环境进行调整或者修改。As shown in the figure, in order to clearly implement the structure of the embodiment of the present invention, specific structures and devices are marked in the figure, but this is only for illustrative purposes and is not intended to limit the present invention to the specific structure, device and environment. According to specific needs, ordinary technicians in this field can adjust or modify these devices and environments.

具体实施方式DETAILED DESCRIPTION

下面结合附图和具体实施例对本发明进行详细描述。同时在这里做以说明的是,为了使实施例更加详尽,下面的实施列为最佳、优选实施例,对于一些公知技术领域技术人员也可采用其他替代方式而实施;而且附图部分仅是为了更具体地描述实施例,而并不旨在对本发明进行具体的限定。The present invention is described in detail below in conjunction with the accompanying drawings and specific embodiments. At the same time, it is explained here that in order to make the embodiments more detailed, the following embodiments are listed as the best and preferred embodiments, and other alternatives can also be used by technicians in some known technical fields; and the accompanying drawings are only for more specific description of the embodiments, and are not intended to specifically limit the present invention.

需要指出的是,在说明书中提到“一个实施例”、“实施例”、“示例性实施例”、“一些实施例”等指示所述的实施例可以包括特定特征、结构或特性,但未必每个实施例都包括该特定特征、结构或特性。另外,在结合实施例描述特定特征、结构或特性时,结合其他实施例(无论是否明确描述)实现这种特征、结构或特性应在相关领域技术人员的知识范围内。It should be noted that the references to "one embodiment", "embodiment", "exemplary embodiments", "some embodiments" and the like in the specification indicate that the embodiments described may include specific features, structures or characteristics, but not every embodiment may include the specific features, structures or characteristics. In addition, when a specific feature, structure or characteristic is described in conjunction with an embodiment, it should be within the knowledge of a person skilled in the art to implement such feature, structure or characteristic in conjunction with other embodiments (whether or not explicitly described).

通常,可以至少部分从上下文中的使用来理解术语。例如,至少部分取决于上下文,本文中使用的术语“一个或多个”可以用于描述单数意义的任何特征、结构或特性,或者可以用于描述复数意义的特征、结构或特性的组合。另外,术语“基于”可以被理解为不一定旨在传达一组排他性的因素,而是可以替代地,至少部分地取决于上下文,允许存在不一定明确描述的其他因素。In general, a term can be understood, at least in part, from its use in context. For example, depending, at least in part, on the context, the term "one or more" as used herein can be used to describe any feature, structure, or characteristic in the singular sense, or can be used to describe a combination of features, structures, or characteristics in the plural sense. Additionally, the term "based on" can be understood as not necessarily intended to convey an exclusive set of factors, but can instead, depending, at least in part, on the context, allow for the presence of other factors that are not necessarily explicitly described.

可以理解的是,本发明中的“在……上”、“在……之上”和“在……上方”的含义应当以最宽方式被解读,以使得“在……上”不仅表示“直接在”某物“上”而且还包括在某物“上”且其间有居间特征或层的含义,并且“在……之上”或“在……上方”不仅表示“在”某物“之上”或“上方”的含义,而且还可以包括其“在”某物“之上”或“上方”且其间没有居间特征或层的含义。It will be understood that the meanings of “on,” “over,” and “above” in the present invention should be interpreted in the broadest manner, so that “on” not only means “directly on” something, but also includes the meaning of being “on” something with intervening features or layers therebetween, and “on” or “over” not only means “on” or “above” something, but also includes the meaning of being “on” or “above” something with no intervening features or layers therebetween.

此外,诸如“在…之下”、“在…下方”、“下部”、“在…之上”、“上部”等空间相关术语在本文中为了描述方便可以用于描述一个元件或特征与另一个或多个元件或特征的关系,如在附图中示出的。空间相关术语旨在涵盖除了在附图所描绘的取向之外的在设备使用或操作中的不同取向。设备可以以另外的方式被定向,并且本文中使用的空间相关描述词可以类似地被相应解释。Additionally, spatially relative terms such as "under," "beneath," "lower," "above," "upper," and the like may be used herein for descriptive convenience to describe the relationship of one element or feature to another element or features, as shown in the accompanying drawings. Spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the accompanying drawings. The device may be oriented in other ways, and the spatially relative descriptors used herein may be similarly interpreted accordingly.

如图1至图8所示,本发明实施例提供一种用于弹射座椅的减震缓冲机构,包括弹射座椅1;所述弹射座椅1的背部上侧位置处安装有可调插拔结构2,可调插拔结构2的外侧伸于弹射座椅1的前侧;且从下往上依次配置有用于护颈的颈部防护模块3以及用于给头部缓冲的联动拉紧机构4;As shown in FIGS. 1 to 8 , an embodiment of the present invention provides a shock absorbing and buffering mechanism for an ejection seat, comprising an ejection seat 1; an adjustable plug-in structure 2 is installed at the upper back side of the ejection seat 1, and the outer side of the adjustable plug-in structure 2 extends to the front side of the ejection seat 1; and a neck protection module 3 for protecting the neck and a linkage tensioning mechanism 4 for buffering the head are sequentially arranged from bottom to top;

所述弹射座椅1的上侧中间位置处开设有U形开口,可调插拔结构2包括固定连接于该U形开口后侧的插口套框21以及插入其内的插拔板22,颈部防护模块3包括设置于插拔板22前端下侧位置处的U形敞口架31,联动拉紧机构4包括设置于插拔板22前端上侧位置处的导轨槽口架41;A U-shaped opening is provided at the middle position of the upper side of the ejection seat 1, the adjustable plug-in structure 2 includes a socket sleeve frame 21 fixedly connected to the rear side of the U-shaped opening and a plug-in plate 22 inserted therein, the neck protection module 3 includes a U-shaped open frame 31 arranged at the lower side of the front end of the plug-in plate 22, and the linkage tensioning mechanism 4 includes a guide rail slot frame 41 arranged at the upper side of the front end of the plug-in plate 22;

其中,所述导轨槽口架41的两侧均配置有相对称的第二防护垫块47,U形敞口架31的外侧配置有第一防护垫块32,第一防护垫块32贴合颈部被向后推动过程中带动上部两侧的第二防护垫块47向中间收紧托住头部进行减震缓冲。Among them, symmetrical second protection pads 47 are arranged on both sides of the guide groove frame 41, and the first protection pad 32 is arranged on the outer side of the U-shaped open frame 31. When the first protection pad 32 fits the neck and is pushed backward, it drives the second protection pads 47 on both sides of the upper part to tighten toward the middle to support the head for shock absorption and buffering.

通过采用上述技术方案,可解决现有技术中弹射座椅1上并不能够对飞行员的颈部起到很好的减震缓冲作用的问题,其上述技术方案主要由弹射座椅1、可调插拔结构2、颈部防护模块3以及联动拉紧机构4组成,其中弹射座椅1为现有技术中常规式的弹射椅,配置有对应的弹射装置以及自动弹射程序、降落伞等固有配置,区别在于其座椅后靠背上开设有U形开口,而颈部防护模块3的第一防护垫块32处于该U形开口的前侧,且由于U形敞口架31整体为U形的敞口状,故在受到挤压时其U形敞口架31会插于开口中,使其能够借助弹射座椅1作为缓冲端,并且弹射座椅1上的U形开口还能够为后续U形敞口架31向内侧后推提供空间,而在U形敞口架31向内侧后推时,上侧的第二防护垫块47会由于杠杆原理的作用向前侧送出,去夹住后靠的头部,进行减震缓冲。By adopting the above technical solution, the problem that the ejection seat 1 in the prior art cannot play a good shock-absorbing and buffering role for the pilot's neck can be solved. The above technical solution mainly consists of an ejection seat 1, an adjustable plug-in structure 2, a neck protection module 3 and a linkage tensioning mechanism 4. The ejection seat 1 is a conventional ejection seat in the prior art, equipped with a corresponding ejection device and an automatic ejection program, a parachute and other inherent configurations. The difference is that a U-shaped opening is opened on the backrest of the seat, and the neck protection module 3 has a U-shaped opening on the backrest of the seat. A protective pad 32 is located at the front side of the U-shaped opening, and because the U-shaped open frame 31 is an overall U-shaped open shape, the U-shaped open frame 31 will be inserted into the opening when squeezed, so that it can use the ejection seat 1 as a buffer end, and the U-shaped opening on the ejection seat 1 can also provide space for the subsequent U-shaped open frame 31 to be pushed inward and backward. When the U-shaped open frame 31 is pushed inward and backward, the second protective pad 47 on the upper side will be sent forward due to the effect of the lever principle to clamp the head leaning back for shock absorption and buffering.

如图1至图4所示,所述插拔板22的表面从上往下依次开设多个开口,插口套框21的侧面对应插拔板22上开设的开口亦开设有的插口;且其插口上插入安装有与插拔板22上开设的开口对应的定位插销23,插拔板22的前侧活动铰接有U形外翻板24;且其铰接端侧面转动安装有用于控制其松紧状态的螺栓。As shown in FIGS. 1 to 4 , the surface of the plug plate 22 is provided with a plurality of openings in sequence from top to bottom, and the side of the socket frame 21 is provided with sockets corresponding to the openings provided on the plug plate 22; and positioning pins 23 corresponding to the openings provided on the plug plate 22 are inserted and installed on the sockets; a U-shaped outer flap 24 is movably hinged on the front side of the plug plate 22; and a bolt for controlling its tightness is rotatably installed on the side of the hinged end.

如图1至图4所示,所述U形外翻板24的外侧U形开口端内活动铰接有翻转块25;且其铰接端侧面转动安装有用于控制其松紧状态的收紧螺栓26,翻转块25的上下两侧均固定安装有电动伸缩杆27。As shown in Figures 1 to 4, a flip block 25 is movably hinged inside the outer U-shaped opening end of the U-shaped outer flap 24; and a tightening bolt 26 for controlling its tightness is rotatably installed on the side of its hinged end, and electric telescopic rods 27 are fixedly installed on the upper and lower sides of the flip block 25.

如前述实施例,其可调插拔结构2用于起杠杆作用,其具体为:根据实际情况可将插拔板22插入于插口套框21中,并根据其插拔板22上对应位置处的开口对准插口套框21侧面的插口,使用定位插销23进行定位固定,使外侧伸出的U形外翻板24停靠于弹射座椅1前侧合适的位置处,在使用过程中,还可以通过转动U形外翻板24与插拔板22铰接位置处的螺栓与U形外翻板24外侧的收紧螺栓26,去调节铰接端的松紧程度,当铰接端松开时即可进行对应转动,去改变外侧构件的倾斜角度,进一步提高其外侧翻转块25的可控效果,使其能够以不同倾斜角度伸出,而当铰接端收紧时即可对铰接端进行固定;As in the aforementioned embodiment, the adjustable plug-in structure 2 is used to act as a lever, which is specifically as follows: according to actual conditions, the plug-in plate 22 can be inserted into the socket sleeve frame 21, and the opening at the corresponding position on the plug-in plate 22 is aligned with the socket on the side of the socket sleeve frame 21, and the positioning pin 23 is used for positioning and fixing, so that the U-shaped outer flap 24 extending outward is parked at a suitable position on the front side of the ejection seat 1. During use, the tightness of the hinged end can be adjusted by rotating the bolts at the hinged position of the U-shaped outer flap 24 and the plug-in plate 22 and the tightening bolts 26 on the outside of the U-shaped outer flap 24. When the hinged end is loosened, it can be rotated accordingly to change the inclination angle of the outer member, further improving the controllable effect of the outer flip block 25, so that it can be extended at different inclination angles, and when the hinged end is tightened, the hinged end can be fixed;

其中,配置的电动伸缩杆27为现有技术中的电动伸缩设备,用于控制其输出端构件的实际伸出长度,配置在铰接位置处的螺栓与收紧螺栓26结构相同,均为现有技术中的螺栓套结构,可通过转紧转松去改变铰接端的收紧程度。Among them, the configured electric telescopic rod 27 is an electric telescopic device in the prior art, which is used to control the actual extension length of its output end component. The bolt configured at the hinged position has the same structure as the tightening bolt 26, both of which are bolt sleeve structures in the prior art, and the tightening degree of the hinged end can be changed by tightening or loosening.

如图3至图5所示,所述U形敞口架31固定连接于翻转块25下侧的电动伸缩杆27上,U形敞口架31的外敞口端上固定连接有第一防护垫块32,第一防护垫块32表面中间位置处开设有开口;且通过其开口固定连接有纱网层33。As shown in Figures 3 to 5, the U-shaped open frame 31 is fixedly connected to the electric telescopic rod 27 on the lower side of the flip block 25, and a first protective pad 32 is fixedly connected to the outer open end of the U-shaped open frame 31. An opening is provided in the middle position of the surface of the first protective pad 32; and a mesh layer 33 is fixedly connected through its opening.

如图3至图5所示,所述第一防护垫块32的内侧面上固定安装有吸附风机34,吸附风机34的吸附端贴合于纱网层33上,U形敞口架31的后表面中间位置处固定安装有透气槽口架35,透气槽口架35的两侧端均固定安装有气囊块36。As shown in Figures 3 to 5, an adsorption fan 34 is fixedly installed on the inner side surface of the first protective pad block 32, and the adsorption end of the adsorption fan 34 is attached to the mesh layer 33. A breathable slot frame 35 is fixedly installed in the middle position of the rear surface of the U-shaped open frame 31, and airbag blocks 36 are fixedly installed on both side ends of the breathable slot frame 35.

如前述实施例,其颈部防护模块3起颈部防护的作用以及拉动上侧联动拉紧机构4紧托头部的作用,其具体为:U形敞口架31安装于翻转块25底部的电动伸缩杆27上,配置的U形敞口架31以及外侧的第一防护垫块32均为凹口状的圆弧形状,以方便贴合颈部,通过翻转块25底部的电动伸缩杆27的电动伸缩作用可以控制其第一防护垫块32伸出的长度,松开收紧螺栓26,使翻转块25可自由翻转,将翻转块25底部的第一防护垫块32整体向前倾斜伸出,当弹射座椅1向外弹射,飞行员的后颈靠于第一防护垫块32的纱网层33上时,U形敞口架31整体会向后侧移动,此时翻转块25上侧的联动拉紧机构4就会向前移动,去稳住飞行员的头部,在整体会向后侧移动过程中,由于在弹射座椅1上配置的安全带会在弹射过程中进行适应收紧,故可保证后背的相对稳定,从而避免后颈的前后晃动;As in the above-mentioned embodiment, the neck protection module 3 plays the role of neck protection and pulling the upper linkage tensioning mechanism 4 to tightly support the head, which is specifically as follows: the U-shaped open frame 31 is installed on the electric telescopic rod 27 at the bottom of the flip block 25, and the configured U-shaped open frame 31 and the first protective pad 32 on the outside are both in a concave arc shape to facilitate fitting the neck. The electric telescopic effect of the electric telescopic rod 27 at the bottom of the flip block 25 can control the extension length of the first protective pad 32, and loosen the tightening bolt 26 to allow the flip block 25 to flip freely. The first protective pad 32 at the bottom of the flip block 25 is tilted forward and extended as a whole. When the ejection seat 1 is ejected outward and the pilot's neck rests on the mesh layer 33 of the first protective pad 32, the U-shaped open frame 31 moves backward as a whole. At this time, the linkage tensioning mechanism 4 on the upper side of the flip block 25 moves forward to stabilize the pilot's head. During the overall backward movement, the safety belt configured on the ejection seat 1 is adapted and tightened during the ejection process, so that the back can be relatively stable, thereby preventing the back neck from shaking back and forth.

其中,所述第一防护垫块32为海绵套块,而其表面上连接的纱网层33为绷紧状态的纱网,且沿着凹槽圆弧的内开口向外绷紧,形成一个有弧度的托网,而内侧的吸附风机34为现有技术中的吸附设备,在工作时可向内侧此时吸附分,去吸住后颈,气囊块36为现有技术中的气囊结构,在U形敞口架31向后侧移动时,气囊块36可作为缓冲层去紧贴内侧,起缓冲作用。Among them, the first protective pad block 32 is a sponge cover block, and the gauze layer 33 connected on its surface is a taut gauze, and is stretched outward along the inner opening of the arc of the groove to form a curved support net, and the inner adsorption fan 34 is an adsorption device in the prior art, which can adsorb inward when working to suck the back neck, and the airbag block 36 is an airbag structure in the prior art. When the U-shaped open frame 31 moves toward the rear side, the airbag block 36 can be used as a buffer layer to stick to the inside to play a buffering role.

如图3至图8所示,所述导轨槽口架41固定连接于翻转块25上侧的电动伸缩杆27上,导轨槽口架41的内部中间位置处活动安装有双向螺纹杆42,双向螺纹杆42一侧贯穿伸出导轨槽口架41且固定连接有调节转扣43,导轨槽口架41的内槽口两端相对称的位置处均通过双向螺纹杆42啮合安装有螺母U形套块44。As shown in Figures 3 to 8, the guide rail slot frame 41 is fixedly connected to the electric telescopic rod 27 on the upper side of the flip block 25, and a bidirectional threaded rod 42 is movably installed at the middle position inside the guide rail slot frame 41. One side of the bidirectional threaded rod 42 passes through the guide rail slot frame 41 and is fixedly connected with an adjustment buckle 43. Nut U-shaped sleeve blocks 44 are installed at symmetrical positions at both ends of the inner slot of the guide rail slot frame 41 through the bidirectional threaded rod 42.

如图3至图8所示,所述螺母U形套块44的外侧U形槽口内均活动铰接有一个向外倾斜敞开的弧形翻转板45,弧形翻转板45的外表面上侧两端位置处均固定安装有翻转接头46,弧形翻转板45的外表面通过两侧的翻转接头46活动安装有第二防护垫块47。As shown in Figures 3 to 8, an arc-shaped flip plate 45 that is tilted and opened outward is movably hinged in the outer U-shaped groove of the nut U-shaped sleeve 44, and flip joints 46 are fixedly installed at both ends of the upper side of the outer surface of the arc-shaped flip plate 45. The outer surface of the arc-shaped flip plate 45 is movably installed with a second protective pad 47 through the flip joints 46 on both sides.

如图1至图8所示,所述第二防护垫块47的内侧两端位置处均固定安装有与弧形翻转板45外表面贴合对应的减震弹簧套48,第二防护垫块47整体为从上往下向内侧凹陷的圆弧块结构。As shown in Figures 1 to 8, shock-absorbing spring sleeves 48 corresponding to the outer surface of the arc-shaped flip plate 45 are fixedly installed at both ends of the inner side of the second protective pad 47. The second protective pad 47 is an arc block structure that is concave inward from top to bottom.

如图3至图8所示,所述弧形翻转板45远离螺母U形套块44铰接的一端均固定连接有翻转套筒49,导轨槽口架41的背面中间位置处固定连接有两根限位杆410,限位杆410的上滑动套有套口支架411。As shown in Figures 3 to 8, the end of the arc-shaped flip plate 45 that is hinged away from the nut U-shaped sleeve block 44 is fixedly connected to a flip sleeve 49, and two limit rods 410 are fixedly connected to the middle position of the back side of the guide rail slot frame 41, and the upper sliding sleeve of the limit rod 410 is provided with a sleeve bracket 411.

如图3和图4、图6至图8所示,所述套口支架411整体为H形结构,套口支架411的内侧与导轨槽口架41背面之间均通过限位杆410固定连接有复位弹簧412,套口支架411的两侧均活动安装有与翻转套筒49连接的铰接板413。As shown in Figures 3 and 4, and Figures 6 to 8, the sleeve bracket 411 is an H-shaped structure as a whole, and a return spring 412 is fixedly connected between the inner side of the sleeve bracket 411 and the back side of the guide rail slot bracket 41 through a limit rod 410, and hinge plates 413 connected to the flip sleeve 49 are movably installed on both sides of the sleeve bracket 411.

如前述实施例,其联动拉紧机构4为配合颈部防护模块3进行进一步稳定的结构,其具体为:首先其亦可通过翻转块25上侧的电动伸缩杆27控制其伸出的长度,去调节改变导轨槽口架41的位置,以调整第二防护垫块47的托举位置,根据需求可转动导轨槽口架41侧面的调节转扣43,控制双向螺纹杆42进行顺时针转动,使两侧啮合的螺母U形套块44向两侧同步展开,拉开两侧第二防护垫块47的间隔,以适应不同环境使用,两侧的第二防护垫块47均通过弧形翻转板45铰接于螺母U形套块44的外侧,在内侧中间位置处受到力时,两侧的第二防护垫块47可向中间靠近收紧,去托住飞行员的头部或者头盔,进一步的由于第二防护垫块47与弧形翻转板45是通过上侧的翻转接头46铰接的,所以在两侧的第二防护垫块47向中间挤压时,还会以从上往下倾斜的状态去挤压,更能够贴合类圆形的头部,形成更好的托举稳定作用;As in the aforementioned embodiment, the linkage tensioning mechanism 4 is a structure for further stabilizing the neck protection module 3, which is specifically as follows: first, the electric telescopic rod 27 on the upper side of the flip block 25 can be used to control its extended length to adjust the position of the guide rail slot frame 41 to adjust the lifting position of the second protection pad 47. The adjustment buckle 43 on the side of the guide rail slot frame 41 can be rotated according to the needs to control the bidirectional threaded rod 42 to rotate clockwise, so that the nut U-shaped sleeve blocks 44 engaged on both sides are synchronously expanded to both sides, and the interval between the second protection pads 47 on both sides is pulled apart to adapt to different When used in the same environment, the second protective pads 47 on both sides are hinged to the outer side of the nut U-shaped sleeve 44 through the arc-shaped flip plate 45. When a force is applied to the middle position of the inner side, the second protective pads 47 on both sides can be tightened toward the middle to support the pilot's head or helmet. Furthermore, since the second protective pads 47 and the arc-shaped flip plate 45 are hinged through the flip joint 46 on the upper side, when the second protective pads 47 on both sides are squeezed toward the middle, they will also be squeezed in a state of tilting from top to bottom, so that they can better fit the round head and form a better lifting and stabilizing effect.

而为了提高其第二防护垫块47的复位能力,在导轨槽口架41的背面设置有对应的复位弹簧412,在复位弹簧412的复位状态下,套口支架411始终具有一个向外伸出趋势,使得两侧的铰接板413拉动弧形翻转板45,使两侧的第二防护垫块47始终具有向外展开的趋势,以配合其快速复位,在不需要托举时可自动展开,对应的其第二防护垫块47亦为现有技术中的高弹性海绵结构,且整体为圆角形状的圆弧块结构,去提高侧面贴合飞行员时的舒适度。In order to improve the reset ability of the second protection pad 47, a corresponding reset spring 412 is provided on the back side of the guide rail slot frame 41. When the reset spring 412 is in the reset state, the sleeve bracket 411 always has a tendency to extend outward, so that the hinge plates 413 on both sides pull the arc-shaped flip plates 45, so that the second protection pads 47 on both sides always have a tendency to expand outward to cooperate with its rapid reset. When no support is needed, it can be automatically expanded. The corresponding second protection pad 47 is also a high-elasticity sponge structure in the prior art, and the overall structure is a rounded arc block structure to improve the comfort of the side when it fits the pilot.

本发明提供的技术方案工作过程如下:The working process of the technical solution provided by the present invention is as follows:

首先,根据飞行员的体型需求通过插拔板22调整翻转块25的位置,并对应转动U形外翻板24铰接端的螺栓,去调整外侧的倾斜程度,使第一防护垫块32能够处于飞行员的后颈部的位置处,在弹射座椅1被弹射出去更好,对应的安全带将飞行员收紧,收紧的飞行员会紧靠弹射座椅1,使得后颈部贴合在纱网层33上,并进一步向后推动,使翻转块25上侧的导轨槽口架41向前移动,带动两侧的第二防护垫块47从两侧向中间靠近,去稳稳地托住其头部,进行全面的减震缓冲。First, the position of the flip block 25 is adjusted through the plug-in plate 22 according to the pilot's body shape requirements, and the bolts at the hinged end of the U-shaped outer flap 24 are rotated accordingly to adjust the inclination of the outside so that the first protection pad 32 can be located at the position of the pilot's back neck, which is better when the ejection seat 1 is ejected. The corresponding safety belt tightens the pilot, and the tightened pilot will be close to the ejection seat 1, so that the back neck fits on the mesh layer 33 and is further pushed backward, so that the guide slot frame 41 on the upper side of the flip block 25 moves forward, driving the second protection pads 47 on both sides to move from both sides to the middle, to steadily support the pilot's head and perform comprehensive shock absorption and buffering.

本发明涵盖任何在本发明的精髓和范围上做的替代、修改、等效方法以及方案。为了使公众对本发明有彻底的了解,在以下本发明优选实施例中详细说明了具体的细节,而对本领域技术人员来说没有这些细节的描述也可以完全理解本发明。另外,为了避免对本发明的实质造成不必要的混淆,并没有详细说明众所周知的方法、过程、流程、元件和电路等。The present invention covers any substitution, modification, equivalent method and scheme made on the essence and scope of the present invention. In order to make the public have a thorough understanding of the present invention, specific details are described in detail in the following preferred embodiments of the present invention, but those skilled in the art can fully understand the present invention without the description of these details. In addition, in order to avoid unnecessary confusion about the essence of the present invention, well-known methods, processes, procedures, components and circuits are not described in detail.

以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明原理的前提下,还可以作出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above is only a preferred embodiment of the present invention. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the principle of the present invention. These improvements and modifications should also be regarded as the scope of protection of the present invention.

Claims (10)

1.一种用于弹射座椅的减震缓冲机构,包括弹射座椅;其特征在于,所述弹射座椅的背部上侧位置处安装有可调插拔结构,所述可调插拔结构的外侧延伸至弹射座椅的前侧;在所述可调插拔结构上且自下往而上依次配置颈部防护模块和联动拉紧机构;1. A shock absorbing and buffering mechanism for an ejection seat, comprising an ejection seat; characterized in that an adjustable plug-in structure is installed at the upper side of the back of the ejection seat, and the outer side of the adjustable plug-in structure extends to the front side of the ejection seat; a neck protection module and a linkage tensioning mechanism are sequentially arranged on the adjustable plug-in structure from bottom to top; 所述弹射座椅的顶端的中间位置处开设有U形开口,所述可调插拔结构包括插口套框和插拔板,所述插口套框设置在所述U形开口的背侧且与所述U形开口固定连接,所述插拔板插入所述插口套框内,所述颈部防护模块包括设置于插拔板前端下侧位置处的U形敞口架,所述联动拉紧机构包括设置于插拔板前端上侧位置处的导轨槽口架;A U-shaped opening is provided at the middle position of the top of the ejection seat, the adjustable plug-in structure comprises a socket sleeve frame and a plug-in plate, the socket sleeve frame is arranged at the back side of the U-shaped opening and is fixedly connected to the U-shaped opening, the plug-in plate is inserted into the socket sleeve frame, the neck protection module comprises a U-shaped open frame arranged at the lower side of the front end of the plug-in plate, and the linkage tensioning mechanism comprises a guide rail slot frame arranged at the upper side of the front end of the plug-in plate; 其中,所述导轨槽口架的两侧均配置有相对称的第二防护垫块,所述U形敞口架的外侧配置有第一防护垫块,所述第一防护垫块贴合颈部被向后推动过程中带动上部两侧的第二防护垫块向中间收紧托住头部进行减震缓冲。Among them, symmetrical second protective pads are arranged on both sides of the guide rail slot frame, and a first protective pad is arranged on the outer side of the U-shaped open frame. When the first protective pad fits the neck and is pushed backward, it drives the second protective pads on both sides of the upper part to tighten toward the middle to support the head for shock absorption and buffering. 2.根据权利要求1所述的用于弹射座椅的减震缓冲机构,其特征在于,所述插拔板的表面从上往下依次开设多个开口,所述插口套框的侧壁上设置有插口,所述插拔板的开口与所述插口套框的插口通过插入安定位插销固定,所述插拔板的顶部活动铰接有U形外翻板。2. The shock-absorbing and buffering mechanism for an ejection seat according to claim 1 is characterized in that a plurality of openings are sequentially provided on the surface of the plug-in plate from top to bottom, a socket is provided on the side wall of the socket sleeve, the opening of the plug-in plate and the socket of the socket sleeve are fixed by inserting and installing a positioning pin, and a U-shaped outer flap is movably hinged on the top of the plug-in plate. 3.根据权利要求2所述的用于弹射座椅的减震缓冲机构,其特征在于,所述U形外翻板的外侧U形开口端内活动铰接有翻转块;所述翻转块的铰接端侧面转动安装有用收紧螺栓,所述收紧螺栓用于控制所述翻转块的松紧状态,所述翻转块的上下两侧分别固定安装有电动伸缩杆。3. The shock-absorbing and buffering mechanism for an ejection seat according to claim 2 is characterized in that a flip block is movably hinged inside the outer U-shaped opening end of the U-shaped outer flap; a tightening bolt is rotatably installed on the side of the hinged end of the flip block, and the tightening bolt is used to control the tightness of the flip block, and electric telescopic rods are fixedly installed on the upper and lower sides of the flip block respectively. 4.根据权利要求3所述的用于弹射座椅的减震缓冲机构,其特征在于,所述U形敞口架固定连接于所述翻转块下侧的电动伸缩杆上,所述U形敞口架的外敞口端上固定连接有第一防护垫块,所述第一防护垫块表面中间位置处开设有开口;所述第一防护垫块的开口固定连接有纱网层。4. The shock-absorbing and buffering mechanism for an ejection seat according to claim 3 is characterized in that the U-shaped open frame is fixedly connected to the electric telescopic rod on the lower side of the flip block, and a first protective pad is fixedly connected to the outer open end of the U-shaped open frame, and an opening is opened in the middle position of the surface of the first protective pad; the opening of the first protective pad is fixedly connected to a mesh layer. 5.根据权利要求4所述的用于弹射座椅的减震缓冲机构,其特征在于,所述第一防护垫块的内侧面上固定安装有吸附风机,所述吸附风机的吸附端与所述纱网层贴合,所述U形敞口架的后表面中间位置处固定安装有透气槽口架,所述透气槽口架的两侧端均固定安装有气囊块。5. The shock absorbing and buffering mechanism for an ejection seat according to claim 4 is characterized in that an adsorption fan is fixedly installed on the inner side surface of the first protective pad, the adsorption end of the adsorption fan is in contact with the mesh layer, and a breathable slot frame is fixedly installed at the middle position of the rear surface of the U-shaped open frame, and airbag blocks are fixedly installed on both side ends of the breathable slot frame. 6.根据权利要求3所述的用于弹射座椅的减震缓冲机构,其特征在于,所述导轨槽口架固定连接于所述翻转块上侧的电动伸缩杆上,所述导轨槽口架的内部中间位置处活动水平安装有双向螺纹杆,所述双向螺纹杆一侧贯穿伸出导轨槽口架的侧壁且所述双向螺杆的同侧端部固定连接有调节转扣,所述导轨槽口架的内槽口两端相对称的位置处均通过双向螺纹杆啮合安装有螺母U形套块。6. The shock absorbing and buffering mechanism for an ejection seat according to claim 3 is characterized in that the guide rail slot frame is fixedly connected to the electric telescopic rod on the upper side of the flip block, a two-way threaded rod is movably installed horizontally at the inner middle position of the guide rail slot frame, one side of the two-way threaded rod penetrates through the side wall of the guide rail slot frame and an adjusting buckle is fixedly connected to the same side end of the two-way screw rod, and nut U-shaped sleeve blocks are installed at symmetrical positions at both ends of the inner slot of the guide rail slot frame through the engagement of the two-way threaded rod. 7.根据权利要求6所述的用于弹射座椅的减震缓冲机构,其特征在于,所述螺母U形套块的外侧U形槽口内均活动铰接有一个向外倾斜敞开的弧形翻转板,所述弧形翻转板的外表面上侧两端位置处均固定安装有翻转接头,所述弧形翻转板的外表面通过两侧的翻转接头活动安装有第二防护垫块。7. The shock absorbing and buffering mechanism for an ejection seat according to claim 6 is characterized in that an arc-shaped flip plate that is tilted and opened outward is movably hinged in the outer U-shaped groove of the nut U-shaped sleeve block, and flip joints are fixedly installed at both ends of the upper side of the outer surface of the arc-shaped flip plate, and a second protective pad is movably installed on the outer surface of the arc-shaped flip plate through the flip joints on both sides. 8.根据权利要求7所述的用于弹射座椅的减震缓冲机构,其特征在于,所述第二防护垫块的内侧两端位置处均固定安装有与弧形翻转板外表面贴合对应的减震弹簧套,所述第二防护垫块整体为自上而下向背面凹陷的圆弧块结构。8. The shock-absorbing and buffering mechanism for an ejection seat according to claim 7 is characterized in that shock-absorbing spring sleeves corresponding to the outer surface of the arc-shaped flip plate are fixedly installed at both ends of the inner side of the second protective pad block, and the second protective pad block as a whole is an arc block structure that is concave from top to bottom toward the back. 9.根据权利要求7所述的用于弹射座椅的减震缓冲机构,其特征在于,所述弧形翻转板远离螺母U形套块铰接的一端均固定连接有翻转套筒,所述导轨槽口架的背面中间位置处固定连接有两根限位杆,所述限位杆外表面滑动套有套口支架。9. The shock absorbing and buffering mechanism for an ejection seat according to claim 7 is characterized in that one end of the arc-shaped flip plate away from the hinge of the nut U-shaped sleeve block is fixedly connected to a flip sleeve, two limit rods are fixedly connected to the middle position of the back side of the guide rail slot frame, and the outer surface of the limit rod is slidably sleeved with a sleeve bracket. 10.根据权利要求9所述的用于弹射座椅的减震缓冲机构,其特征在于,所述套口支架整体为H形结构,所述套口支架的内侧与导轨槽口架背面之间均固定连接有复位弹簧,所述复位弹簧的一端与所述导轨槽口架背面连接,所述复位弹簧的另一端与所述套口支架连接,所述套口支架的两侧均活动安装有与所述翻转套筒连接的铰接板。10. The shock absorbing and buffering mechanism for an ejection seat according to claim 9 is characterized in that the sleeve bracket is an H-shaped structure as a whole, and a return spring is fixedly connected between the inner side of the sleeve bracket and the back side of the guide rail slot bracket, one end of the return spring is connected to the back side of the guide rail slot bracket, and the other end of the return spring is connected to the sleeve bracket, and hinge plates connected to the flip sleeve are movably installed on both sides of the sleeve bracket.
CN202410991714.7A 2024-07-23 2024-07-23 Damping buffer mechanism for ejection seat Active CN118597426B (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB831472A (en) * 1957-02-22 1960-03-30 Baker Martin Aircraft Co Improvements in or relating to ejection seats for aircraft
US4477041A (en) * 1982-08-19 1984-10-16 Michael Dunne Head and neck restraint system
EP0361369A2 (en) * 1988-09-27 1990-04-04 Rockwell International Corporation Head support/spine offloading ejection seat insert
GB0804037D0 (en) * 2007-03-05 2008-04-09 Ami Ind Inc Aircraft ejection seat with movable headrest
CN212448111U (en) * 2020-04-20 2021-02-02 江西冠一通用飞机有限公司 Seat backrest structure for general aircraft
CN112977845A (en) * 2021-03-04 2021-06-18 北京交通大学 Overturning type head and neck protection device for fighter plane ejection seat
CN113071684A (en) * 2021-03-04 2021-07-06 北京交通大学 Folding sliding type head and neck protection device for fighter plane ejection seat
CN113264191A (en) * 2021-06-16 2021-08-17 上海工程技术大学 Aircraft cockpit seat damping device with over travel protection function
CN216762180U (en) * 2022-01-19 2022-06-17 湖北百星旭昊机电科技有限公司 Damping and buffering device for ejection seat

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB831472A (en) * 1957-02-22 1960-03-30 Baker Martin Aircraft Co Improvements in or relating to ejection seats for aircraft
US4477041A (en) * 1982-08-19 1984-10-16 Michael Dunne Head and neck restraint system
EP0361369A2 (en) * 1988-09-27 1990-04-04 Rockwell International Corporation Head support/spine offloading ejection seat insert
GB0804037D0 (en) * 2007-03-05 2008-04-09 Ami Ind Inc Aircraft ejection seat with movable headrest
CN212448111U (en) * 2020-04-20 2021-02-02 江西冠一通用飞机有限公司 Seat backrest structure for general aircraft
CN112977845A (en) * 2021-03-04 2021-06-18 北京交通大学 Overturning type head and neck protection device for fighter plane ejection seat
CN113071684A (en) * 2021-03-04 2021-07-06 北京交通大学 Folding sliding type head and neck protection device for fighter plane ejection seat
CN113264191A (en) * 2021-06-16 2021-08-17 上海工程技术大学 Aircraft cockpit seat damping device with over travel protection function
CN216762180U (en) * 2022-01-19 2022-06-17 湖北百星旭昊机电科技有限公司 Damping and buffering device for ejection seat

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