CN218937179U - Quick bullet-withdrawing shell structure for bird expelling - Google Patents

Quick bullet-withdrawing shell structure for bird expelling Download PDF

Info

Publication number
CN218937179U
CN218937179U CN202223402019.8U CN202223402019U CN218937179U CN 218937179 U CN218937179 U CN 218937179U CN 202223402019 U CN202223402019 U CN 202223402019U CN 218937179 U CN218937179 U CN 218937179U
Authority
CN
China
Prior art keywords
bullet
barrel
locking
unlocking
seat
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202223402019.8U
Other languages
Chinese (zh)
Inventor
骆祖元
张小军
莫建栋
王特
赵鑫
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang Xinhua Machinery Manufacturing Co ltd
Original Assignee
Zhejiang Xinhua Machinery Manufacturing Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhejiang Xinhua Machinery Manufacturing Co ltd filed Critical Zhejiang Xinhua Machinery Manufacturing Co ltd
Priority to CN202223402019.8U priority Critical patent/CN218937179U/en
Application granted granted Critical
Publication of CN218937179U publication Critical patent/CN218937179U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Catching Or Destruction (AREA)

Abstract

The utility model relates to the technical field of bullet-withdrawing structures, and discloses a rapid bullet-withdrawing structure for driving birds, which comprises a transmitting assembly, a transmission base assembly and an electric appliance control assembly, wherein the transmitting assembly and the transmission base assembly are movably arranged, and the electric appliance control assembly is arranged in the transmission base assembly. When the firing assembly is in the loading position, the open-close locking column is pulled out, the open-close locking hook is pulled open, the firing plate component is opened, the bullet withdrawing device is pulled open, and the bird-repellent shell or the bird-repellent bullet is taken out, so that the shell or the bullet is withdrawn. When loading, loading and driving the bird bullet, cover the launching plate part, close the switching latch hook, insert and open the locking post, accomplish the loading, the structure has intensity height, the loading is returned the bullet convenient, safe and reliable's advantage, this drives bird emitter and adopts flip back dress formula, barrel, bottom plate and the clamp plate material in the magazine all adopt high strength aluminum alloy material, has alleviateed device total weight when guaranteeing to drive bird emitter's structural strength.

Description

Quick bullet-withdrawing shell structure for bird expelling
Technical Field
The utility model relates to the technical field of bullet-withdrawing structures, in particular to a rapid bullet-withdrawing structure for bird driving.
Background
Bird repelling is also called bird repelling. Broadly speaking, all means for preventing harmful birds from invading the self-territory, such as farms, orchards, wind power plants, civil and military airports and the like, so as to endanger the labor results or equipment safety of the self-territory are called bird repelling; in a narrow sense, bird repelling is specially used for protecting the taking-off and landing safety of an aircraft in a civil airport, and is used for preventing birds from being sucked into an aircraft engine or striking all aircraft bodies such as an aircraft body, a landing gear, a tail wing, a windshield and the like during the taking-off and landing of the aircraft at a high speed, so that all means for preventing birds from invading such as auditory frightening, visual frightening, direct catching, chemical, ecological or radar early warning are adopted in a critical flight area of the airport, particularly on a runway or taxiway for taking-off and landing of the aircraft.
At present, bird-repellent bomb equipment is widely used in the market, is a comprehensive electromechanical and electric titanium bomb launcher, and can control the direction, pitching motion and launching of the bird-repellent bomb launcher through network signals. The bird-repellent bomb equipment is arranged on a bird-repellent vehicle, can emit titanium bomb according to a specified direction and is used for airport bird-repellent, however, the existing bird-repellent bomb equipment does not have a function of rapidly withdrawing a bomb shell, can be completed only through manual operation, cannot realize full-automatic bomb withdrawal, cannot effectively improve the persistence and timeliness of bird-repellent operation, and reduces the workload of maintaining the bird-repellent equipment.
Disclosure of Invention
The utility model aims to provide a rapid ejection shell structure for bird repelling, which achieves the aim of convenient use.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a but drive bird fast bullet shell structure that returns, includes emission subassembly, drive frame subassembly, electrical apparatus control assembly, the activity sets up between emission subassembly, the drive frame subassembly, electrical apparatus control assembly sets up the inside at the drive frame subassembly, emission subassembly, including fly leaf part, fixed pin, barrel seat spare, fly leaf part passes through fixed pin and barrel seat spare swing joint.
Preferably, the transmitting plate component comprises an opening and closing column, an opening and closing lock hook, a connecting pin, an inner hexagonal cylindrical head screw A, a rear cover plate, an opening and closing lock block and a needle striking plate.
Preferably, one end of the unlocking and locking column movably penetrates through the unlocking and locking hook and extends into the unlocking and locking block, a through hole is formed between one end of the unlocking and locking column and the movably penetrating through the unlocking and locking hook, and the unlocking and locking block is fixedly arranged on the gun barrel through an inner hexagonal cylindrical head screw C.
Preferably, the outer wall cover of the opening and closing post is provided with an opening and closing spring, the opening and closing spring is positioned in the through hole, one end of the opening and closing spring is fixedly connected with the inner wall of the through hole, the other end of the opening and closing spring is fixedly connected with the opening and closing post, the other end of the opening and closing lock hook is connected with the needle plate through a connecting pin, the rear cover plate is fixedly installed with the needle plate through an inner hexagonal cylindrical head screw A, and a pulling rod switch is arranged on the outer surface of the rear cover plate.
Preferably, the needle striking plate is uniformly distributed with needle striking elements at equal intervals, and the needle striking elements specifically comprise an inner hexagonal cylindrical head screw B, a needle striking seat cover, a needle striking seat, a needle striking contact rod and a contact rod.
Preferably, the firing pin seat cover and the firing pin seat are fixedly installed through an inner hexagonal cylindrical head screw B, the firing pin contact rod and the contact rod are respectively arranged on the firing pin seat, the outer wall of the firing pin contact rod is provided with a firing pin contact rod spring, and the outer wall of the contact rod is provided with a contact rod spring.
Preferably, the gun barrel seat part comprises a gun barrel, a hexagon socket head cap screw C, a gun barrel seat, a deep groove ball bearing, a shaft lug, a suspender screw, a large gear, a gasket, a shaft, an A-shaped flat key, a hexagon socket head cap screw D, a connecting hook, a first ejector, a hexagon socket head cap screw E and a second ejector.
Preferably, the fixed cover of front end outer wall of barrel is equipped with the barrel front bezel, the fixed cover of rear end outer wall of barrel is equipped with the rifle seat, the barrel seat passes through jib screw and hits needle board fixed mounting, one side of rifle seat is connected with the axle ear rotation through deep groove ball bearing, the opposite side of rifle seat is connected with A type flat key through the axle, gear wheel, gasket are all overlapped and are established the outer wall at the axle, coupling hook fixed mounting is in rifle seat bottom, first and second refunds the bullet ware and all install on the rifle seat through interior hexagon socket head screw E, first and second refunds the outer wall of bullet ware and all is provided with the refund spring.
The utility model provides a rapid ejection shell structure for bird repellent. The beneficial effects are as follows:
(1) When the launching assembly is in the loading position, the open-close locking column is pulled out, the open-close locking hook is pulled open, the launching plate component is opened, the bullet extractor is pulled open, and the bird-repellent shell or the bird-repellent bullet is taken out, so that the shell or the bullet is retracted. When loading, loading and driving the bird bullet, cover the launching plate part, close the switching latch hook, insert and open the locking post, accomplish the loading, the structure has intensity height, the loading is returned the bullet convenient, safe and reliable's advantage, this drives bird emitter and adopts flip back dress formula, barrel, bottom plate and the clamp plate material in the magazine all adopt high strength aluminum alloy material, has alleviateed device total weight when guaranteeing to drive bird emitter's structural strength.
(2) The bullet-withdrawing device is contacted with the step surface at the bottom of the bullet shell through the arc groove, the bullet shell attached to the gun barrel is withdrawn from the gun barrel rapidly through drawing the bullet-withdrawing device, the problem that bare hands cannot withdraw the bullet is solved, one bullet-withdrawing device can withdraw the bullet shell simultaneously, when the bullet-withdrawing device is pulled to a limited position, the bullet-withdrawing device is withdrawn by bare hands, and meanwhile, a return bullet-withdrawing device spring is arranged in the bullet-withdrawing device, so that the bullet-withdrawing device is reset, and the function of withdrawing the bullet shell rapidly is achieved.
Drawings
FIG. 1 is a view of a bird repellent emission device according to the present utility model;
FIG. 2 is a view of a bird repellent emission assembly according to the present utility model;
FIG. 3 is a perspective view of a transmitting plate assembly of the present utility model;
FIG. 4 is a three view of the gun barrel holder assembly of the present utility model;
FIG. 5 is a view showing the structure of the bullet-ejecting casing of the present utility model;
FIG. 6 is a view showing the internal structure of the barrel of the present utility model
In the figure: the device comprises a1 firing assembly, a 2 transmission seat assembly, a 3 electric appliance control assembly, a11 firing plate assembly, a 12 fixing pin, a 13 gun tube seat assembly, a 111 unlocking and locking column, a 112 unlocking and locking spring, a 113 unlocking and locking hook, a 114 connecting pin, 115 inner hexagonal socket head screw A, a 116 back cover plate, a 1161 pulling rod switch, 117 unlocking and locking block, a 118 needle striking plate, 1181 inner hexagonal socket head screw B, 1182 needle striking seat cover, 1183 needle striking seat, 1184 needle striking contact rod spring, 1185 needle striking contact rod, 1186 contact rod spring, 1187 contact rod, 131 gun tube, 1311 gun tube front plate, 1312 inner hexagonal socket head screw C, 1313 gun tube seat, 1321 deep groove ball bearing, 1322 shaft ear, 1323 boom screw, 1324 large gear, 1325 gasket, 1326 shaft, 1327A type flat key, 1328 inner hexagonal socket head screw D, 133 connecting hook, 134 ejector one, 135 inner hexagonal socket head screw E, ejector two and 137 ejector.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Examples of the embodiments are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements throughout or elements having like or similar functionality. The embodiments described below by referring to the drawings are illustrative and intended to explain the present utility model and should not be construed as limiting the utility model.
In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model.
In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
As shown in fig. 1-6, the present utility model provides a technical solution: the utility model provides a but drive bird fast bullet shell structure that moves back, includes emission subassembly 1, transmission frame subassembly 2, electrical apparatus control assembly 3, and the activity sets up between emission subassembly 1, the transmission frame subassembly 2, and electrical apparatus control assembly 3 sets up in the inside of transmission frame subassembly 2, emission subassembly 1, including emitter plate part 11, fixed pin 12, barrel seat spare 13, emitter plate part 11 passes through fixed pin 12 and barrel seat spare 13 swing joint;
the transmitting plate part 11 comprises an unlocking and locking column 111, an unlocking and locking hook 113, a connecting pin 114, a hexagon socket head cap screw A115, a rear cover plate 116, an unlocking and locking block 117 and a firing pin plate 118;
one end of the opening and closing column 111 movably penetrates through the opening and closing lock hook 113 and extends into the opening and closing block 117, a through hole is formed between one end of the opening and closing column 111 and the movable penetrating through the opening and closing lock hook 113, the opening and closing block 117 is fixedly arranged on the gun barrel 131 through an inner hexagonal cylindrical head screw C1312, an opening and closing spring 112 is sleeved on the outer wall of the opening and closing column 111, the opening and closing spring 112 is positioned in the through hole, one end of the opening and closing spring 112 is fixedly connected with the inner wall of the through hole, the other end of the opening and closing spring 112 is fixedly connected with the opening and closing column 111, the other end of the opening and closing lock hook 113 is connected with the needle striking plate 118 through a connecting pin 114, the rear cover plate 116 is fixedly arranged with the needle striking plate 118 through an inner hexagonal cylindrical head screw A115, and an extraction rod switch 1161 is arranged on the outer surface of the rear cover plate 116;
the striking plate 118 is uniformly provided with striking pin elements at equal intervals, and the striking pin elements comprise a hexagonal socket head cap B1181, a striking pin seat cap 1182, a striking pin seat 1183, a striking pin contact rod 1185 and a contact rod 1187;
the firing pin seat cover 1182 and the firing pin seat 1183 are fixedly arranged through an inner hexagonal cylindrical head screw B1181, a firing pin contact rod 1185 and a contact rod 1187 are respectively arranged on the firing pin seat 1183, a firing pin contact rod spring 1184 is arranged on the outer wall of the firing pin contact rod 1185, and a contact rod spring 1186 is arranged on the outer wall of the contact rod 1187;
the gun barrel seat component 13 comprises a gun barrel 131, an inner hexagonal socket head screw C1312, a gun barrel seat 1313, a deep groove ball bearing 1321, a shaft lug 1322, a suspension rod screw 1323, a large gear 1324, a gasket 1325, a shaft 1326, an A-shaped flat key 1327, an inner hexagonal socket head screw D1328, a connecting hook 133, a first bullet refunder 134, an inner hexagonal socket head screw E135 and a second bullet refunder 136;
the fixed cover of front end outer wall of barrel 131 is equipped with barrel front bezel 1311, the fixed cover of rear end outer wall of barrel 131 is equipped with barrel seat 1313, barrel seat 1313 passes through jib screw 1323 and hits faller 118 fixed mounting, one side of barrel seat 1313 passes through deep groove ball bearing 1321 and is connected with axle ear 1322 rotation, the opposite side of barrel seat 1313 passes through axle 1326 and is connected with A flat key 1327, gear wheel 1324, the equal cover of gasket 1325 is established at the outer wall of axle 1326, connecting hook 133 fixed mounting is in barrel seat 1313 bottom, the first 134 of bullet return, the second 136 of bullet return is all installed on barrel seat 1313 through interior hexagonal cylinder head screw E135, the outer wall of first 134 of bullet return, second 136 of bullet return all is provided with the bullet return spring 137.
When the device is used, when the launching assembly is in the loading position, the unlocking and locking column is pulled out, the unlocking and locking hook is pulled open, the launching plate component is opened, the bullet withdrawing device is pulled open, and the bird-repellent shell or bird-repellent bullet is taken out, so that the shell or bullet withdrawing is realized. When loading, loading and driving the bird bullet, cover the deflector part, close the switching latch hook, insert and open the locking post, accomplish the loading, the structure has intensity height, the loading is returned to the bullet convenience, advantages such as safe and reliable, this drives bird emitter and adopts flip back loading, barrel in the magazine, bottom plate and clamp plate material all adopt high strength aluminum alloy material, the structural strength who drives bird emitter has alleviateed the device gross weight when guaranteeing, the bullet ware passes through circular arc recess and the bottom step face contact of shell case, make the shell case that laminates with the barrel withdraw from in the barrel fast through drawing the bullet ware, solve the problem that bare-handed can't withdraw from the bullet, a bullet ware can withdraw the shell case simultaneously, when the bullet ware is pulled to the limit position, bare-handed the shell case is taken out, built-in bullet ware spring returns simultaneously, it resets to let the bullet ware, but play the effect of quick withdrawal shell case.
When the launching assembly is in the loading position, the unlocking and locking column is pulled out, the unlocking and locking hook is pulled out, the launching plate component is opened, the bullet withdrawing device is pulled out, and the bird-repellent shell or bird-repellent bullet is taken out, so that the shell or bullet withdrawing is realized. When loading, loading and driving the bird bullet, cover the launching plate part, close the switching latch hook, insert and open the locking post, accomplish the loading, the structure has intensity height, the loading is returned the bullet convenient, safe and reliable's advantage, this drives bird emitter and adopts flip back dress formula, barrel, bottom plate and the clamp plate material in the magazine all adopt high strength aluminum alloy material, has alleviateed device total weight when guaranteeing to drive bird emitter's structural strength.
The bullet case can be withdrawn simultaneously by one bullet case withdrawing device, when the bullet case is pulled to a limiting position by hands, the bullet case is taken out, and meanwhile, a return bullet case withdrawing spring is built in, so that the bullet case withdrawing device resets, and the effect of withdrawing the bullet case rapidly is achieved.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims (6)

1. The utility model provides a but drive bird fast bullet shell structure that falls, includes transmission subassembly (1), drive frame subassembly (2), electrical apparatus control assembly (3), its characterized in that: the electric appliance control assembly is characterized in that the emission assembly (1) and the transmission seat assembly (2) are movably arranged, the electric appliance control assembly (3) is arranged inside the transmission seat assembly (2), the emission assembly (1) comprises an emission plate component (11), a fixing pin (12) and a barrel seat component (13), the emission plate component (11) is movably connected with the barrel seat component (13) through the fixing pin (12), the emission plate component (11) comprises an opening and closing column (111), an opening and closing hook (113), a connecting pin (114), an inner hexagonal socket head screw A (115), a rear cover plate (116), an opening and closing block (117) and a firing pin plate (118), and the barrel seat component (13) comprises a barrel (131), an inner hexagonal socket head screw C (1312), a barrel seat (1313), a deep groove ball bearing (1321), a shaft lug (1322), a suspension rod screw (1323), a large gear (1324), a gasket (1325), a shaft (1326), an A-type flat key (1327), an inner hexagonal socket head screw D (1328), a connecting hook (134), a first elastic head screw (133) and a second elastic head screw (133).
2. The rapid ejection shell structure for driving birds according to claim 1, wherein: one end of the unlocking and locking column (111) movably penetrates through the unlocking and locking hook (113) and extends into the unlocking and locking block (117), a through hole is formed between one end of the unlocking and locking column (111) and the movably penetrating through the unlocking and locking hook (113), and the unlocking and locking block (117) is fixedly mounted on the gun barrel (131) through an inner hexagonal cylindrical head screw C (1312).
3. The rapid ejection shell structure for driving birds according to claim 1, wherein: the outer wall cover of the locking and unlocking post (111) is provided with a locking and unlocking spring (112), the locking and unlocking spring (112) is located in the through hole, one end of the locking and unlocking spring (112) is fixedly connected with the inner wall of the through hole, the other end of the locking and unlocking spring (112) is fixedly connected with the locking and unlocking post (111), the other end of the locking and unlocking hook (113) is connected with a needle beating plate (118) through a connecting pin (114), a rear cover plate (116) is fixedly installed with the needle beating plate (118) through an inner hexagonal cylindrical head screw A (115), and a pulling rod switch (1161) is arranged on the outer surface of the rear cover plate (116).
4. The rapid ejection shell structure for driving birds according to claim 1, wherein: the firing pin plate (118) is uniformly provided with firing pin elements at equal intervals, and the firing pin elements specifically comprise a hexagon socket head cap screw B (1181), a firing pin seat cover (1182), a firing pin seat (1183), a firing pin contact rod (1185) and a contact rod (1187).
5. The rapid ejection shell structure for bird repellent according to claim 4, wherein: the utility model discloses a novel structure of a hammer, including a hammer seat cover (1182), a hammer seat (1183), a hammer contact rod (1185), a contact rod (1187), a hammer contact rod spring (1184) and a contact rod spring (1186), wherein the hammer seat cover (1182) and the hammer seat are fixedly installed through an inner hexagonal cylindrical head screw B (1181), the hammer contact rod (1185) and the contact rod (1187) are respectively arranged on the hammer seat (1183), the outer wall of the hammer contact rod (1185) is provided with the hammer contact rod spring (1184), and the outer wall of the contact rod (1187) is provided with the contact rod spring (1186).
6. The rapid ejection shell structure for driving birds according to claim 1, wherein: the front end outer wall fixed cover of barrel (131) is equipped with barrel front bezel (1311), the fixed cover of rear end outer wall of barrel (131) is equipped with rifle socket (1313), barrel socket (1313) pass through jib screw (1323) and firing pin board (118) fixed mounting, one side of barrel socket (1313) is passed through deep groove ball bearing (1321) and is connected with hub (1322) rotation, the opposite side of barrel socket (1313) is passed through axle (1326) and is connected with A type flat key (1327), the outer wall at axle (1326) is all established to gear wheel (1324), gasket (1325) cover, connecting hook (133) fixed mounting is in rifle socket (1313) bottom, first bullet return (134), bullet return (136) are all installed on rifle socket (1313) through interior hexagonal cylinder head screw E (135), the outer wall of first bullet return (134), bullet return (136) all is provided with bullet return (137).
CN202223402019.8U 2022-12-19 2022-12-19 Quick bullet-withdrawing shell structure for bird expelling Active CN218937179U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202223402019.8U CN218937179U (en) 2022-12-19 2022-12-19 Quick bullet-withdrawing shell structure for bird expelling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202223402019.8U CN218937179U (en) 2022-12-19 2022-12-19 Quick bullet-withdrawing shell structure for bird expelling

Publications (1)

Publication Number Publication Date
CN218937179U true CN218937179U (en) 2023-04-28

Family

ID=86094669

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202223402019.8U Active CN218937179U (en) 2022-12-19 2022-12-19 Quick bullet-withdrawing shell structure for bird expelling

Country Status (1)

Country Link
CN (1) CN218937179U (en)

Similar Documents

Publication Publication Date Title
CN108583889B (en) Airborne pneumatic net throwing device of unmanned aerial vehicle
CN208975018U (en) A kind of window breaking device for fire-fighting unmanned plane
CN110271671B (en) Bullet throwing device and fire-fighting unmanned aerial vehicle
CN218937179U (en) Quick bullet-withdrawing shell structure for bird expelling
CN108910073A (en) Unmanned aerial vehicle ejecting frame launching trolley and unmanned plane launching technique
CN209426866U (en) Bindiny mechanism, lid assembly and motor vehicle assembly
CN110663675B (en) Automatic spring-up type bird repeller
CN109264002A (en) A kind of half active opener of unmanned plane recorery parachute of rear power
CN111186586B (en) Smog emitter suitable for unmanned aerial vehicle
CN219121218U (en) Spring type rocket thrust testing device
CN213620225U (en) Air capture net throwing type unmanned aerial vehicle
CN212253860U (en) Lock hook type cylinder shooting patrol missile wing unfolding and locking mechanism
CN218937178U (en) Bird repellent emitter capable of electrically controlling emission
CN109552595A (en) A kind of the quick dispatch mechanism and quick dispatch method of unmanned plane hatchcover
CN219927968U (en) Built-in weapon stores pylon system
CN108674629B (en) Mechanism type sealing opening cover of aircraft external hanging point
CN111623667A (en) Multifunctional tactical stick
CN209485157U (en) Unmanned plane arrests module with net rifle
CN113120251B (en) Air-jet unmanned aerial vehicle launching tube
CN211618090U (en) Air capture net throwing type unmanned aerial vehicle
CN216523445U (en) Repeatedly usable's wireless electric shock bullet
CN219090930U (en) Accurate guided fire extinguishing bullet capable of carrying ammunition with band
CN218066140U (en) Flying capture net gun
CN202956030U (en) Shield
CN215826984U (en) Small-bore electric primer multi-tube emitter

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant