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CN115214901A - A high-pressure gas ejection device and method with controllable acceleration - Google Patents

A high-pressure gas ejection device and method with controllable acceleration Download PDF

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Publication number
CN115214901A
CN115214901A CN202210898810.8A CN202210898810A CN115214901A CN 115214901 A CN115214901 A CN 115214901A CN 202210898810 A CN202210898810 A CN 202210898810A CN 115214901 A CN115214901 A CN 115214901A
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ejection
reset
cylinder
piston
piston rod
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CN115214901B (en
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田海飞
张华良
尹钊
徐玉杰
陈海生
沈昊天
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Zhongke Nanjing Future Energy System Research Institute
Institute of Engineering Thermophysics of CAS
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Zhongke Nanjing Future Energy System Research Institute
Institute of Engineering Thermophysics of CAS
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/04Ground or aircraft-carrier-deck installations for launching aircraft
    • B64F1/06Ground or aircraft-carrier-deck installations for launching aircraft using catapults
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66DCAPSTANS; WINCHES; TACKLES, e.g. PULLEY BLOCKS; HOISTS
    • B66D1/00Rope, cable, or chain winding mechanisms; Capstans
    • B66D1/02Driving gear
    • B66D1/08Driving gear incorporating fluid motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66DCAPSTANS; WINCHES; TACKLES, e.g. PULLEY BLOCKS; HOISTS
    • B66D1/00Rope, cable, or chain winding mechanisms; Capstans
    • B66D1/60Rope, cable, or chain winding mechanisms; Capstans adapted for special purposes
    • B66D1/74Capstans
    • B66D1/7442Capstans having a horizontal rotation axis
    • B66D1/7447Capstans having a horizontal rotation axis driven by motor only
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/06Servomotor systems without provision for follow-up action; Circuits therefor involving features specific to the use of a compressible medium, e.g. air, steam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/16Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/06Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with two or more servomotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/02Mechanical layout characterised by the means for converting the movement of the fluid-actuated element into movement of the finally-operated member
    • F15B15/06Mechanical layout characterised by the means for converting the movement of the fluid-actuated element into movement of the finally-operated member for mechanically converting rectilinear movement into non- rectilinear movement
    • F15B15/065Mechanical layout characterised by the means for converting the movement of the fluid-actuated element into movement of the finally-operated member for mechanically converting rectilinear movement into non- rectilinear movement the motor being of the rack-and-pinion type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/08Characterised by the construction of the motor unit
    • F15B15/14Characterised by the construction of the motor unit of the straight-cylinder type
    • F15B15/1404Characterised by the construction of the motor unit of the straight-cylinder type in clusters, e.g. multiple cylinders in one block
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66DCAPSTANS; WINCHES; TACKLES, e.g. PULLEY BLOCKS; HOISTS
    • B66D2700/00Capstans, winches or hoists
    • B66D2700/01Winches, capstans or pivots
    • B66D2700/0125Motor operated winches
    • B66D2700/0133Fluid actuated

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Actuator (AREA)

Abstract

本发明公开了一种加速度可控的高压气体弹射装置及方法,包括高压气罐、弹射气缸、复位气缸、活塞杆、复位活塞、充气管道、弹射活塞、充气阀门、复位排气阀门、动力齿轮、绞盘、传动绳索和载体车;高压气罐通过充气管道与弹射气缸连通,充气阀门设置于充气管道上,复位活塞设置于复位气缸内,弹射活塞设置于弹射气缸内,弹射气缸和复位气缸共用一根活塞杆,复位排气阀门设置于复位气缸上;活塞杆上设有齿条,动力齿轮与活塞杆的齿条啮合,动力齿轮与齿轮变速器同轴设置,齿轮变速器的输出端与绞盘连接,传动绳索缠绕于绞盘上,传动绳索与载体车连接。实现弹射加速度的可控调节,使弹射体在特定的弹射轨道长度下实现最大的弹射出口速度。

Figure 202210898810

The invention discloses a high-pressure gas ejection device and method with controllable acceleration, comprising a high-pressure gas tank, an ejection cylinder, a reset cylinder, a piston rod, a reset piston, an inflation pipeline, an ejection piston, an inflation valve, a reset exhaust valve, and a power gear. , winch, transmission rope and carrier vehicle; the high-pressure air tank is connected to the ejection cylinder through the inflation pipeline, the inflation valve is set on the inflation pipeline, the reset piston is set in the reset cylinder, the ejection piston is set in the ejection cylinder, and the ejection cylinder and the reset cylinder are shared A piston rod, the reset exhaust valve is arranged on the reset cylinder; the piston rod is provided with a rack, the power gear meshes with the rack of the piston rod, the power gear and the gear transmission are coaxially arranged, and the output end of the gear transmission is connected with the winch , the transmission rope is wound on the winch, and the transmission rope is connected with the carrier vehicle. The controllable adjustment of the ejection acceleration is realized, so that the ejection body can achieve the maximum ejection exit velocity under the specific ejection track length.

Figure 202210898810

Description

一种加速度可控的高压气体弹射装置及方法A high-pressure gas ejection device and method with controllable acceleration

技术领域technical field

本发明涉及弹射技术领域,特别是一种加速度可控的高压气体弹射装置及方法。The invention relates to the technical field of ejection, in particular to a high-pressure gas ejection device and method with controllable acceleration.

背景技术Background technique

随着无人机技术的发展,无人机在各行业的应用越来越广泛:其中固定翼无人机的起飞重量大、速度快、滞空时间长,不同型号的无人机在野外勘测、军事侦察打击、军事演习训练,灾难救援及日常航拍等领域具有广泛的应用前景。但是固定翼无人机常规起飞方式受到地形和跑道的制约,且在起飞阶段消耗的能量占比很高。目前已有的技术包括液压弹射、电磁弹射、蒸汽弹射等,但由于经济或技术上的不足,在应用中需要较高的专业知识、普适性差等缺点,推广应用的难度较大。而压缩气体弹射动力技术以高压气体为主要动力来源,通过动力气缸等装置来带动无人机发射起飞,使其获得较高的初速度和加速度,该技术具有弹射成本低、爆发力强、能源易得、通用性好、维护方便等诸多优势,国内外应用压缩气体进行无人机发射已有比较成熟的应用产品。With the development of UAV technology, UAVs are more and more widely used in various industries: fixed-wing UAVs have large take-off weight, fast speed, and long stay in the air. Different types of UAVs are used in field surveys, It has broad application prospects in the fields of military reconnaissance and strike, military exercise training, disaster rescue and daily aerial photography. However, the conventional take-off method of fixed-wing UAVs is restricted by terrain and runways, and consumes a high proportion of energy during the take-off phase. At present, the existing technologies include hydraulic ejection, electromagnetic ejection, steam ejection, etc., but due to economic or technical deficiencies, the application requires high professional knowledge, poor universality and other shortcomings, and it is difficult to popularize and apply. The compressed gas ejection power technology uses high-pressure gas as the main power source, and drives the UAV to launch and take off through power cylinders and other devices, so that it can obtain a higher initial speed and acceleration. This technology has the advantages of low ejection cost, strong explosive power, and easy energy. There are many advantages such as good versatility, convenient maintenance, etc., there are relatively mature application products using compressed gas for UAV launch at home and abroad.

然而当前对压缩空气弹射系统的研究设计围绕实现特定的弹射出口速度展开,弹射过程为短时间内的突变过程,弹射开始后加速度迅速达到峰值后又急速下降,对弹射体产生的冲击力是突变的,易对弹射体造成冲击损坏;同时加速度的突变,使一定长度的弹射轨道所实现的速度较小,因此达到设计的弹射速度不得不设计较长的弹射轨道,系统紧凑性差;而且压缩气体弹射系统所采用的行程加速系统由滑轮绳索组成,加速系统稳定性差,且加速比固定不能调节,造成弹射系统的通用性较差。However, the current research and design of the compressed air ejection system revolves around the realization of a specific ejection exit velocity. The ejection process is a short-term mutation process. After the ejection starts, the acceleration quickly reaches the peak and then drops rapidly. The impact force on the projectile is a sudden change. It is easy to cause impact damage to the projectile; at the same time, the sudden change of acceleration makes the speed achieved by a certain length of the ejection track smaller, so to achieve the designed ejection speed, a longer ejection track has to be designed, and the system has poor compactness; and the compressed gas The stroke acceleration system used in the ejection system is composed of pulley ropes, the stability of the acceleration system is poor, and the acceleration ratio cannot be adjusted, resulting in poor universality of the ejection system.

发明内容SUMMARY OF THE INVENTION

本发明要解决的技术问题是针对上述现有技术的不足,而提供一种加速度可控的高压气体弹射装置及方法,弹射气缸内的压力保持恒定,在相同的气缸行程条件下,实现特定弹射体在强度耐受基础上具有最大且固定的弹射加速度,进而实现特定的弹射轨道长度下最大的弹射出口速度,或在更短的弹射轨道长度下,实现一定的弹射出口速度。The technical problem to be solved by the present invention is to provide a high-pressure gas ejection device and method with a controllable acceleration in view of the deficiencies of the above-mentioned prior art. The body has a maximum and fixed ejection acceleration on the basis of strength tolerance, and then achieves the maximum ejection exit velocity under a specific ejection track length, or achieves a certain ejection exit velocity under a shorter ejection track length.

为解决上述技术问题,本发明采用的技术方案是:In order to solve the above-mentioned technical problems, the technical scheme adopted in the present invention is:

一种加速度可控的高压气体弹射装置,包括高压气罐、弹射气缸、复位气缸、活塞杆、复位活塞、充气管道、弹射活塞、充气阀门、复位排气阀门、动力齿轮、绞盘、齿轮变速器、传动绳索和载体车;高压气罐通过充气管道与弹射气缸连通,充气阀门设置于充气管道上,复位活塞设置于复位气缸内,弹射活塞设置于弹射气缸内,活塞杆一端连接复位活塞,另一端连接弹射活塞,弹射气缸和复位气缸共用一根活塞杆,复位排气阀门设置于复位气缸上;活塞杆上设有齿条,动力齿轮与活塞杆的齿条啮合,动力齿轮与齿轮变速器同轴设置,齿轮变速器的输出端与绞盘连接,传动绳索缠绕于绞盘上,传动绳索的一端与载体车连接。A high-pressure gas ejection device with controllable acceleration, comprising a high-pressure gas tank, an ejection cylinder, a reset cylinder, a piston rod, a reset piston, an inflation pipeline, an ejection piston, an inflation valve, a reset exhaust valve, a power gear, a winch, a gear transmission, Transmission rope and carrier vehicle; high-pressure air tank is communicated with the ejection cylinder through the inflation pipeline, the inflation valve is arranged on the inflation pipeline, the reset piston is arranged in the reset cylinder, the ejection piston is arranged in the ejection cylinder, one end of the piston rod is connected to the reset piston, and the other end is connected to the ejection cylinder. Connect the ejection piston, the ejection cylinder and the reset cylinder share a piston rod, the reset exhaust valve is set on the reset cylinder; the piston rod is provided with a rack, the power gear meshes with the rack of the piston rod, and the power gear is coaxial with the gear transmission The output end of the gear transmission is connected with the winch, the transmission rope is wound on the winch, and one end of the transmission rope is connected with the carrier vehicle.

作为本发明的进一步优选,还包括复位管道、复位充气阀门和弹射排气阀门;高压气罐通过复位管道与复位气缸连通,复位充气阀门设置于复位管道上,弹射排气阀门设置于弹射气缸上。As a further preference of the present invention, it also includes a reset pipeline, a reset inflation valve and an ejection exhaust valve; the high-pressure gas tank is communicated with the reset cylinder through the reset pipeline, the reset inflation valve is arranged on the reset pipeline, and the ejection exhaust valve is arranged on the ejection cylinder. .

作为本发明的进一步优选,还包括连通管道和中间阀门,连通管道将复位气缸和弹射气缸连通,中间阀门设置于连通管道上。As a further preference of the present invention, it also includes a communication pipe and an intermediate valve, the communication pipe communicates the reset cylinder and the ejection cylinder, and the intermediate valve is arranged on the communication pipe.

作为本发明的进一步优选,还包括限位齿轮,活塞杆的两侧均设有齿条,限位齿轮与动力齿轮分别啮合于活塞杆两侧的齿条上。As a further preference of the present invention, a limit gear is also included, racks are provided on both sides of the piston rod, and the limit gear and the power gear are respectively meshed with the racks on both sides of the piston rod.

作为本发明的进一步优选,活塞杆为偏心杆,动力齿轮与活塞杆的啮合线中点所连成的直线为复位活塞、复位气缸、弹射活塞和弹射气缸的轴线。As a further preference of the present invention, the piston rod is an eccentric rod, and the straight line formed by the midpoint of the meshing line of the power gear and the piston rod is the axis of the reset piston, the reset cylinder, the ejection piston and the ejection cylinder.

作为本发明的进一步优选,还包括弹射轨道,所述弹射轨道倾斜设置,载体车设置于弹射轨道上,载体车在传动绳索的牵引下从低处向高处移动。As a further preference of the present invention, it also includes an ejection track, the ejection track is inclined and the carrier vehicle is arranged on the ejection track, and the carrier vehicle moves from a low place to a high place under the traction of the transmission rope.

一种加速度可控的高压气体弹射方法,步骤(1)、弹射阶段:开始弹射时,打开充气阀门和复位排气阀门,其余阀门关闭;高压气罐向弹射气缸供气驱动弹射活塞向左运动,活塞杆伸出弹射气缸的同时,通过位于活塞杆上的齿条驱动动力齿轮和限位齿轮转动;通过传动绳索的缠绕收起对载体车拉动;通过调节齿轮变速器,可以调节传动绳索拉动长度和活塞杆伸出长度的比,进而控制连接传动绳索且在弹射轨道上移动的载体车的弹射加速度,实现加速度的调节,适用于不同的弹射体;步骤(2-2)、复位阶段:弹射完成后,关闭充气阀门和复位排气阀门,打开复位充气阀门和弹射排气阀门,高压气罐中的气体流向复位气缸,推动复位活塞反向运动,在活塞杆的齿条的啮合作用下,带动动力齿轮反向转动,进而通过齿轮变速器带动绞盘反向转动,释放传动绳索,载体车拖动传动绳索返回弹射出发点;当弹射活塞复位到初始位置时,关闭复位充气阀门和弹射排气阀门,打开复位排气阀门,准备进入下一个弹射循环。A high-pressure gas ejection method with controllable acceleration, step (1), ejection stage: when the ejection starts, open the inflation valve and reset the exhaust valve, and the remaining valves are closed; the high-pressure gas tank supplies air to the ejection cylinder to drive the ejection piston to move to the left When the piston rod extends out of the ejection cylinder, the power gear and the limit gear are driven to rotate by the rack on the piston rod; the carrier vehicle is pulled by winding and retracting the transmission rope; by adjusting the gear transmission, the pulling length of the transmission rope can be adjusted The ratio of the extension length of the piston rod to control the ejection acceleration of the carrier vehicle connected to the transmission rope and moving on the ejection track to realize the adjustment of the acceleration, which is suitable for different projectiles; step (2-2), reset stage: ejection After completion, close the charging valve and reset exhaust valve, open the reset charging valve and ejection exhaust valve, the gas in the high-pressure gas tank flows to the reset cylinder, push the reset piston to move in the opposite direction, under the meshing action of the rack of the piston rod, Drive the power gear to rotate in the reverse direction, and then drive the winch to rotate in the reverse direction through the gear transmission, release the transmission rope, and the carrier vehicle drags the transmission rope back to the ejection starting point; when the ejection piston returns to the initial position, close the reset inflation valve and ejection exhaust valve, Open the reset exhaust valve in preparation for the next ejection cycle.

作为本发明的进一步优选,步骤(1)与步骤(2-2)之间还包括步骤(2-1);步骤(2-1):关闭充气阀门和复位排气阀门,打开中间阀门,利用弹射气缸中残余的中高压气体,中高压气体通过中间阀门流向复位气缸,当弹射气缸和复位气缸内的压力平衡时,关闭中间阀门。As a further preference of the present invention, step (2-1) is also included between step (1) and step (2-2); step (2-1): close the inflation valve and reset the exhaust valve, open the middle valve, use The residual medium and high pressure gas in the ejection cylinder flows to the reset cylinder through the intermediate valve. When the pressure in the ejection cylinder and the reset cylinder are balanced, the intermediate valve is closed.

本发明具有如下有益效果:The present invention has the following beneficial effects:

1、弹射加速度的恒定可以防止加速度剧烈变化导致弹射体受到剧烈冲击力,实现弹射体在强度耐受基础上具有最大且固定的弹射加速度,进而实现特定的弹射轨道长度下最大的弹射出口速度,或实现一定的弹射出口速度时弹射轨道长度较小;1. The constant ejection acceleration can prevent the ejection body from being subjected to severe impact force due to the drastic change of acceleration, realize the maximum and fixed ejection acceleration of the ejection body on the basis of strength tolerance, and then realize the maximum ejection exit velocity under the specific ejection track length, Or the length of the ejection track is small when a certain ejection exit velocity is achieved;

2、弹射气缸复位时利用了气缸内残存的中高压气体能量,提高了能量利用率;2. When the ejection cylinder is reset, the residual medium and high pressure gas energy in the cylinder is used to improve the energy utilization rate;

3、动力齿轮和限位齿轮对伸出气缸的活塞杆起到导向作用,有效避免了活塞杆伸出过长时端部不稳,活塞杆的偏心设计使啮合力的作用线即啮合线中点所连成的直线与活塞与气缸的轴线重合,防止活塞长期承受偏心力,进而延长活塞及气缸部件的使用寿命。3. The power gear and limit gear play a guiding role for the piston rod extending out of the cylinder, which effectively avoids the instability of the end of the piston rod when it is extended for too long. The eccentric design of the piston rod makes the action line of the meshing force in the meshing line. The straight line formed by the points coincides with the axes of the piston and the cylinder, preventing the piston from bearing eccentric force for a long time, thereby prolonging the service life of the piston and cylinder components.

4、齿轮/齿条行程转换结构和齿轮变速器,可以在弹射气缸内压力不变的情况下,通过调整齿轮变速器的变速比,成比例的改变弹射体的弹射加速度,进而实现不同的弹射出口速度要求,相比滑轮组变速系统,调节方面,可靠性更高,便于维护。4. The gear/rack stroke conversion structure and gear transmission can proportionally change the ejection acceleration of the projectile by adjusting the speed ratio of the gear transmission under the condition that the pressure in the ejection cylinder remains unchanged, thereby achieving different ejection exit speeds Compared with the pulley block speed change system, the adjustment is more reliable and easy to maintain.

附图说明Description of drawings

图1是本发明的结构示意图;Fig. 1 is the structural representation of the present invention;

图2是本发明的动力齿轮、齿轮变速器和绞盘的连接示意图;Fig. 2 is the connection schematic diagram of the power gear of the present invention, the gear transmission and the winch;

图3是本发明的传动拉索与载体车的连接示意图;Fig. 3 is the connection schematic diagram of the transmission cable of the present invention and the carrier vehicle;

图4是本发明弹射阶段的示意图;Figure 4 is a schematic diagram of the ejection stage of the present invention;

图5是本发明复位阶段的示意图。Figure 5 is a schematic diagram of the reset phase of the present invention.

其中有:1.高压气罐;2.充气阀门;3.弹射排气阀门;4.弹射气缸;5.弹射活塞;6.活塞杆;7.齿条;8.动力齿轮;9.限位齿轮;10.复位活塞;11.复位气缸;12.复位排气阀门;13.复位充气阀门;14.中间阀门;15.绞盘;16.传动绳索;17.弹射轨道;18.载体车;19.弹射体;20.齿轮变速器;21.充气管道;22.连通管道;23.复位管道。Among them are: 1. High pressure gas tank; 2. Inflatable valve; 3. Ejection exhaust valve; 4. Ejection cylinder; 5. Ejection piston; 6. Piston rod; 7. Rack; 8. Power gear; 9. Limit Gear; 10. Reset piston; 11. Reset cylinder; 12. Reset exhaust valve; 13. Reset inflation valve; 14. Intermediate valve; 15. Winch; 16. Drive rope; 17. Ejection track; 18. Carrier cart; . projectile; 20. gear transmission; 21. inflation pipe; 22. communication pipe; 23. reset pipe.

具体实施方式Detailed ways

下面结合附图和具体较佳实施方式对本发明作进一步详细的说明。The present invention will be described in further detail below with reference to the accompanying drawings and specific preferred embodiments.

本发明的描述中,需要理解的是,术语“左侧”、“右侧”、“上部”、“下部”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,“第一”、“第二”等并不表示零部件的重要程度,因此不能理解为对本发明的限制。本实施例中采用的具体尺寸只是为了举例说明技术方案,并不限制本发明的保护范围。In the description of the present invention, it should be understood that the orientation or positional relationship indicated by the terms "left side", "right side", "upper", "lower part", etc. are based on the orientation or positional relationship shown in the drawings, only For the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a particular orientation, be constructed and operate in a particular orientation, "first", "second", etc. importance, and therefore should not be construed as a limitation to the present invention. The specific dimensions used in this embodiment are only for illustrating the technical solution, and do not limit the protection scope of the present invention.

如图1-5所示,一种加速度可控的高压气体弹射装置,包括高压气罐1、弹射气缸4、复位气缸11、活塞杆6、复位活塞10、充气管道21、弹射活塞5、充气阀门2、复位排气阀门12、动力齿轮8、绞盘15、传动绳索16和载体车18;高压气罐1通过充气管道21与弹射气缸4连通,充气阀门2设置于充气管道21上,复位活塞10设置于复位气缸11内,弹射活塞5设置于弹射气缸4内,活塞杆6一端连接复位活塞10,另一端连接弹射活塞5,弹射气缸4和复位气缸11共用一根活塞杆6,复位排气阀门12设置于复位气缸11上。As shown in Figures 1-5, a high-pressure gas ejection device with controllable acceleration includes a high-pressure gas tank 1, an ejection cylinder 4, a reset cylinder 11, a piston rod 6, a reset piston 10, an inflation pipe 21, an ejection piston 5, and an inflation Valve 2, reset exhaust valve 12, power gear 8, winch 15, transmission rope 16 and carrier vehicle 18; high-pressure gas tank 1 is communicated with ejection cylinder 4 through charging pipe 21, and charging valve 2 is arranged on the charging pipe 21 to reset the piston 10 is arranged in the reset cylinder 11, the ejection piston 5 is arranged in the ejection cylinder 4, one end of the piston rod 6 is connected with the reset piston 10, and the other end is connected with the ejection piston 5, the ejection cylinder 4 and the reset cylinder 11 share a piston rod 6, and the reset row The air valve 12 is arranged on the reset cylinder 11 .

活塞杆6上设有齿条7,动力齿轮8与活塞杆6的齿条7啮合,还包括齿轮变速器20,动力齿轮8与齿轮变速器20同轴设置,齿轮变速器20的输出端与绞盘15连接。传动绳索16缠绕于绞盘15上,传动绳索16的末端连接载体车18,载体车18用来放置弹射体19。The piston rod 6 is provided with a rack 7, the power gear 8 meshes with the rack 7 of the piston rod 6, and also includes a gear transmission 20, the power gear 8 and the gear transmission 20 are coaxially arranged, and the output end of the gear transmission 20 is connected with the winch 15. . The drive rope 16 is wound on the winch 15 , and the end of the drive rope 16 is connected to the carrier cart 18 , which is used to place the projectile 19 .

在弹射过程,活塞杆6直接/间接推动弹射体19而中所受到的负载是常量,只要通过一系列控制使气缸内的压力保持恒定,则气缸活塞的加速度也会保持恒定,相应的通过一系列传动机构传导给无人机的加速度也会保持恒定。During the ejection process, the load received by the piston rod 6 directly/indirectly pushing the ejection body 19 is constant. As long as the pressure in the cylinder is kept constant through a series of controls, the acceleration of the cylinder piston will also remain constant. The acceleration transmitted to the drone by the series transmission mechanism will also remain constant.

还包括复位管道23、复位充气阀门13和弹射排气阀门3;高压气罐1通过复位管道23与复位气缸11连通,复位充气阀门13设置于复位管道23上,弹射排气阀门3设置于弹射气缸4上。利用高压气罐1的气体压力使活塞杆6从左往右移动,带动动力齿轮8回转,同时绞盘15上的传动绳索16放长,载体车18回到最初起点复位。It also includes a reset pipeline 23, a reset inflation valve 13 and an ejection exhaust valve 3; the high-pressure gas tank 1 is communicated with the reset cylinder 11 through the reset pipeline 23, the reset inflation valve 13 is arranged on the reset pipeline 23, and the ejection exhaust valve 3 is arranged on the ejection on cylinder 4. Using the gas pressure of the high-pressure gas tank 1, the piston rod 6 moves from left to right, driving the power gear 8 to rotate, and at the same time, the transmission rope 16 on the winch 15 is extended, and the carrier vehicle 18 returns to the original starting point.

还包括连通管道22和中间阀门14,连通管道22将复位气缸11和弹射气缸4连通,中间阀门14设置于连通管道22上。连通管道22在弹射完成后,关闭充气阀门2和复位排气阀门12,打开中间阀门14,利用弹射气缸4中残余的中高压气体,中高压气体通过中间阀门14流向复位气缸11,使弹射气缸4和复位气缸11内的压力平衡,以减少高压气罐1内气体的使用。It also includes a communication pipe 22 and an intermediate valve 14 . The communication pipe 22 communicates the reset cylinder 11 with the ejection cylinder 4 , and the intermediate valve 14 is arranged on the communication pipe 22 . After the ejection of the communication pipe 22 is completed, the inflation valve 2 and the reset exhaust valve 12 are closed, the intermediate valve 14 is opened, and the medium and high pressure gas remaining in the ejection cylinder 4 is used, and the medium and high pressure gas flows to the reset cylinder 11 through the intermediate valve 14 to make the ejection cylinder 4. Balance the pressure in the reset cylinder 11 to reduce the use of gas in the high-pressure gas tank 1.

同时高压气罐1、弹射气缸4和复位气缸11上均设有压力传感器和温度传感器,采集高压气罐1内的压力和温度,由此得到高压气罐1流向弹射气缸4的单位流通面积的质量流量,由于流向弹射气缸4的高压气体的压力、温度已知,且需要在弹射气缸4内进行膨胀,通过控制阀门流通面积,使流向弹射气缸4的高压气体质量能够维持弹射气缸4内的压力恒定。At the same time, the high-pressure gas tank 1, the ejection cylinder 4 and the reset cylinder 11 are all provided with pressure sensors and temperature sensors to collect the pressure and temperature in the high-pressure gas tank 1, thereby obtaining the unit flow area of the high-pressure gas tank 1 flowing to the ejection cylinder 4. Mass flow, since the pressure and temperature of the high-pressure gas flowing to the ejection cylinder 4 are known, and it needs to be expanded in the ejection cylinder 4, by controlling the flow area of the valve, the mass of the high-pressure gas flowing to the ejection cylinder 4 can be maintained in the ejection cylinder 4. The pressure is constant.

还包括限位齿轮9,活塞杆6的两侧均设有齿条7,限位齿轮9与动力齿轮8分别啮合于活塞杆6两侧的齿条7上。限位齿轮9防止活塞杆6在啮合处受力侧弯,使活塞杆6上的齿与动力齿轮8保持良好的啮合。It also includes a limit gear 9 , both sides of the piston rod 6 are provided with racks 7 , and the limit gear 9 and the power gear 8 are respectively meshed with the racks 7 on both sides of the piston rod 6 . The limit gear 9 prevents the piston rod 6 from bending sideways under force at the meshing place, so that the teeth on the piston rod 6 maintain a good meshing with the power gear 8 .

活塞杆6为偏心杆,动力齿轮8与活塞杆6的啮合线中点所连成的直线为复位活塞10、复位气缸11、弹射活塞5和弹射气缸4的轴线,防止活塞承受轴向偏心力。The piston rod 6 is an eccentric rod, and the straight line formed by the midpoint of the meshing line of the power gear 8 and the piston rod 6 is the axis of the reset piston 10, the reset cylinder 11, the ejection piston 5 and the ejection cylinder 4 to prevent the piston from bearing the axial eccentric force .

所以绞盘15上的传动绳索16收起的长度远大于弹射活塞5向左移动的距离。通过传动绳索16的缠绕收起对载体车18的拉动,从而使较短的气缸行程带动弹射体19具有较大的弹射行程。Therefore, the retracted length of the drive rope 16 on the winch 15 is much greater than the distance the ejection piston 5 moves to the left. The pulling of the carrier cart 18 is retracted by the winding of the transmission rope 16 , so that the short cylinder stroke drives the projectile 19 to have a large projectile stroke.

通过调节齿轮变速器20,可以调节传动绳索16拉动长度和活塞杆6伸出长度的比,进而控制连接传动绳索16且在弹射轨道17上移动的载体车18的弹射加速度,实现加速度的调节,适用于不同的弹射体19。By adjusting the gear transmission 20, the ratio of the pulling length of the transmission rope 16 to the extension length of the piston rod 6 can be adjusted, thereby controlling the ejection acceleration of the carrier vehicle 18 connected to the transmission rope 16 and moving on the ejection track 17, so as to realize the adjustment of the acceleration, suitable for on different projectiles 19.

活塞与弹射体19运动关系说明:Description of the motion relationship between the piston and the projectile 19:

由于变速器的输入轴为动力齿轮8轴,输出轴为绞盘15轴,设齿轮变速器20转速比(输出轴/输入轴)为π,动力齿轮8的中心半径为r,与变速器输出轴同轴的绞盘15传动半径为R。由于变速器输入轴和输出轴的功率相等(P=T*n/9550),Since the input shaft of the transmission is the power gear 8 shaft, and the output shaft is the capstan shaft 15, let the gear transmission 20 speed ratio (output shaft/input shaft) be π, the center radius of the power gear 8 is r, and the output shaft of the transmission is coaxial. The transmission radius of the winch 15 is R. Since the power of the transmission input shaft and output shaft is equal (P=T*n/9550),

a)故输入轴扭矩(Fin*r)与输出轴扭矩(Fout*r)的比为π;a) Therefore, the ratio of input shaft torque (F in *r) to output shaft torque (F out *r) is π;

b)即动力齿轮8端的啮合力沿轴向的分力Fin(不考虑活塞阻力时Fin等于弹射活塞5受到的压力)/传动绳索16的拉力Fout (不考虑载体车18的阻力时Fout为加速度力)为π*R/r;b) That is, the component force F in along the axial direction of the meshing force at the end of the power gear 8 (Fin is equal to the pressure on the ejection piston 5 when the resistance of the piston is not considered)/the pulling force F out of the transmission rope 16 (F out when the resistance of the carrier vehicle 18 is not considered) out is the acceleration force) is π*R/r;

c)传动绳索16的牵引(加)速度/活塞的(加)速度为π*R/r;c) The traction (acceleration) speed of the drive rope 16/the (acceleration) speed of the piston is π*R/r;

d)相应的弹射体19的弹射行程/活塞的行程也为π*R/r,进而在弹射气缸4较短的行程下可以实现弹射体19在较长的轨道上进行弹射。d) The corresponding ejection stroke/piston stroke of the projectile 19 is also π*R/r, so that the projectile 19 can be ejected on a longer track under the shorter stroke of the ejection cylinder 4.

在弹射气缸4内压力恒定的情况下,Fin不变,因此Fout也不变,可以拉动载体车18以恒定加速度进行弹射,此外通过调节变速器的转速比π,可以相应的的调节弹射加速度。Under the condition that the pressure in the ejection cylinder 4 is constant, F in does not change, so F out also remains unchanged. The carrier cart 18 can be pulled to eject at a constant acceleration. In addition, by adjusting the speed ratio π of the transmission, the ejection acceleration can be adjusted accordingly. .

还包括弹射轨道17,所述弹射轨道17倾斜设置,载体车18设置于弹射轨道17上,弹射体19设置于载体车18上,载体车18在传动绳索16的牵引下从低处向高处移动。It also includes an ejection track 17, the ejection track 17 is arranged obliquely, the carrier vehicle 18 is arranged on the ejection track 17, the ejection body 19 is arranged on the carrier vehicle 18, and the carrier vehicle 18 is pulled by the transmission rope 16 from a low place to a high place. move.

一种加速度可控的高压气体弹射方法:A high-pressure gas ejection method with controlled acceleration:

步骤(1)、弹射阶段:开始弹射时,打开充气阀门2和复位排气阀门12,其余阀门关闭;高压气罐1向弹射气缸4供气驱动弹射活塞5向左运动,活塞杆6伸出弹射气缸4的同时,通过位于活塞杆6上的齿条7驱动动力齿轮8和限位齿轮9转动;通过传动绳索16的缠绕收起对载体车18拉动;通过调节齿轮变速器20,可以调节传动绳索16拉动长度和活塞杆6伸出长度的比,进而控制连接传动绳索16且在弹射轨道17上移动的载体车18的弹射加速度,实现加速度的调节,适用于不同的弹射体;Step (1), ejection stage: when the ejection starts, open the inflation valve 2 and reset the exhaust valve 12, and the other valves are closed; the high-pressure air tank 1 supplies air to the ejection cylinder 4 to drive the ejection piston 5 to move to the left, and the piston rod 6 extends At the same time of ejecting the cylinder 4, the power gear 8 and the limit gear 9 are driven to rotate by the rack 7 located on the piston rod 6; the carrier cart 18 is pulled by the winding and retracting of the transmission rope 16; by adjusting the gear transmission 20, the transmission can be adjusted. The ratio between the pulling length of the rope 16 and the extension length of the piston rod 6, and then control the ejection acceleration of the carrier vehicle 18 connected to the transmission rope 16 and moving on the ejection track 17, so as to realize the adjustment of the acceleration, which is suitable for different projectiles;

步骤(2-1):弹射完成后,关闭充气阀门2和复位排气阀门12,打开中间阀门14,利用弹射气缸4中残余的中高压气体,中高压气体通过中间阀门14流向复位气缸11,当弹射气缸4和复位气缸11内的压力平衡时,关闭中间阀门14。Step (2-1): After the ejection is completed, close the inflation valve 2 and reset the exhaust valve 12, open the intermediate valve 14, use the residual medium and high pressure gas in the ejection cylinder 4, and the medium and high pressure gas flows through the intermediate valve 14 to the reset cylinder 11, When the pressures in the ejection cylinder 4 and the reset cylinder 11 are equalized, the intermediate valve 14 is closed.

步骤(2-2)、复位阶段:弹射完成后,关闭充气阀门2和复位排气阀门12,打开复位充气阀门13和弹射排气阀门3,高压气罐1中的气体流向复位气缸11,推动复位活塞10反向运动,在活塞杆6的齿条的啮合作用下,带动动力齿轮8反向转动,进而通过齿轮变速器20带动绞盘15反向转动,释放传动绳索16,载体车18拖动传动绳索16返回弹射出发点;当弹射活塞5复位到初始位置时,关闭复位充气阀门13和弹射排气阀门3,打开复位排气阀门12,准备进入下一个弹射循环。Step (2-2), reset stage: after the ejection is completed, close the inflation valve 2 and reset exhaust valve 12, open the reset inflation valve 13 and ejection exhaust valve 3, the gas in the high-pressure gas tank 1 flows to the reset cylinder 11, push The reset piston 10 moves in the reverse direction, under the meshing action of the rack of the piston rod 6, it drives the power gear 8 to rotate in the reverse direction, and then drives the winch 15 to rotate in the reverse direction through the gear transmission 20, releases the transmission rope 16, and the carrier vehicle 18 drives the transmission The rope 16 returns to the ejection starting point; when the ejection piston 5 is reset to the initial position, the reset inflation valve 13 and ejection exhaust valve 3 are closed, and the reset exhaust valve 12 is opened, ready to enter the next ejection cycle.

以上详细描述了本发明的优选实施方式,但是,本发明并不限于上述实施方式中的具体细节,在本发明的技术构思范围内,可以对本发明的技术方案进行多种等同变换,这些等同变换均属于本发明的保护范围。The preferred embodiments of the present invention have been described in detail above. However, the present invention is not limited to the specific details of the above-mentioned embodiments. Within the scope of the technical concept of the present invention, various equivalent transformations can be made to the technical solutions of the present invention. These equivalent transformations All belong to the protection scope of the present invention.

Claims (8)

1. The utility model provides a controllable high-pressure gas jettison device of acceleration which characterized in that: the device comprises a high-pressure gas tank (1), an ejection cylinder (4), a reset cylinder (11), a piston rod (6), a reset piston (10), an inflation pipeline (21), an ejection piston (5), an inflation valve (2), a reset exhaust valve (12), a power gear (8), a winch (15), a gear transmission (20), a transmission rope (16) and a carrier vehicle (18);
the high-pressure gas tank (1) is communicated with the ejection cylinder (4) through a gas charging pipeline (21), a gas charging valve (2) is arranged on the gas charging pipeline (21), a reset piston (10) is arranged in a reset cylinder (11), the ejection piston (5) is arranged in the ejection cylinder (4), one end of a piston rod (6) is connected with the reset piston (10), the other end of the piston rod is connected with the ejection piston (5), the ejection cylinder (4) and the reset cylinder (11) share one piston rod (6), and a reset exhaust valve (12) is arranged on the reset cylinder (11);
the gear transmission mechanism is characterized in that a rack (7) is arranged on the piston rod (6), the power gear (8) is meshed with the rack (7) of the piston rod (6), the power gear (8) and the gear transmission (20) are coaxially arranged, the output end of the gear transmission (20) is connected with the winch (15), the transmission rope (16) is wound on the winch (15), and one end of the transmission rope (16) is connected with the carrier vehicle (18).
2. The accelerated velocity controlled high pressure gas ejection apparatus as claimed in claim 1, wherein: the device also comprises a reset pipeline (23), a reset inflation valve (13) and an ejection exhaust valve (3); the high-pressure gas tank (1) is communicated with the reset cylinder (11) through a reset pipeline (23), the reset inflation valve (13) is arranged on the reset pipeline (23), and the ejection exhaust valve (3) is arranged on the ejection cylinder (4).
3. The acceleration-controllable high-pressure gas ejection device as claimed in claim 2, wherein: the ejection mechanism is characterized by further comprising a communicating pipeline (22) and a middle valve (14), wherein the communicating pipeline (22) is used for communicating the reset cylinder (11) with the ejection cylinder (4), and the middle valve (14) is arranged on the communicating pipeline (22).
4. The accelerated velocity controlled high pressure gas ejection apparatus as claimed in claim 1, wherein: the piston rod is characterized by further comprising a limiting gear (9), racks (7) are arranged on two sides of the piston rod (6), and the limiting gear (9) and the power gear (8) are respectively meshed with the racks (7) on two sides of the piston rod (6).
5. The accelerated velocity controlled high pressure gas ejection apparatus as claimed in claim 1, wherein: the piston rod (6) is an eccentric rod, and a straight line formed by connecting the middle points of meshing lines of the power gear (8) and the piston rod (6) is superposed with the axes of the reset piston (10), the reset cylinder (11), the ejection piston (5) and the ejection cylinder (4).
6. The accelerated velocity controlled high pressure gas ejection apparatus as claimed in claim 1, wherein: the device is characterized by further comprising an ejection track (17), wherein the ejection track (17) is obliquely arranged, the carrier vehicle (18) is arranged on the ejection track (17), and the carrier vehicle (18) moves from a low position to a high position under the traction of the transmission rope (16).
7. An acceleration-controllable high-pressure gas ejection method according to any one of claims 1 to 6, characterized in that:
step (1) and ejection stage: when the ejection is started, the inflation valve (2) and the reset exhaust valve (12) are opened, and the other valves are closed; the high-pressure gas tank (1) supplies gas to the ejection cylinder (4) to drive the ejection piston (5) to move leftwards, and the piston rod (6) extends out of the ejection cylinder (4) and simultaneously drives the power gear (8) and the limiting gear (9) to rotate through the rack (7) positioned on the piston rod (6); the carrier vehicle (18) is pulled by winding and retracting the transmission rope (16); the ratio of the pulling length of the transmission rope (16) to the extending length of the piston rod (6) can be adjusted by adjusting the gear transmission (20), so that the ejection acceleration of a carrier vehicle (18) which is connected with the transmission rope (16) and moves on the ejection track (17) is controlled, the adjustment of the acceleration is realized, and the device is suitable for different ejectors;
step (2-2), resetting: after the ejection is finished, the inflation valve (2) and the reset exhaust valve (12) are closed, the reset inflation valve (13) and the ejection exhaust valve (3) are opened, the gas in the high-pressure gas tank (1) flows to the reset cylinder (11), the reset piston (10) is pushed to move in the reverse direction, the power gear (8) is driven to rotate in the reverse direction under the meshing action of the rack of the piston rod (6), the winch (15) is driven to rotate in the reverse direction through the gear speed changer (20), the transmission rope (16) is released, and the carrier vehicle (18) drags the transmission rope (16) to return to the ejection starting point; when the ejection piston (5) is reset to the initial position, the reset inflation valve (13) and the ejection exhaust valve (3) are closed, and the reset exhaust valve (12) is opened to prepare for entering the next ejection cycle.
8. The acceleration-controllable high-pressure gas ejection method according to claim 7, wherein: a step (2-1) is also included between the step (1) and the step (2-2);
step (2-1): and closing the inflation valve (2) and the reset exhaust valve (12), opening the intermediate valve (14), utilizing residual medium-high pressure gas in the ejection cylinder (4), leading the medium-high pressure gas to flow to the reset cylinder (11) through the intermediate valve (14), and closing the intermediate valve (14) when the pressures in the ejection cylinder (4) and the reset cylinder (11) are balanced.
CN202210898810.8A 2022-07-28 2022-07-28 Acceleration-controllable high-pressure gas ejection device and method Active CN115214901B (en)

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Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB150411A (en) * 1919-05-29 1920-08-30 W G Armstrong Improvements in or relating to apparatus for launching aeroplanes from floating structures or other restricted areas
FR1016921A (en) * 1944-10-09 1952-11-26 Lima Hamilton Corp Pressure control of a free piston engine
US6536708B1 (en) * 1998-05-26 2003-03-25 Prospective Concepts Ag Take-off device for airplanes
US20110225961A1 (en) * 2008-12-10 2011-09-22 Numatics, Incorporated Pressurized Air-Spring Return Cylinder and Pneumatic Intensifier System
CN102765486A (en) * 2012-08-16 2012-11-07 刘光其 Shipboard aircraft ejection device for aircraft carrier
CN103010478A (en) * 2012-12-11 2013-04-03 淮南市明月环保科技有限责任公司 Power equipment and process of aircraft catapult
CN206417215U (en) * 2016-12-15 2017-08-18 邵大伟 Launch the ejection firing device of the cable traction of the gas storage promotion of gas or gas recoverable
CN110466793A (en) * 2018-05-09 2019-11-19 沈金钟 A kind of twin-tub side opening internal combustion type aircraft carrier ejector
US10962030B1 (en) * 2019-12-05 2021-03-30 Dadco, Inc. Pneumatic cylinder
CN217969960U (en) * 2022-07-28 2022-12-06 中科南京未来能源系统研究院 A high-pressure gas ejection device with controllable acceleration

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB150411A (en) * 1919-05-29 1920-08-30 W G Armstrong Improvements in or relating to apparatus for launching aeroplanes from floating structures or other restricted areas
FR1016921A (en) * 1944-10-09 1952-11-26 Lima Hamilton Corp Pressure control of a free piston engine
US6536708B1 (en) * 1998-05-26 2003-03-25 Prospective Concepts Ag Take-off device for airplanes
US20110225961A1 (en) * 2008-12-10 2011-09-22 Numatics, Incorporated Pressurized Air-Spring Return Cylinder and Pneumatic Intensifier System
CN102765486A (en) * 2012-08-16 2012-11-07 刘光其 Shipboard aircraft ejection device for aircraft carrier
CN103010478A (en) * 2012-12-11 2013-04-03 淮南市明月环保科技有限责任公司 Power equipment and process of aircraft catapult
CN206417215U (en) * 2016-12-15 2017-08-18 邵大伟 Launch the ejection firing device of the cable traction of the gas storage promotion of gas or gas recoverable
CN110466793A (en) * 2018-05-09 2019-11-19 沈金钟 A kind of twin-tub side opening internal combustion type aircraft carrier ejector
US10962030B1 (en) * 2019-12-05 2021-03-30 Dadco, Inc. Pneumatic cylinder
CN217969960U (en) * 2022-07-28 2022-12-06 中科南京未来能源系统研究院 A high-pressure gas ejection device with controllable acceleration

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