Modular airborne reconnaissance and strike micro rocket launcher

Abstract

The application provides a modular airborne detection and attack micro-rocket launching device, which comprises a weapon station module, a shell cabin module and a female head, a male head and a transmission module are respectively electrically connected to two ends of an electric control module and are controlled by the electric control module; a rotating shaft rotates along an axis; the shell cabin module is detachably connected to the rotating shaft and rotates with the rotating shaft; a shell cabin body is used for accommodating spare bullets; the female head is detachably connected to the male head, at this time, the weapon station module, the female head and the shell cabin module are in a non-integral structure, and the weapon station module, the female head and the shell cabin module can be separately disassembled, so that the modules of the modular airborne detection and attack micro-rocket launching device cannot be separately maintained, the maintenance convenience of the modules of the modular airborne detection and attack micro-rocket launching device is improved, in addition, the shell cabin module is detachably connected to the rotating shaft and rotates with the rotating shaft, so that the angle of the shell cabin module relative to the transmission module can be adjusted.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of weapon stations, and particularly relates to a modular airborne detection and attack micro-rocket launcher. BACKGROUND

[0002] With the development of science and technology, weapon stations are used for suppressing or destroying targets, at which time, a UAV can be connected with an airborne detection and attack micro-rocket launcher, and the airborne detection and attack micro-rocket launcher is below the UAV. In the prior art, the airborne detection and attack micro-rocket launcher comprises a weapon station module, a mother head and a shell cabin module. The mother head is connected to the bottom of the UAV, the mother head is connected to the upper end of the weapon station module, and the shell cabin module is connected to the weapon station module. In order to improve the overall stability of the modular airborne detection and attack micro-rocket launcher, the weapon station module, the mother head and the shell cabin module are integrated, and the weapon station module, the mother head and the shell cabin module cannot be disassembled, so that the modules of the existing modular airborne detection and attack micro-rocket launcher cannot be repaired individually. SUMMARY

[0003] The present application relates to the technical field of weapon stations, and particularly relates to a modular airborne detection and attack micro-rocket launcher.

[0004] To achieve the above object, the present application provides the following technical scheme.

[0005] A modular airborne detection and attack micro-rocket launcher comprises:

[0006] A weapon station module comprises a male head, a transmission module and an electric control module. The male head and the transmission module are respectively electrically connected to two ends of the electric control module and are controlled by the electric control module. The transmission module is provided with a rotating shaft which rotates along its axis.

[0007] A shell cabin module is arranged on one side of the weapon station module and is detachably connected to the rotating shaft and rotates with the rotating shaft. The shell cabin module is provided with a shell cabin body which is used for accommodating spare bullets.

[0008] A mother head is arranged on the upper side of the weapon station body and is detachably connected to the male head. The upper end of the mother head is used for connecting the lower end of the UAV.

[0009] Optionally, the transmission module comprises a frame, a driving wheel, a driven wheel and a motor, the motor is connected to the frame, the rotating shaft is rotatably arranged in the frame, the driven wheel is connected to the rotating shaft, the driving wheel is engaged with the driven wheel, the driving wheel is connected to the motor, the driven wheel rotates with the driving wheel driven by the motor, and the driven wheel drives the ammunition module connected to the rotating shaft to rotate.

[0010] Optionally, the ammunition module comprises a shell, one side of the shell is provided with a positioning shaft, the rotating shaft is provided with a positioning groove, the positioning shaft is arranged relative to the positioning groove and enters the rotating shaft along the inner side wall of the positioning groove.

[0011] Optionally, the ammunition module further comprises a handle, the handle is arranged on one side of the shell for the operator's hand to hold; the handle is swingably connected to the shell, one side of the handle is provided with a lock catch, the lock catch is located outside the positioning shaft and can be locked or unlocked to the rotating shaft.

[0012] Optionally, the lock catch is provided with a first boss, the rotating shaft is provided with a second boss, the first boss is arranged at the rear side of the second boss, the first boss and the second boss are superimposed in the left-right direction to limit the first boss from separating from the second boss in the left-right direction;

[0013] Or, when the first boss and the second boss are staggered in the swinging direction of the handle, the lock catch is unlocked to the rotating shaft.

[0014] Optionally, the lock catch is provided with a circular arc hole, a screw is arranged between the shell and the lock catch, the threaded end of the screw is connected to the shell and penetrates the circular arc hole, so that the handle is swingably connected to the shell.

[0015] Optionally, the nut end of the screw is located outside the circular arc hole and abuts against the outer surface of the lock catch.

[0016] Optionally, the upper end of the male head is provided with a positioning boss, the lower end of the female head is provided with a positioning groove, the positioning groove is inserted into the positioning boss, and the positioning boss and the positioning groove have a guiding effect.

[0017] Optionally, a lock catch assembly is arranged between the male head and the female head, the lock catch assembly comprises a lock catch body and a fixing piece, the lock catch body and the fixing piece are respectively installed on the male head and the female head, and the lock catch body clamps the fixing piece to fixedly connect the male head and the female head.

[0018] Optionally, the lower end of the female head is attached to the upper end of the male head and detachably connected to the male head through the lock buckle assembly.

[0019] Compared with the prior art, the application has the following beneficial effects:

[0020] The application provides a modular airborne detection and attack micro-rocket projectile launching device, a weapon station module includes a male head, a transmission module and an electric control module, the male head and the transmission module are respectively electrically connected to two ends of the electric control module and controlled by the electric control module, the transmission module is provided with a rotating shaft, the rotating shaft rotates along its axis, a projectile cabin module is arranged on one side of a weapon station body and detachably connected to the rotating shaft and rotates with the rotating shaft, the projectile cabin module is provided with a projectile cabin body for accommodating spare projectiles, the upper end of the female head is used for connecting the lower end of an unmanned aerial vehicle, the female head is arranged on the upper side of the weapon station body and detachably connected to the male head, at this time, the weapon station module, the female head and the projectile cabin module are in a non-integral structure, and the weapon station module, the female head and the projectile cabin module can be separately disassembled, so that the modules of the modular airborne detection and attack micro-rocket projectile launching device cannot be separately maintained, the maintenance convenience of the modules of the modular airborne detection and attack micro-rocket projectile launching device is improved, in addition, the projectile cabin module is detachably connected to the rotating shaft and rotates with the rotating shaft, so as to adjust the angle of the projectile cabin module relative to the transmission module, thereby facilitating the adjustment of the projectile cabin module at various angles and adapting to work at different angles. BRIEF DESCRIPTION OF DRAWINGS

[0021] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiment description. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can also be obtained by those skilled in the art without creative labor.

[0022] In order to more completely understand the present application and its beneficial effects, the following will be described with reference to the drawings. In the following description, the same reference numerals represent the same parts.

[0023] Fig. 1 The present application provides a modular airborne detection and attack micro-rocket projectile launching device.

[0024] Fig. 2 The present application provides a modular airborne detection and attack micro-rocket projectile launching device.

[0025] Fig. 3 The present application provides a modular airborne detection and attack micro-rocket projectile launching device.

[0026] Fig. 4 The present application provides a modular airborne detection and attack micro-rocket projectile launching device. Fig. 3A local enlarged view of the middle A.

[0027] Fig. 5 An unlocking state diagram of the locking buckle of the modular airborne reconnaissance and strike micro-rocket projectile launching device is provided for the embodiment of the present application.

[0028] Fig. 6 A side view of the locking buckle of the modular airborne reconnaissance and strike micro-rocket projectile launching device is provided for the embodiment of the present application. DETAILED DESCRIPTION

[0029] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the present application.

[0030] Please refer to the drawings Figs. 1-6 The embodiment of the present application provides a modular airborne reconnaissance and strike micro-rocket projectile launching device 100, which is used for suppressing or destroying targets. The modular airborne reconnaissance and strike micro-rocket projectile launching device 100 comprises a weapon station module 10, a projectile cabin module 20 and a parent head 30. The projectile cabin module 20 and the parent head 30 are arranged on one side of the weapon station module 10.

[0031] The weapon station module 10 comprises a male head 11, a transmission module 12 and an electric control module 13. The male head 11 and the transmission module 12 are respectively electrically connected to two ends of the electric control module 13 and are controlled by the electric control module 13. The transmission module 12 is provided with a rotating shaft 121 which rotates along its axis.

[0032] At this time, the male head 11 and the transmission module 12 are respectively electrically connected to two ends of the electric control module 13. The male head 11 is relative to the upper end of the electric control module 13, and the transmission module 12 is relative to the lower end of the electric control module 13. The male head 11 and the transmission module 12 are controlled by the electric control module 13. The rotating shaft 121 rotates along its axis so as to drive the projectile cabin module 20 to rotate. The electric control module 13 can be a circuit board of an integrated control circuit or an electric control cabinet, which can be adjusted according to actual application scenarios. The electric control module 13 is electrically connected to the male head 11 and the transmission module 12 and controls the communication of the male head 11 and the transmission module 12, so as to facilitate the transmission and feedback of working signals.

[0033] The transmission module 12 comprises a frame 122, a driving wheel 124, a driven wheel 123 and a motor 125, the motor 125 is connected to the frame 122, the rotating shaft 121 is rotatably arranged through the frame 122, the driven wheel 123 is connected to the rotating shaft 121, the driving wheel 124 is engaged with the driven wheel 123, the driving wheel 124 is connected to the motor 125, the driven wheel 123 rotates with the rotation of the driving wheel 124 driven by the motor 125, and the ammunition module 20 connected to the rotating shaft 121 rotates.

[0034] At this time, the rotating shaft 121 rotates under the drive of the motor 125, the rotating shaft 121 rotates along its axis, and drives the ammunition module 20 connected to the rotating shaft 121 to rotate, so as to adjust the position of the ammunition module 20 relative to the transmission module 12, and the multiple positions are adjusted by the ammunition module 20.

[0035] The ammunition module 20 is arranged on one side of the weapon station module 10 and is detachably connected to the rotating shaft 121 and rotates with the rotating shaft 121.

[0036] At this time, the ammunition module 20 has two, two ammunition modules 20 are arranged on one side of the weapon station module 10, two ammunition modules 20 are arranged opposite to each other and are detachably connected to the rotating shaft 121 and rotate with the rotating shaft 121, so as to adjust the position of the two ammunition modules 20 relative to the rotating shaft 121, the ammunition module 20 is provided with an ammunition body 21 for accommodating spare bullets, and the multiple positions are adjusted by the two ammunition modules 20.

[0037] The ammunition module 20 comprises an outer shell 22, one side of the outer shell 22 is provided with a positioning shaft 221, the rotating shaft 121 is provided with a positioning groove 121a, the positioning shaft 221 is arranged relative to the positioning groove 121a and enters the rotating shaft 121 along the inner side wall of the positioning groove 121a.

[0038] At this time, the positioning shaft 221 is positioned and connected with the rotating shaft 121, the positioning shaft 221 is arranged opposite to the positioning groove 121a, the positioning shaft 221 is inserted into the positioning groove 121a and enters the rotating shaft 121 along the inner side wall of the positioning groove 121a, so as to connect the outer shell 22 to the transmission module 12 of the weapon station module 10.

[0039] The rotating shaft 121 is provided with a limiting groove 121b, the limiting groove 121b is communicated with the positioning groove 210a; the peripheral wall of the positioning shaft 221 is provided with a limiting boss 2211, the limiting boss 2211 is inserted into the limiting groove 121b, so that the positioning shaft 12 rotates with the rotating shaft 121.

[0040] At this time, the limiting groove 121b is located at one end of the rotating shaft 121, the limiting groove 121b is in communication with the positioning groove 210a, the circumferential side wall of the positioning shaft 12 is provided with a limiting boss 2211, the limiting boss 2211 is inserted into the limiting groove 121b, the limiting boss 2211 and the limiting groove 121b have a guiding effect, so that the positioning shaft 12 rotates with the rotating shaft 121, so as to drive the ammunition compartment module 20 to rotate by the transmission mechanism 210. Optionally, the limiting groove 121b has a plurality of limiting grooves 121b, and the plurality of limiting grooves 121b are arranged in a square along the circumference of the rotating shaft 213.

[0041] Optionally, the ammunition compartment body 21 has a plurality of rows of bullet grooves 21a, and the plurality of rows of bullet grooves 21a are arranged in a length direction of the ammunition compartment body 21. The bullet groove 21a is used for accommodating the spare bullet. By arranging the plurality of rows of bullet grooves 21a, the number of spare bullets can be increased.

[0042] The ammunition compartment module 20 further comprises a handle 23 arranged on one side of the shell 22 and used for holding by the hand of an operator. The handle 23 is swingably connected to the shell 22. One side of the handle 23 is provided with a lock catch 231 located outside the positioning shaft 221 and capable of being locked or unlocked to the rotating shaft 121.

[0043] The handle 23 is swung under the holding of the hand of the operator. At this time, the handle 23 swings relative to the shell 22 under the action of an external force. At the same time, the lock catch 231 is locked or unlocked to the rotating shaft 121 under the swinging of the handle 23. The ammunition compartment body 21 is separated from the rotating shaft 121 and maintained in the hand of the operator through the handle 23. The hands of the operator are prevented from clamping the surface of the shell 22. The ammunition compartment module 20 is prevented from falling to the ground during the installation process of the ammunition compartment module 20. Thus, the ammunition compartment module 20 is prevented from being easily damaged during the replacement process.

[0044] The lock catch 231 is provided with a first boss 2311, and the rotating shaft 121 is provided with a second boss 1211. The first boss 2311 is arranged at the rear side of the second boss 1211. The first boss 2311 and the second boss 1211 are superimposed in the left-right direction to limit the first boss 2311 from separating from the second boss 1211 in the left-right direction. Alternatively, when the first boss 2311 and the second boss 1211 are staggered in the swinging direction of the handle 23, the lock catch 231 is unlocked to the rotating shaft 121.

[0045] At this time, the first boss 2311 is arranged at the rear side of the second boss 1211. The first boss 2311 and the second boss 1211 are superimposed in the left-right direction. The left end of the first boss 2311 is in contact with the right end of the second boss 1211. The first boss 2311 cannot move outward to limit the first boss 2311 from separating from the second boss 1211 in the left-right direction. Thus, the lock catch 231 is locked to the rotating shaft 121.

[0046] When the first protrusion 2311 and the second protrusion 1211 are staggered along the swing direction of the handle 23, the first protrusion 2311 can move outward, so that the lock catch 231 is unlocked from the rotating shaft 121 and maintained on the operator's hand through the handle 23, avoiding the operator's two hands clamping the surface of the shell 22, preventing falling to the ground during the installation process of the ammunition compartment module 20, thereby avoiding the ammunition compartment module 20 being easily damaged during replacement.

[0047] Optionally, the first protrusion 2311 has a plurality of first protrusions 2311 arranged along the circumference of the lock catch 231, and the fixing effect between the lock catch 231 and the rotating shaft 121 is increased by arranging a plurality of first protrusions 2311.

[0048] The lock catch 231 is provided with a circular arc hole 231a, and the shell 22 and the lock catch 231 are provided with a screw 222, the shank end of the screw 222 is connected to the shell 22 and penetrates the circular arc hole 231a, so that the handle 23 is swingably connected to the shell 22.

[0049] At this time, the shank end of the screw 222 is connected to the shell 22 and penetrates the circular arc hole 231a, and the lock catch 231 swings along the axis direction of the circular arc hole 231a under the action of an external force, so as to adjust the position of the lock catch 231 relative to the transmission module 12, thereby adjusting the position of the first protrusion 2311 relative to the second protrusion 1211. When the handle 23 is inclined at 45° relative to the shell 22, the first protrusion 2311 is staggered with the second protrusion 1211, so that the lock catch 231 is unlocked from the transmission shaft. When the handle 23 is at 90° relative to the shell 22, the first protrusion 2311 coincides with the second protrusion 1211, so that the lock catch 231 is locked on the transmission shaft.

[0050] The nut end of the screw 222 is outside the circular arc hole 231a and abuts against the outer surface of the lock catch 231.

[0051] At this time, the shank end of the screw 222 penetrates the circular arc hole 231a, and the handle 23 swings along the axis direction of the circular arc hole 231a under the action of an external force, so as to swing the position of the handle 23 relative to the transmission module 12. In addition, the nut end of the screw 222 abuts against the outer surface of the lock catch 231, so as to limit the lock catch 231 from being separated from the shell 22, thereby ensuring the connection stability between the lock catch 231 and the shell 22. Optionally, the circular arc hole 231a has a plurality of circular arc holes 231a arranged along the circumference of the lock catch 231.

[0052] The surface of the lock catch 231 facing the shell 22 is provided with a spherical groove 231b, and the lock catch 231 and the shell 22 are provided with a pull bead 2312, which is embedded in the spherical groove 231b and rolls relative to the lock catch 231 and the shell 22 in the spherical groove 231b.

[0053] At this time, the outer contour of the pull bead 2312 is matched with the inner contour of the spherical groove 231b, one end of the pull bead 2312 is embedded in the spherical groove 231b, and the other end of the pull bead 2312 rolls in the spherical groove 231b relative to the lock catch 231 and the shell 22, so as to make the lock catch 231 rotate more smoothly relative to the shell 22.

[0054] The upper end of the female head 30 is used for connecting the lower end of the unmanned aerial vehicle, at this time, the upper end of the female head 30 is provided with a threaded hole 30a, and a bolt is screwed in the threaded hole 30a, so as to be screwed in the female head 30, thereby realizing the fixed connection of the bolt and the female head 30, and fixing the unmanned aerial vehicle.

[0055] The female head 30 is arranged on the upper side of the weapon station module 10 and is detachably connected to the male head 11, the upper end of the male head 11 is provided with a positioning boss 111, and the lower end of the female head 30 is provided with a positioning groove 30b which is inserted into the positioning boss 111, and the positioning boss 111 and the positioning groove 30b have a guiding effect.

[0056] At this time, when the female head 30 is connected to the male head 11, the positioning groove 121a moves towards the positioning boss 111, the positioning boss 111 is inserted into the positioning groove 121a, the male head 11 is built-in with a second connecting end 112, the female head 30 is built-in with a first connecting end 31, the first connecting end 31 is arranged relative to the second connecting end 112, the first connecting end 31 and the second connecting end 112 are connected, so that the first connecting end 31 is connected to the second connecting end 112 under the guidance of the positioning groove 121a, avoiding the misaligned contact of the first connecting end 31 and the second connecting end 112, thereby avoiding the damage of the first connecting end 31 and the second connecting end 112 in the connection process, and further improving the service life of the weapon station module 10.

[0057] The positioning boss 111 and the positioning groove 121a are arranged oppositely, and the outer contour of the positioning boss 111 is matched with the inner contour of the positioning groove 121a.

[0058] At this time, the positioning boss 111 is arranged below the positioning groove 121a, the positioning boss 111 and the positioning groove 121a are arranged oppositely, the outer contour of the positioning boss 111 is matched with the inner contour of the positioning groove 121a, and the positioning boss 111 and the positioning groove 121a have a positioning and guiding effect, so as to insert the positioning boss 111 into the positioning groove 121a, and make the male head 11 and the female head 30 fit and assemble, and optionally, the positioning boss 111 and the positioning groove 121a are gap-fitted, and optionally, the positioning groove 121a is trumpet-shaped, wherein the positioning groove 121a is gradually widened from top to bottom.

[0059] The first connecting end 31 is plugged into the second connecting end 112 and is electrically connected with the second connecting end 112, at this time, the first connecting end 31 is arranged opposite to the second connecting end 112, the second connecting end 112 is electrically connected with the unmanned aerial vehicle, and the first connecting end 31 is electrically connected with the second connecting end 112, so as to electrically communicate the first connecting end 31 with the unmanned aerial vehicle.

[0060] The lock catch assembly 113 is arranged between the male head 11 and the female head 30, the lock catch assembly 113 comprises a lock catch body 1131, a push piece 1132 and a fixing piece 1133, the lock catch body 1131 and the fixing piece 1133 are respectively installed on the male head 11 and the female head 30, the lock catch body 1131 is buckled with the fixing piece 1133, and the lock catch body 1131 is connected with the push piece 1132, so that the male head 11 and the female head 30 are fixedly connected.

[0061] At this time, the lock catch assembly 113 is used for buckling the male head 11 and the female head 30, the lock catch body 1131 and the fixing piece 1133 are respectively installed on the male head 11 and the female head 30, the lock catch body 1131 swings to the upper side of the fixing piece 1133 under the action of an external force, the push piece 1132 is pushed downward under the action of the external force, the lock catch body 1131 is buckled with the fixing piece 1133, so that the male head 11 and the female head 30 are in fixed connection.

[0062] In addition, the push piece 1132 is pushed upward under the action of an external force, so that the lock catch 231 is separated from the fixing piece 1133, so that the male head 11 and the female head 30 are in a disengaged state, so as to facilitate the debugging or maintenance of the weapon station module 10.

[0063] The lower end of the female head 30 is attached to the upper end of the male head 11 and is detachably connected with the male head 11 through the lock catch assembly 113, avoiding that the female head 30 is fixed with the male head 11 through screws, and improving the disassembly efficiency of the female head 30 and the male head 11.

[0064] Specifically, the lock catch body 1131 is connected to the outer side wall of the male head 11 and is detachably buckled with the fixing piece 1133 connected with the female head 30, the lock catch body 1131 is arranged opposite to the female head 30, and optionally, the lock catch assembly 113 has a plurality of lock catch assemblies 113, the plurality of lock catch assemblies 113 are arranged along the circumferential direction of the female head 30, the fixing area between the female head 30 and the male head 11 is increased by arranging the plurality of lock catch assemblies 113, and the fixing effect between the female head 30 and the male head 11 is improved.

[0065] Compared with the prior art, the beneficial effects of the present application are:

[0066] The application provides a modular airborne detection and shooting micro-rocket launcher 100, a weapon station module 10 includes a male head 11, a transmission module 12 and an electric control module 13, the male head 11 and the transmission module 12 are respectively electrically connected to two ends of the electric control module 13 and are controlled by the electric control module 13, the transmission module 12 is provided with a rotating shaft 121, the rotating shaft 121 rotates along the axis, a shell cabin module 20 is arranged on one side of the weapon station module and is detachably connected to the rotating shaft 121 and rotates with the rotating shaft 121, the shell cabin module 20 is provided with a shell cabin main body 21, the shell cabin main body 21 is used for accommodating a spare bullet, a female head 30 is used for connecting the lower end of the unmanned aerial vehicle, the female head 30 is arranged on the upper side of the weapon station module and is detachably connected to the male head 11, at this time, the weapon station module 10, the female head 30 and the shell cabin module 20 are non-integral structures, the weapon station module 10, the female head 30 and the shell cabin module 20 can be separately disassembled, so that the modules of the modular airborne detection and shooting micro-rocket launcher 100 cannot be separately maintained, the maintenance convenience of the modules of the modular airborne detection and shooting micro-rocket launcher 100 is improved, in addition, the shell cabin module 20 is detachably connected to the rotating shaft 121 and rotates with the rotating shaft 121, so that the angle of the shell cabin module 20 relative to the transmission module 12 can be adjusted, thereby the adjustment of the shell cabin module 20 at various angles is facilitated, and the work at different angles is adapted.

[0067] In the above embodiments, the description of each embodiment has its own focus, and the parts not described in detail in a certain embodiment can be referred to the related description of other embodiments.

[0068] In the description of the present application, the terms "first", "second" are only for the purpose of description, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of indicated technical features. Therefore, the features defined as "first", "second" can explicitly or implicitly include one or more features.

[0069] The principles and implementation modes of the present application are described by using specific examples in the present application, and the above embodiment descriptions are only used to help understand the method and its core idea of the present application; meanwhile, according to the idea of the present application, the specific implementation modes and application ranges will be changed by those skilled in the art, and in summary, the content of the specification should not be understood as the limitation of the present application.

Claims

1. A modular airborne reconnaissance and strike miniature rocket launching device, characterized in that, include: The weapon station module includes a male connector, a transmission module, and an electronic control module. The male connector is electrically connected to both ends of the electronic control module and controlled by the electronic control module. The transmission module is provided with a rotating shaft, which rotates along its axis. The ammunition compartment module is located on one side of the weapon station module and is detachably connected to the rotating shaft, and rotates with the rotation of the rotating shaft; the ammunition compartment module has an ammunition compartment body, which is used to hold spare ammunition; The female connector, the upper end of which is used to connect to the lower end of the UAV, is located on the upper side of the weapon station body and is detachably connected to the male connector; The bomb bay module includes an outer shell and a handle. A positioning shaft protrudes from one side of the outer shell, and a positioning groove is provided on the rotating shaft. The positioning shaft is arranged relative to the positioning groove and enters the rotating shaft along the inner wall of the positioning groove. The handle is located on one side of the housing for the operator's hand to grip; the handle is swayably connected to the housing, and a latch is provided on one side of the handle. The latch is located outside the positioning shaft and can be locked or unlocked to the rotating shaft. The latch is provided with a first protrusion, and the rotating shaft is provided with a second protrusion. The first protrusion is located on the rear side of the second protrusion. The first protrusion and the second protrusion overlap in the left-right direction to restrict the first protrusion from disengaging from the second protrusion in the left-right direction. Alternatively, when the first boss and the second boss are offset along the swing direction of the handle, the latch is unlocked from the rotating shaft; The latch has an arc-shaped hole, and a screw is provided between the outer shell and the latch. The stud end of the screw is connected to the outer shell and passes through the arc-shaped hole, so that the handle is swayably connected to the outer shell. The nut end of the screw is located outside the arc hole and abuts against the outer surface of the latch.

2. The modular airborne detect and engage micro-rocket projectile launcher of claim 1, wherein, The transmission module includes a frame, a drive wheel, a driven wheel, and a motor. The motor is connected to the frame, and the rotating shaft rotatably passes through the frame. The driven wheel is connected to the rotating shaft, and the drive wheel meshes with the driven wheel. The drive wheel is connected to the motor, and the driven wheel rotates as the motor drives the drive wheel to rotate, thereby driving the bomb bay module connected to the rotating shaft to rotate.

3. The modular airborne detect and engage micro-rocket projectile launcher of claim 1, wherein, The male head has a positioning boss protruding from its upper end, and the female head has a positioning groove at its lower end. The positioning groove is inserted into the positioning boss, and the positioning boss and the positioning groove have a guiding function.

4. The modular airborne detect and engage micro-rocket projectile launcher of claim 3, wherein, A locking assembly is provided between the male connector and the female connector. The locking assembly includes a locking body and a fixing member. The locking body and the fixing member are respectively installed on the male connector and the female connector. The locking body fastens the fixing member to fix the male connector and the female connector in place.

5. The modular airborne detect and engage micro-rocket projectile launcher of claim 4, wherein, The lower end of the female connector fits against the upper end of the male connector and is detachably connected to the male connector via a locking assembly.

Images