CN110853478A - Variable-angle high-speed transmitting device - Google Patents

Variable-angle high-speed transmitting device Download PDF

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Publication number
CN110853478A
CN110853478A CN201911036222.8A CN201911036222A CN110853478A CN 110853478 A CN110853478 A CN 110853478A CN 201911036222 A CN201911036222 A CN 201911036222A CN 110853478 A CN110853478 A CN 110853478A
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gun barrel
support
bracket
frame
gun
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袁绪龙
栗敏
任伟
周方旭
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Northwestern Polytechnical University
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    • G09B25/00Models for purposes not provided for in G09B23/00, e.g. full-sized devices for demonstration purposes
    • G09B25/02Models for purposes not provided for in G09B23/00, e.g. full-sized devices for demonstration purposes of industrial processes; of machinery

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Abstract

The invention discloses a variable-angle high-speed launching device, belonging to the research field of high-speed underwater vehicle underwater test; comprises a front bracket, a gun barrel bracket, a bracket system, a lifting system, a gas tank, a gas pipe and a rear cover of a launching gun; the front bracket and the bracket system are horizontally fixed and are used for supporting the whole launching device; the front end of the gun barrel support is hinged with the top end of the front support, and the rear end of the gun barrel support is supported by the support system, so that the rear end of the gun barrel support is inclined upwards relative to the front end of the gun barrel support; the inclination angle of the gun barrel support is adjusted by adjusting the height of the lifting frame; the gun barrel is fixed on the gun barrel bracket; the gas tank is fixed outside the other side of the support frame of the bracket system; one end of the air pipe is connected with the air tank through an electromagnetic valve, and the other end of the air pipe is connected with the gun barrel; the launching gun rear cover is arranged at the tail end of the gun barrel. The device can replace the transmitting tubes with different calibers, and has good universality, simple and safe operation.

Description

一种变角度高速发射装置A variable-angle high-speed launcher

技术领域technical field

本发明属于水下航行器高速入水试验研究领域,具体涉及一种变角度高速发射装置。The invention belongs to the field of high-speed water entry test research of an underwater vehicle, in particular to a variable-angle high-speed launching device.

背景技术Background technique

新时代的战争已经演化为全方位、立体化的战争。其中占有地球总面积71%的海洋更是新时代战争的主战场之一。目前,世界上诸多军事强国正在积极提高海上军事实力,扩大海上军备优势。在新国际形势下,我国海军武器装备的发展显得尤为重要。针对各型水下航行器的试验研究也成为水下武器装备研制的重要环节。因此,用于水下航行器模型高速入水试验的可变角度高速发射装置尤其重要。The war in the new era has evolved into an all-round and three-dimensional war. Among them, the ocean, which accounts for 71% of the total area of the earth, is one of the main battlefields of war in the new era. At present, many military powers in the world are actively improving their maritime military strength and expanding their maritime armament advantages. Under the new international situation, the development of my country's naval weapons and equipment is particularly important. The experimental research on various types of underwater vehicles has also become an important link in the development of underwater weapons and equipment. Therefore, the variable-angle high-speed launch device for the high-speed water entry test of the underwater vehicle model is particularly important.

现有技术背景下,在《西北工业大学学报》2015年3月第36卷第2期299-304页《超空泡模型对固态介质侵彻及影响因素实验研究》中,文章图2中Ф25mm口径空气炮如附图6中所示,其高压室直径为200mm,长2m,最大发射压力1Mpa,发射管长4m,发射速度范围30~300m/s。其发射装置仅能实现水平角度的发射,发射过程中产生过大的冲击力。现有装置中缺少一种可调角度的稳定的高速发射装置,本发明可以在一定的范围内实现水下航行器入水角和入水速度的要求,填补当前试验研究发射装置的空白。Under the background of the existing technology, in the "Experimental Research on the Penetration and Influencing Factors of the Supercavitation Model to Solid Media" in "Journal of Northwestern Polytechnical University", Vol. 36, No. 2, March 2015, Ф25mm The caliber air cannon is shown in Figure 6. Its high-pressure chamber is 200mm in diameter, 2m long, with a maximum firing pressure of 1Mpa, a firing tube of 4m long, and a firing speed range of 30 to 300m/s. Its launching device can only achieve horizontal angle launch, which generates excessive impact force during the launch process. The existing device lacks a stable high-speed launch device with an adjustable angle. The invention can meet the requirements of the water entry angle and entry speed of the underwater vehicle within a certain range, and fill the gap of the current experimental research launch device.

发明内容SUMMARY OF THE INVENTION

要解决的技术问题:Technical problem to be solved:

为了避免现有技术的不足之处,本发明提出一种变角度高速发射装置,能够将航行器模型以一定的角度和速度发射入水,用于对航行器入水冲击载荷与入水弹道特性的研究;该装置结构简单紧凑,适用性良好。In order to avoid the deficiencies of the prior art, the present invention proposes a variable-angle high-speed launching device, which can launch the aircraft model into the water at a certain angle and speed, and is used for the research on the impact load and the ballistic characteristics of the aircraft entering the water; The device has a simple and compact structure and good applicability.

本发明的技术方案是:一种变角度高速发射装置,其特征在于:包括前支架、炮管、炮管支架、支架系统、升降系统、气罐、气管和发射炮后盖;所述前支架和支架系统水平固定,用于支撑整个发射装置;所述炮管支架的前端与所述前支架的顶端铰接,其后端通过所述支架系统支撑,使得所述炮管支架的后端相对于其前端向上倾斜;The technical scheme of the present invention is: a variable-angle high-speed launching device, which is characterized in that it includes a front bracket, a gun barrel, a gun barrel bracket, a bracket system, a lifting system, a gas tank, a gas pipe and a rear cover of the launching gun; the front bracket and the bracket system is horizontally fixed to support the entire launching device; the front end of the gun barrel bracket is hinged with the top end of the front bracket, and its rear end is supported by the bracket system, so that the rear end of the gun barrel bracket is relative to the its front end slopes upward;

所述支架系统包括底板和支撑框架,所述支撑框架竖直固定于所述底板上;所述升降系统包括钢丝绳、滑轮、升降架和卷扬机,所述卷扬机固定于所述支撑框架的一侧外,所述滑轮固定于所述支撑框架的顶部,所述卷扬机的钢丝绳经过所述滑轮将所述升降架悬挂于所述支撑框架内,通过对钢丝绳的拽引控制所述升降架的高度;所述炮管支架的后部分安装于所述升降架上,通过调节所述升降架的高度进而调节所述炮管支架的倾斜角度;The support system includes a base plate and a support frame, and the support frame is vertically fixed on the base plate; the lift system includes a wire rope, a pulley, a lift frame and a winch, and the winch is fixed on one side of the support frame. , the pulley is fixed on the top of the support frame, the wire rope of the hoist suspends the lift frame in the support frame through the pulley, and the height of the lift frame is controlled by pulling the wire rope; The rear part of the gun barrel bracket is installed on the lifting frame, and the inclination angle of the gun barrel bracket is adjusted by adjusting the height of the lifting frame;

所述炮管固定于所述炮管支架上;所述气罐固定于所述支架系统的支撑框架的另一侧外;所述气管一端经过电磁阀与所述气罐连接,另一端与所述炮管连接;所述发射炮后盖安装于所述炮管的末端。The gun barrel is fixed on the gun barrel bracket; the gas tank is fixed on the other side of the support frame of the bracket system; one end of the gas pipe is connected with the gas tank through a solenoid valve, and the other end is connected with the The gun barrel is connected; the rear cover of the launch gun is installed at the end of the gun barrel.

本发明的进一步技术方案是:所述升降架包括上支撑杆、下支撑杆、中间支撑杆和炮管架支撑杆;所述上支撑杆和下支撑杆通过两个所述中间支撑杆相互平行固定,所述炮管支架的后部分穿过所述上支撑杆、下支撑杆之间并搭装于所述下支撑杆上;两个所述炮管架支撑杆垂直固定于所述下支撑杆上,用于限制所述炮管支架沿所述炮管的切向位移;A further technical solution of the present invention is: the lift frame includes an upper support rod, a lower support rod, an intermediate support rod and a gun barrel support rod; the upper support rod and the lower support rod are parallel to each other through the two intermediate support rods Fixed, the rear part of the gun barrel bracket passes between the upper support rod and the lower support rod and is mounted on the lower support rod; two of the gun barrel support rods are vertically fixed to the lower support rod on the rod, for limiting the tangential displacement of the gun barrel support along the gun barrel;

所述上支撑杆和下支撑杆的两端均设置有滚轮结构,与所述支撑框架两内侧面沿竖直方向开的滑槽配合安装,能够限制所述升降架沿竖直方向上下移动。Both ends of the upper support rod and the lower support rod are provided with roller structures, which are installed in cooperation with the chute opened on the two inner sides of the support frame in the vertical direction, which can limit the vertical movement of the lifting frame.

本发明的进一步技术方案是:所述支架系统的支撑框架两侧均设置有加强筋。A further technical solution of the present invention is that: reinforcing ribs are provided on both sides of the support frame of the support system.

本发明的进一步技术方案是:所述炮管通过U型螺栓固定于炮管支架上。A further technical solution of the present invention is that: the gun barrel is fixed on the gun barrel bracket through U-shaped bolts.

本发明的进一步技术方案是:所述支架系统的支撑框架顶部中心处开有通孔,所述钢丝绳经过所述滑轮后穿过所述通孔,保证所述升降架位于所述支架系统的中间位置。A further technical solution of the present invention is: a through hole is opened at the center of the top of the support frame of the support system, and the wire rope passes through the through hole after passing through the pulley, so as to ensure that the lifting frame is located in the middle of the support system Location.

本发明的进一步技术方案是:所述上支撑杆、下支撑杆与中间支撑杆之间均通过U型螺栓固定连接,U型螺栓使用螺母旋紧以防止松动。A further technical solution of the present invention is that: the upper support rod, the lower support rod and the middle support rod are all fixedly connected by U-shaped bolts, and the U-shaped bolts are tightened with nuts to prevent loosening.

有益效果beneficial effect

本发明的有益效果在于:本发明提出的一种变角度高速发射装置,可以在前支架和发射支架固定的情况下通过升降系统预设发射角度,可以使模型最大以45度的角度斜入水;调整气罐充气压力设定发射速度,从发射管后端装入模型,由电磁阀远程控制发射,使试验模型按要求的角度和速度发射。当模型在发射炮管内在高压气体推动下向前运动时,炮管将在C点(C点为炮管支架前端和炮管连接中心处)受到沿炮管轴向的后坐力F1;在B点(发射炮支架系统上的下支撑与炮管接触处)受到钢丝绳向上的拉力F2;故对于A点(炮管支架前端和前支架连接处)而言受到力矩M1且M1=F1×LCA(LCA为A点和C点之间的距离)和反向力矩M2且M2=F2×LAB(LAB为A点和B点之间的距离),M1=-M2,从而实现后坐力和力矩的合理分配,使得前支架和支架系统受力合理分配,保证了发射炮工作过程中稳定性。本发明装置可更换不同口径的发射管,通用性好,操作简便、安全。The beneficial effects of the present invention are: the variable-angle high-speed launching device proposed by the present invention can preset the launching angle through the lifting system when the front bracket and the launching bracket are fixed, so that the model can be inclined into the water at a maximum angle of 45 degrees; Adjust the inflation pressure of the gas tank to set the launch speed, load the model from the back end of the launch tube, and remotely control the launch by the solenoid valve, so that the test model is launched at the required angle and speed. When the model moves forward under the push of high-pressure gas in the launching gun barrel, the gun barrel will experience the recoil force F1 along the barrel axis at point C (point C is the front end of the gun barrel bracket and the center of the connection of the gun barrel); at point B (The contact between the lower support on the gun support system and the gun barrel) is subjected to the upward pulling force F2 of the wire rope; therefore, for point A (the connection between the front end of the gun barrel support and the front support), it is subjected to a moment M1 and M1=F1×L CA ( L CA is the distance between point A and point C) and the reverse moment M2 and M2=F2×L AB (L AB is the distance between point A and point B), M1=-M2, so as to realize the recoil force and moment The reasonable distribution of the front bracket and the bracket system makes the force distribution of the front bracket and bracket system reasonable, which ensures the stability of the launcher during the working process. The device of the invention can replace the launch tubes of different calibers, and has good versatility, simple and safe operation.

附图说明Description of drawings

图1为本发明装置的受力分析简图,Fig. 1 is the schematic diagram of the force analysis of the device of the present invention,

图2为本发明的结构示意图,展示了各部件位置FIG. 2 is a schematic structural diagram of the present invention, showing the position of each component

图3为升降系统及支架系统示意图Figure 3 is a schematic diagram of the lifting system and the support system

图4为升降系统局部示意图的主视图及俯视图4 is a front view and a top view of a partial schematic diagram of the lifting system

图5为升降系统中U型螺栓连接剖视图Figure 5 is a sectional view of the U-bolt connection in the lifting system

图6为参考文献中Ф25mm口径空气炮Figure 6 shows the Ф25mm caliber air gun in the reference

附图标记说明:1-前支架,2-炮管支架,3-炮管,4-支架系统,5-钢丝绳,6-滑轮,7-升降系统,8-气罐,9-气管,10-发射炮后盖,11-卷扬机,12-上支撑杆,13-中间支撑杆,14-炮管架支撑杆,15-下支撑杆,16-U型螺栓。Description of reference numerals: 1-front bracket, 2-barrel bracket, 3-barrel, 4-bracket system, 5-wire rope, 6-pulley, 7-lifting system, 8-air tank, 9-air pipe, 10- Cannon rear cover, 11- hoist, 12- upper support rod, 13- middle support rod, 14- gun barrel support rod, 15- lower support rod, 16- U-bolt.

具体实施方式Detailed ways

下面通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention and should not be construed as limiting the present invention.

在本发明的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”、“顺时针”、“逆时针”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,因此不能理解为对本发明的限制。In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", " rear, left, right, vertical, horizontal, top, bottom, inside, outside, clockwise, counterclockwise, etc., or The positional relationship is based on the orientation or positional relationship shown in the accompanying drawings, which is 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 specific orientation, be constructed and operated in a specific orientation, Therefore, it should not be construed as a limitation of the present invention.

如图2所示,本发射一种变角度高速发射装置包括前支架1、炮管支架2、炮管3、支架系统4、钢丝绳5、滑轮6、升降系统7、气罐8、气管9、发射炮后盖10、卷扬机11。前支架1和支架系统4由钢材焊接而成并水平固定于地面,用于支撑整个发射装置;支架系统4包括底板和支撑框架,所述支撑框架竖直固定于所述底板上;参照图3,升降系统7包括钢丝绳5、滑轮6、升降架和卷扬机11,所述卷扬机11固定于所述支撑框架左侧台阶面上,滑轮6固定于所述支撑框架的顶部,卷扬机11的钢丝绳5经过滑轮6将所述升降架悬挂于所述支撑框架内,通过对钢丝绳5的拽引控制所述升降架的高度;支架系统4的支撑框架顶部中心处开有通孔,钢丝绳5经过滑轮6后穿过所述通孔,保证所述升降架位于所述支架系统的中间位置。As shown in Figure 2, a variable-angle high-speed launching device for this launch includes a front bracket 1, a gun barrel bracket 2, a gun barrel 3, a bracket system 4, a wire rope 5, a pulley 6, a lifting system 7, a gas tank 8, a gas pipe 9, The rear cover of the launch gun 10 and the hoist 11. The front bracket 1 and the bracket system 4 are welded by steel and are fixed on the ground horizontally to support the entire launcher; the bracket system 4 includes a base plate and a support frame, and the support frame is vertically fixed on the base plate; refer to FIG. 3 , the lifting system 7 includes a wire rope 5, a pulley 6, a lifting frame and a winch 11, the winch 11 is fixed on the left step surface of the support frame, the pulley 6 is fixed on the top of the support frame, and the steel wire rope 5 of the winch 11 passes through The pulley 6 suspends the lifting frame in the support frame, and controls the height of the lifting frame by pulling the wire rope 5; Passing through the through hole ensures that the lifting frame is located in the middle position of the support system.

参照图4和图5,所述升降架包括上支撑杆12、下支撑杆15、中间支撑杆13和炮管架支撑杆14;上支撑杆12和下支撑杆15通过两个中间支撑杆13相互平行固定,炮管支架2的后部分穿过上支撑杆12、下支撑杆15之间并搭装于下支撑杆15上,所述上支撑杆、下支撑杆与中间支撑杆之间均通过U型螺栓固定连接,U型螺栓使用螺母旋紧以防止松动;上支撑杆12和下支撑杆15的两端均设置有滚轮结构,与所述支撑框架两内侧面沿竖直方向开的滑槽配合安装,能够限制所述升降架沿竖直方向上、下移动;4 and 5, the lift frame includes an upper support rod 12, a lower support rod 15, an intermediate support rod 13 and a gun barrel support rod 14; the upper support rod 12 and the lower support rod 15 pass through the two intermediate support rods 13 Fixed parallel to each other, the rear part of the gun barrel bracket 2 passes between the upper support rod 12 and the lower support rod 15 and is mounted on the lower support rod 15, and the upper support rod, the lower support rod and the middle support rod are all The U-bolts are fixed and connected, and the U-bolts are tightened with nuts to prevent loosening; both ends of the upper support rod 12 and the lower support rod 15 are provided with roller structures, which are vertically open with the inner sides of the support frame. The chute is installed together, which can restrict the lifting frame from moving up and down in the vertical direction;

两个炮管架支撑杆14垂直固定于下支撑杆15上,用于限制所述炮管支架2沿炮管3的切向位移;通过调节所述升降架的高度进而调节所述炮管支架的倾斜角度。The two gun barrel support rods 14 are vertically fixed on the lower support rod 15 to limit the tangential displacement of the gun barrel support 2 along the gun barrel 3; adjust the gun barrel support by adjusting the height of the lifting frame angle of inclination.

炮管3通过U型螺栓16固定与炮管支架2上,炮管支架2前端使用螺杆与前支架1上铰接连接,其后端安装在升降系统4内,此时使用卷扬机11的遥控设备便可以前支架上的螺杆为支撑点上下调节炮管,实现发射装置的变角度功能。The gun barrel 3 is fixed to the gun barrel bracket 2 by the U-shaped bolt 16. The front end of the gun barrel bracket 2 is hingedly connected to the front bracket 1 by means of a screw rod, and its rear end is installed in the lifting system 4. At this time, the remote control equipment of the winch 11 is used. The screw on the front bracket can be used as a supporting point to adjust the gun barrel up and down to realize the variable angle function of the launching device.

气罐8安放在支架系统右侧框架内,气罐有外置接口与空压机连接以补充高压气体并连接压力表显示气罐内的压力;气管9一端经过电磁阀与气罐8连接,另一端与炮管3连接。通过向气罐8内充入高压气体可以实现发射装置以一定的速度推动试验模型出管。The gas tank 8 is placed in the frame on the right side of the support system, and the gas tank has an external interface to connect with the air compressor to supplement high-pressure gas and connect a pressure gauge to display the pressure in the gas tank; one end of the gas pipe 9 is connected to the gas tank 8 through a solenoid valve, The other end is connected to the barrel 3. By filling the gas tank 8 with high-pressure gas, the launching device can push the test model out of the tube at a certain speed.

本发明的安装及使用过程:Installation and use process of the present invention:

首先将发射装置安装于合适的试验区域内,其次使用卷扬机的遥控设备将发射装置调整到水平状态便于操作人员安装,打开该装置发射炮后盖,装入试验模型,再拧上发射炮后盖,再使用卷扬机的遥控设备将发射装置调整到所需要的发射角度。然后使用外置气源向气罐内充入指定压力的高压气体。由发控系统打开电磁阀,气罐内的高压气体进入模型后方,推动模型在炮管内加速到指定速度离管,完成发射任务。First, install the launcher in a suitable test area, then use the remote control device of the hoist to adjust the launcher to a horizontal state for the operator to install, open the back cover of the launcher of the device, load it into the test model, and then screw on the back cover of the launcher , and then use the hoist's remote control device to adjust the launcher to the desired launch angle. Then use the external gas source to fill the gas tank with high-pressure gas of the specified pressure. The solenoid valve is opened by the launch control system, and the high-pressure gas in the gas tank enters the rear of the model, pushing the model to accelerate to the specified speed in the gun barrel and leave the tube to complete the launch task.

尽管上面已经示出和描述了本发明的实施例,可以理解的是,上述实施例是示例性的,不能理解为对本发明的限制,本领域的普通技术人员在不脱离本发明的原理和宗旨的情况下在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。Although the embodiments of the present invention have been shown and described above, it should be understood that the above embodiments are exemplary and should not be construed as limiting the present invention, and those of ordinary skill in the art will not depart from the principles and spirit of the present invention Variations, modifications, substitutions, and alterations to the above-described embodiments are possible within the scope of the present invention without departing from the scope of the present invention.

Claims (6)

1. A variable-angle high-speed transmitting device is characterized in that: comprises a front bracket, a gun barrel bracket, a bracket system, a lifting system, a gas tank, a gas pipe and a rear cover of a launching gun; the front bracket and the bracket system are horizontally fixed and are used for supporting the whole launching device; the front end of the gun barrel support is hinged with the top end of the front support, and the rear end of the gun barrel support is supported by the support system, so that the rear end of the gun barrel support is inclined upwards relative to the front end of the gun barrel support;
the support system comprises a bottom plate and a support frame, and the support frame is vertically fixed on the bottom plate; the lifting system comprises a steel wire rope, a pulley, a lifting frame and a winch, the winch is fixed outside one side of the supporting frame, the pulley is fixed at the top of the supporting frame, the steel wire rope of the winch enables the lifting frame to be hung in the supporting frame through the pulley, and the height of the lifting frame is controlled by dragging the steel wire rope; the rear part of the gun barrel support is arranged on the lifting frame, and the inclination angle of the gun barrel support is adjusted by adjusting the height of the lifting frame;
the gun barrel is fixed on the gun barrel bracket; the gas tank is fixed outside the other side of the support frame of the bracket system; one end of the air pipe is connected with the air tank through an electromagnetic valve, and the other end of the air pipe is connected with the gun barrel; the launching gun rear cover is arranged at the tail end of the gun barrel.
2. The variable angle high speed transmitting device of claim 1, wherein: the lifting frame comprises an upper supporting rod, a lower supporting rod, a middle supporting rod and a gun barrel frame supporting rod; the upper supporting rod and the lower supporting rod are fixed in parallel through the two middle supporting rods, and the rear part of the gun barrel support penetrates through the space between the upper supporting rod and the lower supporting rod and is lapped on the lower supporting rod; the two gun tube rack support rods are vertically fixed on the lower support rod and used for limiting the tangential displacement of the gun tube bracket along the gun tube;
the both ends of going up bracing piece and bottom suspension vaulting pole all are provided with the gyro wheel structure, with the spout cooperation installation of opening along vertical direction of two medial surfaces of braced frame can restrict the crane reciprocates along vertical direction.
3. The variable angle high speed transmitting device of claim 1, wherein: and reinforcing ribs are arranged on two sides of the supporting frame of the bracket system.
4. The variable angle high speed transmitting device of claim 1, wherein: the gun barrel is fixed on the gun barrel support through a U-shaped bolt.
5. The variable angle high speed transmitting device of claim 1, wherein: a through hole is formed in the center of the top of a supporting frame of the support system, and the steel wire rope passes through the through hole after passing through the pulley, so that the lifting frame is located in the middle of the support system.
6. The variable angle high speed transmitting device of claim 1, wherein: go up between bracing piece, the bottom suspension vaulting pole and the middle support bar all through U type bolt fixed connection, U type bolt uses the nut to screw in order to prevent not hard up.
CN201911036222.8A 2019-10-29 2019-10-29 Variable-angle high-speed transmitting device Pending CN110853478A (en)

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CN111351631A (en) * 2020-03-30 2020-06-30 中国科学院力学研究所 An experimental device for entering and exiting water with constrained launch

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Application publication date: 20200228