Ground-mounted ammunition vehicle

Abstract

The present application relates to the field of missile assembly technology, and in particular to a ground assembly vehicle, comprising: a walking mechanism and a lifting mechanism, a hoisting mechanism and an assembly auxiliary mechanism arranged on the walking mechanism; wherein the walking mechanism is used for omnidirectional movement on the working surface; the hoisting mechanism is used for hoisting the missile launcher, and the hoisting mechanism can be lifted and lowered relative to the walking mechanism through the lifting mechanism; the assembly auxiliary mechanism is used for installing missiles compatible with the missile launcher. The ground assembly vehicle transfers the installation process of missiles and missile launchers to the ground, and the assembled launcher is directly installed into the interior of the aircraft ammunition bay, shortening the operation time of the missile and launcher mounting, reducing the difficulty of mounting, and being safer. Moreover, the whole process has a high degree of mechanization, which improves the assembly efficiency of missiles and launchers and shortens the combat response time of the troops.

Description

Technical Field

[0001] The present application relates to the technical field of missile assembly, and in particular to a ground missile assembly vehicle. Background Art

[0002] At present, the assembly process of missiles and missile launchers is as follows: the launcher needs to be fixed to the aircraft in advance, and the missile is lifted to the inside of the aircraft for installation. There are many obstructions, which makes installation difficult and reduces assembly efficiency, affecting combat response time. Summary of the invention

[0003] The purpose of the present application is to provide a ground assembly vehicle, which to a certain extent solves the technical problems in the prior art that the assembly of missiles and missile launchers is difficult, time-consuming and labor-intensive, and affects the combat response time.

[0004] The present application provides a ground ammunition assembly vehicle, comprising: a walking mechanism and a lifting mechanism, a hoisting mechanism and an ammunition assembly auxiliary mechanism arranged on the walking mechanism; wherein the walking mechanism is used for omnidirectional movement on a working surface;

[0005] The hoisting mechanism is used for hoisting the missile launcher, and the hoisting mechanism can be lifted and lowered relative to the walking mechanism through the lifting mechanism; the missile assembly auxiliary mechanism is used for installing missiles compatible with the missile launcher.

[0006] In the above technical solution, further, the hoisting mechanism includes a horizontal position adjustment mechanism, a first hoisting auxiliary mechanism, a second hoisting auxiliary mechanism, a lifting mechanism and a rotation adjustment mechanism;

[0007] Wherein, the first lifting auxiliary mechanism and the second lifting auxiliary mechanism can adjust the horizontal position relative to the walking mechanism through the horizontal position adjustment mechanism; the second lifting auxiliary mechanism can adjust the height position relative to the walking mechanism through the lifting mechanism;

[0008] The second lifting auxiliary mechanism is used to install the missile launcher, and the rotation adjustment mechanism is used to adjust the angle between the missile launcher lifted on the second lifting auxiliary mechanism and the horizontal direction.

[0009] In any of the above technical solutions, further, the horizontal position adjustment mechanism includes a first support member, a second support member, a longitudinal drive assembly and a transverse drive assembly; wherein the first support member is rotatably connected to an end of the lifting mechanism away from the walking mechanism;

[0010] The second supporting member is provided with the first supporting member, and the second supporting member can be moved in the longitudinal direction of the first supporting member by the longitudinal driving assembly, and the second supporting member can be moved in the transverse direction of the first supporting member by the transverse driving assembly;

[0011] The first hoisting auxiliary mechanism and the second hoisting auxiliary mechanism are both arranged on the second supporting member.

[0012] In any of the above technical solutions, further, the first lifting auxiliary mechanism includes a support body, a lifting arm, a first guide limiting member and a second guide limiting member; wherein the lifting arm is vertically connected to the support body; the support body is formed with a mounting groove, and the lifting mechanism is arranged in the mounting groove;

[0013] The first guide and limit member is connected to one end of the hanging arm, the rotation adjustment mechanism is connected to the other end opposite to the hanging arm, and the second guide and limit member is connected to the rotation adjustment mechanism;

[0014] The first guide and position-limiting member is formed with a first guide and position-limiting portion, and the second guide and position-limiting member is formed with a second guide and position-limiting portion.

[0015] In any of the above technical solutions, further, the second lifting auxiliary mechanism includes a fixed beam, a lifting ring and a clamping claw member;

[0016] Wherein, a third guide limit portion which is mutually limited with the first guide limit portion is formed at one end of the fixed beam, and a fourth guide limit portion which is mutually limited with the second guide limit portion is formed at the other opposite end of the fixed beam;

[0017] The clamping claw member and the lifting ring are both arranged on the fixed beam.

[0018] In any of the above technical solutions, further, the lifting mechanism includes a mounting seat, a guide wheel, a pulley, a rope, a hook and a first driving device; wherein the mounting seat, the guide wheel and the pulley are sequentially arranged on the second supporting member along the length direction of the second supporting member;

[0019] The rope is rotatably wound around the support shaft of the mounting seat, and one end of the rope passes through the guide wheel and bypasses the pulley to be connected to the hook;

[0020] The first driving device is connected to the supporting shaft and is used for driving the supporting shaft to rotate.

[0021] In any of the above technical solutions, further, the assembly auxiliary mechanism includes a first mounting member, a second mounting member, a third mounting member, a bearing member, a clamping member and a lifting assembly;

[0022] The walking mechanism is formed with a mounting notch, the first mounting member is arranged in the notch, and the first mounting member is detachably connected to the walking mechanism; the second mounting member is connected to the first mounting member, and the second mounting member is formed with a mounting cavity, and the third mounting member and the lifting assembly are both arranged in the mounting cavity;

[0023] The third mounting member is connected to the lifting assembly, and the third mounting member is lifted and lowered relative to the second mounting member through the lifting assembly;

[0024] The bearing member is slidably connected to the third mounting member, and the bearing member can slide along a horizontal direction relative to the third mounting member; the clamping member is arranged on the bearing member.

[0025] In any of the above technical solutions, further, there are multiple load-bearing members, and the multiple load-bearing members are arranged in sequence along the width direction of the walking mechanism; any of the load-bearing members is provided with multiple clamping members; and / or

[0026] The clamping member comprises a clamping portion, a shielding portion and a connecting portion connected to each other;

[0027] The bearing component is formed with an installation groove, the connecting portion is inserted into the installation groove, the shielding portion covers the opening of the installation groove, and the clamping portion is located outside the installation groove; the connecting portion is sleeved with an elastic component.

[0028] In any of the above technical solutions, further, the lifting mechanism includes a second driving device, a screw transmission assembly, a first support beam and a second support beam; wherein the first support beam and the second support beam are cross-rotatably connected;

[0029] One end of the first support beam is slidably connected to the walking mechanism, the second driving device drives the first support beam to slide relative to the walking mechanism through the screw transmission assembly, and the other end of the first support beam is rotatably connected to the hoisting mechanism;

[0030] One end of the second support beam is rotatably connected to the walking mechanism, and the other opposite end of the second support beam is rotatably connected to the hoisting mechanism.

[0031] In any of the above technical solutions, further, the walking mechanism includes a walking frame and four walking wheels rotatably connected to the walking frame, and any of the walking wheels is provided with a steering component;

[0032] One of the two groups of diagonally arranged walking wheels is provided with a power driving component.

[0033] Compared with the prior art, the beneficial effects of this application are:

[0034] This ground assembly vehicle transfers the installation process of missiles and missile launchers to the ground. The assembled launcher is directly installed inside the aircraft's ammunition bay, shortening the operation time of missile and launcher installation, reducing the difficulty of installation, and improving safety.

[0035] Moreover, the entire missile assembly process can be installed remotely with a high degree of automation, which improves the assembly efficiency of missiles and launchers and shortens the combat response time of troops. BRIEF DESCRIPTION OF THE DRAWINGS

[0036] In order to more clearly illustrate the specific implementation methods of the present application or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0037] Figure 1 A schematic diagram of the structure of the ground assembly vehicle and the magnetic levitation conductive rail provided in an embodiment of the present application;

[0038] Figure 2 A schematic diagram of the structure of the hoisting mechanism provided in the embodiment of the present application;

[0039] Figure 3 A schematic diagram of the structure of the auxiliary mechanism for assembling a bullet provided in an embodiment of the present application;

[0040] Figure 4 for Figure 3 A schematic diagram of the enlarged structure at A;

[0041] Figure 5 A schematic diagram of the structure of the walking mechanism provided in the embodiment of the present application;

[0042] Figure 6 This is another structural schematic diagram of the walking mechanism provided in an embodiment of the present application.

[0043] Reference numerals:

[0044] 1-hoisting mechanism, 11-horizontal position adjustment mechanism, 111-first supporting member, 112-second supporting member, 113-longitudinal drive assembly, 114-lateral drive assembly, 115-extension frame, 116-sliding pin, 12-first hoisting auxiliary mechanism, 121-support body, 122-hoisting arm, 123-first guide limiting member, 1231-first guide limiting part, 124-second guide limiting member, 13-second hoisting auxiliary mechanism, 131-fixed beam, 132-lifting ring, 133-clamping claw member, 14-lifting mechanism, 141-mounting seat, 142-guide wheel, 143-pulley, 144-rope, 145-hook, 15-rotation adjustment mechanism, 151-slewing drive device, 152-slewing seat;

[0045] 2-group spring auxiliary mechanism, 21-first mounting member, 22-second mounting member, 23-third mounting member, 24-bearing member, 25-clamping member, 251-clamping part, 252-shielding part, 253-connecting part, 254-lifting assembly, 2541-driving motor, 2542-screw elevator;

[0046] 3- walking mechanism, 31- walking frame, 32- walking wheel;

[0047] 4-lifting mechanism, 41-first support beam, 42-second support beam;

[0048] 5-Electrical control cabinet, 6-Power supply. DETAILED DESCRIPTION

[0049] The technical solution of the present application will be clearly and completely described below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all of the embodiments.

[0050] The components of the embodiments of the present application generally described and shown in the drawings herein can be arranged and designed in various different configurations. Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the application claimed, but merely represents the selected embodiments of the present application.

[0051] Based on the embodiments in this application, all other embodiments obtained by ordinary technicians in this field without making any creative work shall fall within the scope of protection of this application.

[0052] In the description of the present application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present application. In addition, the terms "first", "second", and "third" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance.

[0053] In the description of this application, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0054] Refer to the following Figures 1 to 6 A ground assembly vehicle according to some embodiments of the present application is described.

[0055] See also Figure 1 As shown, an embodiment of the present application provides a ground ammunition assembly vehicle, comprising: a walking mechanism 3 and a lifting mechanism 4, a hoisting mechanism 1 and an ammunition assembly auxiliary mechanism 2 arranged on the walking mechanism 3; wherein the walking mechanism 3 is used for omnidirectional movement on a working surface (omnidirectional movement means movement in any direction in a horizontal plane and free rotation);

[0056] The hoisting mechanism 1 is used for hoisting the missile launcher, and the hoisting mechanism 1 can be lifted and lowered relative to the walking mechanism 3 through the lifting mechanism 4; the missile assembly auxiliary mechanism 2 is used for installing the missile compatible with the missile launcher.

[0057] The working process of this ground assembly vehicle is as follows:

[0058] First, the local surface assembly vehicle is moved to an open installation space by using the walking mechanism 3, and then the missile is installed on the assembly auxiliary mechanism 2 by using the lifting mechanism 1, and then the missile launcher is lifted by the lifting mechanism 1, and then the lifting mechanism 4 is used to descend and the rotating adjustment mechanism 15 of the lifting mechanism 1 described below is used to rotate and adjust the spatial position of the missile launcher, and the missile launcher is assembled on the missile, thereby completing the assembly of the missile and the missile launcher. The assembled launcher is then transported to the interior of the aircraft ammunition bay by the walking mechanism 3 for assembly.

[0059] It can be seen that the local surface assembly vehicle transfers the installation process of missiles and missile launchers to the ground. The assembled launcher is directly installed into the aircraft's ammunition bay, shortening the operation time of missile and launcher installation. The installation operation is unobstructed by obstacles, reducing the difficulty of installation and increasing safety.

[0060] Moreover, the entire missile assembly process can be installed remotely with a high degree of automation, which improves the assembly efficiency of missiles and launchers and shortens the combat response time of troops.

[0061] In one embodiment of the present application, preferably, Figure 1 and Figure 2 As shown, the hoisting mechanism 1 includes a horizontal position adjustment mechanism 11, a first hoisting auxiliary mechanism 12, a second hoisting auxiliary mechanism 13, a lifting mechanism 14 and a rotation adjustment mechanism 15;

[0062] The first lifting auxiliary mechanism 12 and the second lifting auxiliary mechanism 13 can adjust the horizontal position relative to the walking mechanism 3 through the horizontal position adjustment mechanism 11; the second lifting auxiliary mechanism 13 can adjust the height position relative to the walking mechanism 3 through the lifting mechanism 14;

[0063] The second lifting auxiliary mechanism 13 is used to install the missile launcher, and the rotation adjustment mechanism 15 is used to adjust the angle between the missile launcher lifted on the second lifting auxiliary mechanism 13 and the horizontal direction.

[0064] In this embodiment, the missile is firstly lifted by the cooperation of the horizontal position adjustment mechanism 11 and the lifting mechanism 14 and installed on the missile assembly auxiliary mechanism 2;

[0065] Then, the missile launcher is installed on the second lifting auxiliary mechanism 13, and the second lifting auxiliary mechanism 13 is lifted to the first lifting mechanism 1 and the rotation adjustment mechanism 15 by the lifting mechanism 14, and the second lifting auxiliary mechanism 13 is assembled with the first lifting mechanism 1 and the rotation adjustment mechanism 15 respectively;

[0066] Then the rotation adjustment mechanism 15 adjusts the angle between the second lifting auxiliary mechanism 13 and the horizontal plane, that is, indirectly adjusts the angle of the missile launcher. When the preset assembly angle is reached, the adjustment is stopped, and then the missile launcher is adjusted to the preset horizontal position by the horizontal position adjustment mechanism 11. Finally, the missile launcher is moved down by the lifting mechanism 4, so that the missile launcher is assembled with the missile clamped on the missile assembly auxiliary mechanism 2. Note that the adjustment sequence of the angle and horizontal position of the missile launcher is not limited to the above, and can also be set according to actual needs, and the number of adjustments can also be set according to actual needs.

[0067] The above adjustment process can especially use remote control to adjust the spatial position of the missile launcher, which has a high degree of automation and saves time and effort. In addition, the missile launcher can be adjusted in three directions, X, Y, and Z, and the angle formed by the missile launcher and the horizontal direction can be adjusted, which realizes the precise adjustment of the position of the missile launcher and improves the assembly accuracy.

[0068] In one embodiment of the present application, preferably, Figure 1 and Figure 2 As shown, the horizontal position adjustment mechanism 11 includes a first support member 111, a second support member 112, a longitudinal drive assembly 113 and a transverse drive assembly 114; wherein the first support member 111 is rotatably connected to an end of the lifting mechanism 4 away from the walking mechanism 3;

[0069] The second support member 112 is provided with the first support member 111, and the second support member 112 can be moved along the longitudinal direction of the first support member 111 by a longitudinal drive assembly 113, and the second support member 112 can be moved along the transverse direction of the first support member 111 by a transverse drive assembly 114;

[0070] The first hoisting auxiliary mechanism 12 and the second hoisting auxiliary mechanism 13 are both disposed on the second supporting member 112 .

[0071] In this embodiment, the process of adjusting the horizontal position of the missile launcher using the above components is as follows (note that the adjustment sequence is not limited to the following and can also be set according to actual needs):

[0072] The longitudinal drive component 113 is used to drive the second support member 112 to be longitudinally adjusted along the first support member 111, that is, to adjust the position of the X-axis. The transverse drive component 114 is used to drive the second support member 112 to be transversely adjusted along the first support member 111, that is, to adjust the position of the Y-axis, thereby realizing the adjustment of the horizontal position of the first lifting auxiliary mechanism 12 and the second lifting auxiliary mechanism 13, and further indirectly realizing the adjustment of the position of the missile launcher installed on the first lifting auxiliary mechanism 12 and the second lifting auxiliary mechanism 13.

[0073] It can be seen that the above structure not only has an adjusting function during the assembly process of the missile launcher with the first hoisting auxiliary mechanism 12 and the second hoisting auxiliary mechanism 13, but also has a function of accurately adjusting the position during the assembly process of the missile launcher and the missile clamped on the missile assembly auxiliary mechanism 2 after the above assembly process is completed. It has a high degree of automation and stronger controllability.

[0074] Preferably, the second supporting member 112 is slidably connected to the first supporting member 111 via a guide rail.

[0075] Among them, preferably, the first supporting member 111 is a platform, the second supporting member 112 is a movable frame, the movable frame is connected to an extension frame 115 extending along the vertical direction, the extension frame 115 is provided with a slide groove, the first lifting auxiliary mechanism 12 is connected to a sliding pin 116, and the sliding pin 116 can be slidably inserted in this slide groove.

[0076] In one embodiment of the present application, preferably, Figure 1 and Figure 2 As shown, the first lifting auxiliary mechanism 12 includes a supporting body 121, a lifting arm 122, a first guide limiting member 123 and a second guide limiting member 124; wherein the lifting arm 122 is vertically connected to the supporting body 121; the supporting body 121 is formed with a mounting groove, and the lifting mechanism 14 is arranged in the mounting groove;

[0077] The first guide and limiting member 123 is connected to one end of the hanging arm 122, the rotation adjustment mechanism 15 is connected to the other end opposite to the hanging arm 122, and the second guide and limiting member 124 is connected to the rotation adjustment mechanism 15;

[0078] The first guide limiting member 123 is formed with a first guide limiting portion 1231 , and the second guide limiting member 124 is formed with a second guide limiting portion.

[0079] In this embodiment, the assembly process of the second lifting auxiliary mechanism 13 and the first lifting auxiliary mechanism 12 is as follows:

[0080] The lifting mechanism 14 is used to lift the second lifting auxiliary mechanism 13 to the first lifting mechanism 1 and the rotation adjustment mechanism 15. The first guide limit portion 1231 and the second guide limit portion of the second lifting auxiliary mechanism 13 respectively guide and position each other with the corresponding third guide limit portion and fourth guide limit portion of the first lifting auxiliary mechanism 12 described below. In addition, the lifting mechanism 14 maintains the lifting effect on the second lifting auxiliary mechanism 13, which improves the stability of the second lifting auxiliary mechanism 13, thereby realizing the assembly of the missile launcher.

[0081] In addition, the rotation adjustment mechanism 15 can also be used to adjust the angle of the second lifting auxiliary mechanism 13 together with the missile launcher installed on the second lifting auxiliary mechanism 13 to meet the preset installation angle.

[0082] Preferably, the first guide limiting portion 1231 is a trapezoidal groove opened on the first guide limiting member 123 and opening downward, and the second guide limiting portion is a trapezoidal groove opened on the second guide limiting member 124 and opening downward.

[0083] In one embodiment of the present application, preferably, Figure 1 and Figure 2As shown, the second lifting auxiliary mechanism 13 includes a fixed beam 131, a lifting ring 132 and a clamping claw member 133;

[0084] Among them, a third guide limit portion is formed at one end of the fixed beam 131 and is limited to the first guide limit portion 1231, and a fourth guide limit portion is formed at the other opposite end of the fixed beam 131 and is limited to the second guide limit portion, which plays a guiding and positioning role during the assembly of the second lifting auxiliary mechanism 13 and the first lifting auxiliary mechanism 12.

[0085] Preferably, the third guide limiting portion and the fourth guide limiting portion are both trapezoidal blocks adapted to the above-mentioned trapezoidal groove.

[0086] The clamping claw member 133 and the lifting ring 132 are both arranged on the fixed beam 131, wherein the clamping claw member 133 is used to clamp the missile launcher, and the lifting ring 132 is used to connect with the hook 145 of the lifting mechanism 14 described below.

[0087] In one embodiment of the present application, preferably, Figure 1 and Figure 2 As shown, the lifting mechanism 14 includes a mounting seat 141, a guide wheel 142, a pulley 143, a rope 144, a hook 145 and a first driving device; wherein the mounting seat 141, the guide wheel 142 and the pulley 143 are sequentially arranged on the second supporting member 112 along the length direction of the second supporting member 112;

[0088] The rope 144 is rotatably wound around the support shaft of the mounting seat 141, and one end of the rope 144 passes through the guide wheel 142 and passes around the pulley 143 to be connected to the hook 145;

[0089] The first driving device is connected to the supporting shaft and is used for driving the supporting shaft to rotate.

[0090] In this embodiment, the first driving device drives the support shaft to rotate, thereby releasing or retracting the rope 144, thereby lifting and lowering the second lifting auxiliary mechanism 13 connected to the hook 145. The guide wheel 142 and the pulley 143 both play a guiding role.

[0091] In one embodiment of the present application, preferably, Figure 3 and Figure 4 As shown, the assembly auxiliary mechanism 2 includes a first mounting member 21, a second mounting member 22, a third mounting member 23, a bearing member 24, a clamping member 25 and a lifting assembly 254;

[0092] Among them, the walking mechanism 3 forms an installation gap, the first installation component 21 is arranged in the gap, and the first installation component 21 is detachably connected to the walking mechanism 3, that is, the first installation component 21 is pushed into the above-mentioned gap along the side of the walking mechanism 3, thereby realizing the assembly of the walking mechanism 3 and the first installation component 21.

[0093] The second mounting member 22 is connected to the first mounting member 21, and the second mounting member 22 forms a mounting cavity, and the third mounting member 23 and the lifting assembly 254 are both disposed in the mounting cavity;

[0094] The third mounting member 23 is connected to the lifting assembly 254, and the third mounting member 23 is lifted and lowered relative to the second mounting member 22 by the lifting assembly 254;

[0095] The bearing member 24 is slidably connected to the third mounting member 23 , specifically, can be slidably connected via a slide rail, and the bearing member 24 can slide along a horizontal direction relative to the third mounting member 23 ; the clamping member 25 is disposed on the bearing member 24 .

[0096] In this embodiment, the lifting assembly 254 can drive the third mounting component 23 to rise or fall, and then indirectly drive the load-bearing component 24 to rise or fall, so as to adjust the height of the clamping component 25 installed on the load-bearing component 24, and then adjust the height of the missile clamped on the clamping component 25, so as to facilitate the later assembly with the missile launcher.

[0097] In addition, since the bearing member 24 is slidably connected to the third mounting member 23, the missile can also be fine-tuned in the horizontal direction to meet assembly requirements.

[0098] Preferably, there are multiple load-bearing members 24, and multiple load-bearing members 24 are sequentially arranged along the width direction of the walking mechanism 3; any load-bearing member 24 is provided with multiple clamping members 25. Based on the above structure, each load-bearing member 24 can be installed with 1 to 2 missiles, thereby realizing the assembly of a missile launcher with multiple missiles, and improving the assembly efficiency. It should be noted that multiple load-bearing members 24 can be used simultaneously or separately, depending on actual needs.

[0099] Moreover, any bearing member 24 is also provided with a positioning pin, and the third mounting member 23 is formed with a waist-shaped positioning hole. When the bearing member 24 is horizontally moved to a suitable position, the positioning pin can be installed to achieve the positioning of the bearing member 24. Of course, not limited to the above structure, a guide rail strong locking slider can also be set on the guide rail to limit the bearing member 24.

[0100] Among them, preferably, the lifting assembly 254 includes a connected drive motor 2541 and a screw elevator 2542, and the screw elevator 2542 is connected to the third mounting component 23. Of course, it is not limited to this. The lifting assembly 254 can also adopt a drive motor 2541, a bevel gear transmission assembly and a screw assembly connected in sequence, and the nut seat of the screw assembly is connected to the third mounting component 23.

[0101] In one embodiment of the present application, preferably, Figure 4 As shown, the clamping member 25 includes a clamping portion 251, a shielding portion 252 and a connecting portion 253 connected to each other;

[0102] The bearing member 24 is formed with an installation groove, the connecting portion 253 is inserted into the installation groove, the shielding portion 252 covers the opening of the installation groove, and the clamping portion 251 is located outside the installation groove; the connecting portion 253 is sleeved with an elastic member.

[0103] In this embodiment, the clamping portion 251 is used to clamp the missile, and the shielding portion 252 limits the elastic component, and the elastic component has a buffering effect on the missile.

[0104] Preferably, the clamping portion 251 is formed with a U-shaped clamping opening for clamping the missile.

[0105] In one embodiment of the present application, preferably, Figure 2 As shown, the rotation adjustment mechanism 15 includes a rotary drive device 151 and a rotary seat 152 connected to each other, and the first guide limiting component 123 is connected to the rotary seat 152 .

[0106] In one embodiment of the present application, preferably, Figure 1 As shown, the lifting mechanism 4 includes a second driving device, a screw transmission assembly, a first support beam 41 and a second support beam 42; wherein the first support beam 41 and the second support beam 42 are cross-rotatably connected;

[0107] One end of the first support beam 41 is slidably connected to the walking mechanism 3, and the second driving device drives the first support beam 41 to slide relative to the walking mechanism 3 through the screw transmission assembly, and the other opposite end of the first support beam 41 is rotatably connected to the hoisting mechanism 1;

[0108] One end of the second support beam 42 is rotatably connected to the walking mechanism 3 , and the other opposite end of the second support beam 42 is rotatably connected to the hoisting mechanism 1 .

[0109] In this embodiment, the second drive device drives the screw of the screw transmission assembly to rotate, and the rotation of the screw drives the nut seat to move along the screw, thereby driving one end of the first support beam 41 to slide relative to the walking mechanism 3, thereby forcing the first support beam 41 and the second support beam 42 to rotate, and at the same time realizing the lifting and lowering of the lifting mechanism 1 above the lifting mechanism 4.

[0110] In one embodiment of the present application, preferably, Figure 5 and Figure 6 As shown, the walking mechanism 3 includes a walking frame 31 and four walking wheels 32 rotatably connected to the walking frame 31, and each walking wheel 32 is provided with a steering member;

[0111] One of the two groups of diagonally arranged running wheels 32 is provided with a power driving member.

[0112] The above structure can realize the rotation in situ, lateral, longitudinal and oblique movement of the walking mechanism 3, which is conducive to the ground assembly vehicle to quickly avoid obstacles under the aircraft. Among them, the steering component and the power drive component are existing components of the vehicle and are not described in detail here.

[0113] Preferably, an electrical control cabinet 5 and a power supply 6 are provided in the traveling frame 31 .

[0114] In summary, the crane lifting mechanism 4 and the crane platform are adjusted, and the missiles are hoisted and fixed on the clamping member 25 on the bearing member 24 using the hook 145. Each bearing member 24 can be equipped with 1 to 2 missiles.

[0115] Then the missile launcher is installed on the second lifting auxiliary mechanism 13, and then the second lifting auxiliary mechanism 13 is hung on the lifting mechanism 14. The lifting mechanism 14 lifts the second lifting auxiliary mechanism 13 to the lifting arm 122 of the first lifting auxiliary mechanism 12, and the second lifting auxiliary mechanism 13 is respectively assembled with the first guide limit member 123 and the second guide limit member 124. The rotation adjustment mechanism 15 drives the second guide limit member 124 to rotate together with the second lifting auxiliary mechanism 13, thereby adjusting the angle of the missile launcher, and adjusting the height and horizontal position of the missile by using the missile assembly auxiliary mechanism 2, and finally descending by using the lifting mechanism 4, and installing the missile launcher on the missile.

[0116] It realizes the assembly of a launcher and multiple missiles quickly and efficiently, and has a position and angle adjustment mechanism, so it can meet the mounting requirements of missiles and missile launchers of different specifications, comprehensively improve the assembly efficiency of missiles and launchers, and shorten the combat response time of the troops.

[0117] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present application, rather than to limit it. Although the present application has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or replace some or all of the technical features therein with equivalents. However, these modifications or replacements do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of the present application.

Claims

1. A ground-based ammunition assembly vehicle, characterized in that: include: A walking mechanism and a lifting mechanism, a hoisting mechanism and an assembling auxiliary mechanism arranged on the walking mechanism; wherein the walking mechanism is used for omnidirectional movement on the working surface; The hoisting mechanism is used to hoist the missile launcher, and the hoisting mechanism can be lifted and lowered relative to the walking mechanism through the lifting mechanism; the missile assembly auxiliary mechanism is used to install the missile compatible with the missile launcher; The hoisting mechanism includes a horizontal position adjustment mechanism, a first hoisting auxiliary mechanism, a second hoisting auxiliary mechanism, a lifting mechanism and a rotation adjustment mechanism; Wherein, the first lifting auxiliary mechanism and the second lifting auxiliary mechanism can adjust the horizontal position relative to the walking mechanism through the horizontal position adjustment mechanism; the second lifting auxiliary mechanism can adjust the height position relative to the walking mechanism through the lifting mechanism; The second lifting auxiliary mechanism is used to install the missile launcher, and the rotation adjustment mechanism is used to adjust the angle between the missile launcher lifted on the second lifting auxiliary mechanism and the horizontal direction.

2. The ground assembly vehicle according to claim 1, characterized in that: The horizontal position adjustment mechanism comprises a first supporting member, a second supporting member, a longitudinal driving assembly and a transverse driving assembly; wherein the first supporting member is rotatably connected to an end of the lifting mechanism away from the walking mechanism; The second supporting member is provided with the first supporting member, and the second supporting member can be moved in the longitudinal direction of the first supporting member by the longitudinal driving assembly, and the second supporting member can be moved in the transverse direction of the first supporting member by the transverse driving assembly; The first hoisting auxiliary mechanism and the second hoisting auxiliary mechanism are both arranged on the second supporting member.

3. The ground assembly vehicle according to claim 1, characterized in that: The first lifting auxiliary mechanism includes a supporting body, a lifting arm, a first guide limiting member and a second guide limiting member; wherein the lifting arm is vertically connected to the supporting body; the supporting body is formed with a mounting groove, and the lifting mechanism is arranged in the mounting groove; The first guide and limit member is connected to one end of the hanging arm, the rotation adjustment mechanism is connected to the other end opposite to the hanging arm, and the second guide and limit member is connected to the rotation adjustment mechanism; The first guide and limiting member is formed with a first guide and limiting portion, and the second guide and limiting member is formed with a second guide and limiting portion.

4. The ground assembly vehicle according to claim 3, characterized in that: The second lifting auxiliary mechanism includes a fixed beam, a lifting ring and a clamping claw member; Wherein, a third guide limit portion which is mutually limited with the first guide limit portion is formed at one end of the fixed beam, and a fourth guide limit portion which is mutually limited with the second guide limit portion is formed at the other opposite end of the fixed beam; The clamping claw member and the lifting ring are both arranged on the fixed beam.

5. The ground assembly vehicle according to claim 2, characterized in that: The lifting mechanism comprises a mounting seat, a guide wheel, a pulley, a rope, a hook and a first driving device; wherein the mounting seat, the guide wheel and the pulley are sequentially arranged on the second supporting member along the length direction of the second supporting member; The rope is rotatably wound around the support shaft of the mounting seat, and one end of the rope passes through the guide wheel and bypasses the pulley to be connected to the hook; The first driving device is connected to the supporting shaft and is used for driving the supporting shaft to rotate.

6. The ground assembly vehicle according to claim 1, characterized in that: The assembly auxiliary mechanism includes a first mounting member, a second mounting member, a third mounting member, a bearing member, a clamping member and a lifting assembly; The walking mechanism is formed with a mounting notch, the first mounting member is arranged in the notch, and the first mounting member is detachably connected to the walking mechanism; the second mounting member is connected to the first mounting member, and the second mounting member is formed with a mounting cavity, the third mounting member and the lifting assembly are both arranged in the mounting cavity; the third mounting member is connected to the lifting assembly, and the third mounting member is lifted and lowered relative to the second mounting member through the lifting assembly; The bearing member is slidably connected to the third mounting member, and the bearing member can slide along a horizontal direction relative to the third mounting member; the clamping member is arranged on the bearing member.

7. The ground assembly vehicle according to claim 6, characterized in that: There are multiple load-bearing members, and the multiple load-bearing members are arranged in sequence along the width direction of the walking mechanism; any load-bearing member is provided with multiple clamping members; and / or The clamping member comprises a clamping portion, a shielding portion and a connecting portion connected to each other; The bearing component is formed with a mounting groove, the connecting portion is inserted into the mounting groove, the shielding portion covers the opening of the mounting groove, and the clamping portion is located outside the mounting groove; the connecting portion is sleeved with an elastic component.

8. The ground assembly vehicle according to claim 1, characterized in that: The lifting mechanism comprises a second driving device, a screw transmission assembly, a first support beam and a second support beam; wherein the first support beam is cross-rotatably connected with the second support beam; One end of the first support beam is slidably connected to the walking mechanism, the second driving device drives the first support beam to slide relative to the walking mechanism through the screw transmission assembly, and the other opposite end of the first support beam is rotatably connected to the hoisting mechanism; One end of the second support beam is rotatably connected to the walking mechanism, and the other opposite end of the second support beam is rotatably connected to the hoisting mechanism.

9. The ground assembly vehicle according to claim 1, characterized in that: The walking mechanism comprises a walking frame and four walking wheels rotatably connected to the walking frame, and any of the walking wheels is provided with a steering component; One of the two groups of diagonally arranged walking wheels is provided with a power driving component.

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