CN218066140U - Flying capture net gun - Google Patents
Flying capture net gun Download PDFInfo
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- CN218066140U CN218066140U CN202222431958.9U CN202222431958U CN218066140U CN 218066140 U CN218066140 U CN 218066140U CN 202222431958 U CN202222431958 U CN 202222431958U CN 218066140 U CN218066140 U CN 218066140U
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Abstract
The utility model provides a net rifle is arrested in flight, including net rifle body and frame, the net rifle body includes a net section of thick bamboo and percussion pipe, and a net section of thick bamboo possesses the storage net chamber and puts the bullet chamber, and is located the length direction of frame, it is used for putting into the ail shooter to put the bullet chamber. The unmanned aerial vehicle frame and the net gun body are integrally arranged, and the net barrel part of the net gun body faces the length direction of the frame, so that the recoil force can be integrally transmitted to the frame when the net barrel launches and captures a net, the phenomenon that the frame overturns or even crashes due to uneven recoil force distribution is avoided, and meanwhile, the weight of the equipment can be reduced due to the integral arrangement, so that the whole equipment is more flexible, the operability is higher, and the carrying is convenient; the camera is arranged, and meanwhile, the corresponding image transmission receiver is arranged on the rack, so that real-time image transmission can be carried out in the flying process of the rack, real-time control can be conveniently carried out by an operator, and the capturing accuracy is improved.
Description
Technical Field
The utility model relates to an it is alert with equipment technical field, especially relate to a net rifle is arrested in flight.
Background
The unmanned plane is called unmanned plane for short, and is called UAV for short in English, and is a manned plane operated by radio remote control equipment and a self-contained program control device, or is completely or intermittently and autonomously operated by an onboard computer, and the unmanned plane can be loaded with equipment such as a camera and the like to carry out operations such as aerial photography, geological exploration and the like.
At present, the main methods of the domestic and foreign net-catching technology are as follows: the target is caught by adopting a large rotor unmanned aerial vehicle to load a net gun to launch net bullets or adopting modes such as a rotor unmanned aerial vehicle hanging catching net and the like. If the authorized notice number is CN207050575U, "unmanned aerial vehicle mounted aerial capture net gun", it adopts rotor unmanned aerial vehicle mounted capture net to capture operation, and this kind of method needs large unmanned aerial vehicle to carry out mounting only because net gun dead weight is great, is influenced by target direction and maneuverability, leads to aiming strike difficulty increase, and has extremely high operational technical requirement on the capture hand, limited success rate and higher equipment cost.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model provides a net rifle is arrested in flight, through carrying out the integral type setting with net rifle and unmanned aerial vehicle, effectively reduce holistic manufacturing cost, when having reduced simultaneously that the net rifle passes through modes such as carry and installs on unmanned aerial vehicle, the influence of the produced recoil of net rifle transmission improves the transmission degree of accuracy.
The technical scheme of the utility model is realized like this: the utility model provides a flying catching net gun, which comprises a net gun body and a frame, wherein,
the net gun body comprises a net cylinder and a firing tube, wherein,
the net barrel is provided with a net storage cavity and a bullet discharge cavity, is positioned in the length direction of the rack, and is used for placing the nail shooting bullets;
the firing tube is fixed on the rack, one end of the firing tube is detachably fixed with the end part of the net cylinder bullet cavity, and the firing tube is used for firing the nail shooting bullets;
be provided with a plurality of rotor subassembly in the frame, the rotor subassembly is used for driving the frame flight.
On the basis of the above technical solution, preferably, the firing tube includes a tube body, a hammer, a positioning assembly and an elastic portion, wherein,
the pipe body is fixed in the frame;
the driving hammer is provided with a driving pin, the driving hammer is arranged in the pipe body and can move along the length direction of the pipe body, and when the driving hammer moves to one end, close to the net drum, of the pipe body, the driving pin enters the bullet cavity;
the positioning component is fixed on the frame and used for locking or releasing the hammer;
and one end of the elastic part is fixed with the pipe body, and the other end of the elastic part is contacted with the hammer and is used for pushing the hammer to move in the pipe body.
On the basis of the above technical scheme, preferably, the device further comprises a camera, and the camera is rotatably arranged on the rack.
On the basis of the technical scheme, the percussion instrument is preferably characterized by further comprising a locking screw, the locking screw is inserted into the rack and is in threaded connection with the rack, one end of the locking screw inserted into the rack extends into the percussion tube and is in contact with the net barrel, and the locking screw is used for fixing the net barrel and the percussion tube.
Further preferably, the barrel body further comprises a loading trigger, an upper loading opening is formed in the outer side of the barrel body, and the loading trigger is fixed with the hammer and extends to the outer portion of the barrel body through the upper loading opening.
On the basis of the technical scheme, preferably, the rack is provided with a first interlayer and a second interlayer, and the firing tube is fixed in the first interlayer.
Further preferably, the percussion tube comprises a plurality of tube clamps, each of the tube clamps is fixed in the first interlayer and fixed with the outside of the percussion tube, and the tube clamps are used for fixing the percussion tube.
Further preferably, the flight control device further comprises a flight control device fixed in the second interlayer.
The utility model discloses a net rifle is arrested in flight has following beneficial effect for prior art:
(1) The unmanned aerial vehicle frame and the net gun body are integrally arranged, and the net barrel part of the net gun body faces the length direction of the frame, so that the recoil force can be integrally transmitted to the frame when the net barrel launches and captures a net, the phenomenon that the frame overturns or even crashes due to uneven recoil force distribution is avoided, and meanwhile, the weight of the equipment can be reduced due to the integral arrangement, so that the whole equipment is more flexible, the operability is higher, and the carrying is convenient;
(2) The camera is arranged, and meanwhile, the corresponding image transmission receiver is arranged on the rack, so that real-time image transmission can be carried out in the flying process of the rack, real-time control can be conveniently carried out by an operator, and the capturing accuracy is improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a perspective view of the flying catching net gun of the utility model;
fig. 2 is a perspective view of the flying catching net gun of the utility model from another view angle;
fig. 3 is a perspective view of another view angle of the flying catching net gun of the present invention;
fig. 4 is a three-dimensional cross-sectional view of another visual angle of the flying catching net gun of the utility model.
Detailed Description
The technical solutions of the embodiments of the present invention will be described clearly and completely below with reference to the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work all belong to the protection scope of the present invention.
As shown in figures 1-4, the utility model discloses a flying catching net gun, including net gun body 1 and frame 2.
The net gun body 1 comprises a net barrel 11 and a firing pipe 12, the net barrel 11 is composed of two cylindrical barrels with different diameters, the middle of the two barrels is fixed through a conical transition section, the two net barrels 11 are communicated inside, a net storage cavity 111 is arranged in the larger barrel, a nail shooting cavity 112 is arranged in the smaller barrel, the net storage cavity 111 is used for placing a catching net, the nail shooting cavity 112 is used for placing a nail shooting bullet for shooting the catching net, meanwhile, the net barrel 11 is arranged in the length direction of the rack 2, when the net barrel 11 is guaranteed to shoot the catching net, the recoil force generated by the nail shooting bullet cannot drive the rack 2 to overturn in the air, the firing pipe 12 is fixed on the rack 2, one end of the firing pipe is detachably fixed with the end part where the nail shooting cavity 112 of the net barrel 11 is located, the nail shooting bullet can be placed in the shooting cavity 112 or a cartridge case can be replaced by the nail shooting bullet through dismounting the net barrel 11, the shooting pipe 12 strikes the nail shooting bullet when the net is launched, and the net is captured.
Specifically, rotor subassembly 21 includes linking arm and motor, installs the screw to the output of motor on, and it is rotatory to drive the screw through the motor to drive 2 flights of frame, in practical application, rotor subassembly 21 can choose for use to be four, can make 2 stable quick flights of frame, and the cost is lower for installing rotor subassembly 21 more than four.
It should be noted that, in order to further reduce the overall weight of the device, a plurality of weight reducing openings may be formed in the three fixing plates, so that the fixing plates are hollowed out on the premise of ensuring the rigidity thereof, thereby reducing the overall weight of the device after being assembled.
In a preferred embodiment, the firing tube 12 includes a tube 121, a hammer 122, a positioning assembly 123 and an elastic portion 124, the tube 121 is fixed in the frame 2, and is specifically fixed in the first interlayer 201 of the frame 2, the tube 121 is a hollow metal long tube, a firing pin 1221 is disposed on a side of the hammer 122 close to the net barrel 11, the hammer 122 is movably disposed in the tube 121 and can move along a length direction of the tube 121, the hammer 122 is externally cylindrical and is adapted to an interior of the tube 121, so as to avoid large kinetic energy loss and abrasion caused by impacting a tube wall of the tube 121 during moving, the positioning assembly 123 is fixed on the frame 2, one end of the elastic portion 124 is fixed to the tube 121, and the other end of the elastic portion is in contact with the hammer 122, during use, the hammer 122 first moves toward a side away from the net barrel 11 until the positioning assembly 123 is locked, while moving, the elastic portion 124 is compressed, so that an elastic potential energy of the elastic portion 124 is gradually increased, and when the positioning assembly 123 releases the hammer 122, the elastic portion 124 pushes the hammer 122 to move in the tube 121 toward the net barrel 11 until the firing pin 1221 is fired, thereby firing pin 122112.
Specifically, locating component 123 includes the fixing base, percussion steering wheel and setting element, the fixing base is fixed at the top of frame 2, and be located body 121 directly over, the inside of fixing base is provided with the setting element, the setting element is triangle-shaped and sets up, and can be at the inside rotation of fixing base, the setting element is in place the back at hammer 122, stretch into in the body 121, will hit hammer 122 card position behind compression elasticity portion 124, the percussion steering wheel is then fixed on the fixing base, it is rotatory for control setting element, loosen or lock hammer 122, elasticity portion 124 wherein can directly adopt the spring, the transmission operation of hammer 122 is hit in the implementation.
It should be noted that, in order to control the firing steering engine, an electric controller should be installed on the second interlayer 202 to be used as a control device for the firing steering engine.
As a preferred embodiment, the flying-type net drum further comprises a camera 3, wherein the camera 3 is rotatably arranged on the frame 2, and particularly can be fixed on a fixed seat of the positioning assembly 123, and is installed without an additional installation part, and the installation level of the camera 3 is higher than the highest level of the net drum 11, so that real-time image transmission can be performed in the flying process of the frame 2.
Specifically, in order to transmit the image captured by the camera 3 in real time and facilitate the capturing arm to perform the flying operation, the image transceiver may be directly installed in the second interlayer 202 and used as an image transmission device.
As a preferred embodiment, still include locking screw 4, locking screw 4 inserts frame 2 and with frame 2 threaded connection, outside the one end that net section of thick bamboo 11 is connected with percussion pipe 12, is provided with the ring channel, and the tip of net section of thick bamboo 11 inserts percussion pipe 12 in, locking screw 4 inserts the one end of frame 2 and extends to the inside of percussion pipe 12 and insert in the ring channel of net section of thick bamboo 11, can be fixed net section of thick bamboo 11 with percussion pipe 12 through locking screw 4, otherwise, twists locking screw 4, makes it leave net section of thick bamboo 11, can dismantle net section of thick bamboo 11, the installation nail shooting bullet with catch the net.
In the above embodiment, in order to facilitate the driving hammer 122 to perform the loading, a loading trigger 5 is further provided, an loading port 1211 is formed on the outer side of the tube body 121, the loading trigger 5 is fixed to the driving hammer 122 and extends to the outside of the tube body 121 through the loading port 1211, the loading port 1211 is disposed in a straight shape and is consistent with the length direction of the firing tube 12, and after the firing pin 1221 on the driving hammer 122 is inserted into the net barrel 11, the loading trigger 5 can be pulled along the loading port 1211 to move the driving hammer 122 in the tube body 121 to return to the position before the firing of the nail cartridge, thereby completing the loading operation.
On frame 2, still fixed a plurality of pipe clamp 7, each pipe clamp 7 all sets up in first intermediate layer 201, and fixed with the outside of percussion pipe 12, and through segmentation fixed, fixes percussion pipe 12 on frame 2, and it needs to notice that pipe clamp 7 can choose for use for three, and wherein two set up respectively in the both ends of percussion pipe 12, and remaining one need be fixed near the middle section of percussion pipe 12, and need be apart from going up bore 1211 at least one centimetre, avoids influencing and goes up bore trigger 5 and carry out the action of going up the bore.
The utility model discloses a theory of operation does: pull down net section of thick bamboo 11 from frame 2 and percussion pipe 12 to put into through storing up net chamber 111 and catch the net, insert the shot-pin bullet and put bullet chamber 112, install net section of thick bamboo 11 again on percussion pipe 12, in the use, drive frame 2 and the flight of net rifle body 1 through rotor subassembly 21 and remove, when the net is caught in the needs transmission, by the percussion pipe 12 percussion shot-pin bullet, and catch the net through the shot-pin bullet transmission, thereby carry out the net to suspect or illegal flight unmanned aerial vehicle and catch.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and should not be construed as limiting the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. The utility model provides a net rifle is arrested in flight which characterized in that: comprises a net gun body (1) and a frame (2), wherein,
the net gun body (1) comprises a net cylinder (11) and a firing tube (12), wherein,
the net barrel (11) is provided with a net storage cavity (111) and an ejection cavity (112), and is positioned in the length direction of the rack (2), and the ejection cavity (112) is used for putting in nail shooting bullets;
the firing tube (12) is fixed on the rack (2), one end of the firing tube is detachably fixed with the end part of the net drum (11) where the cartridge discharging cavity (112) is located, and the firing tube (12) is used for firing the nail shooting cartridge;
be provided with a plurality of rotor subassembly (21) on frame (2), rotor subassembly (21) are used for driving frame (2) flight.
2. The flight capture net gun of claim 1, wherein: the firing tube (12) comprises a tube body (121), a hammer (122), a positioning component (123) and an elastic part (124), wherein,
a pipe body (121) fixed in the frame (2);
the hammer (122) is provided with a hammer pin (1221), the hammer (122) is arranged in the pipe body (121) and can move along the length direction of the pipe body (121), and when the hammer (122) moves to one end, close to the net barrel (11), of the pipe body (121), the hammer pin (1221) enters the bullet discharge cavity (112);
a positioning assembly (123) fixed on the frame (2) for locking or releasing the hammer (122);
and an elastic part (124) having one end fixed to the pipe body (121) and the other end contacting the hammer (122) and adapted to push the hammer (122) to move in the pipe body (121).
3. The fly capture net gun of claim 1, wherein: still include camera (3), camera (3) rotatable setting is on frame (2).
4. The fly capture net gun of claim 1, wherein: still include locking screw (4), locking screw (4) insert frame (2) and with frame (2) threaded connection, the one end that locking screw (4) inserted frame (2) extends to the inside of percussion pipe (12) and contacts with a net section of thick bamboo (11), locking screw (4) are used for fixing a net section of thick bamboo (11) and percussion pipe (12).
5. The flight capture net gun of claim 2, wherein: the anti-explosion tube further comprises a bore loading trigger (5), a bore loading opening (1211) is formed in the outer side of the tube body (121), and the bore loading trigger (5) is fixed with the hammer (122) and extends to the outer portion of the tube body (121) through the bore loading opening (1211).
6. The flight capture net gun of claim 1, wherein: a first interlayer (201) and a second interlayer (202) are arranged on the rack (2), and the firing tube (12) is fixed in the first interlayer (201).
7. The fly capture net gun of claim 6, wherein: the percussion tube is characterized by further comprising a plurality of tube clamps (7), each tube clamp (7) is fixed in the first interlayer (201) and fixed with the outer portion of the percussion tube (12), and the tube clamps (7) are used for fixing the percussion tube (12).
8. The fly capture net gun of claim 6, wherein: the aircraft further comprises a flight controller (6), and the flight controller (6) is fixed in the second interlayer (202).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222431958.9U CN218066140U (en) | 2022-09-14 | 2022-09-14 | Flying capture net gun |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222431958.9U CN218066140U (en) | 2022-09-14 | 2022-09-14 | Flying capture net gun |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218066140U true CN218066140U (en) | 2022-12-16 |
Family
ID=84408641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222431958.9U Active CN218066140U (en) | 2022-09-14 | 2022-09-14 | Flying capture net gun |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218066140U (en) |
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2022
- 2022-09-14 CN CN202222431958.9U patent/CN218066140U/en active Active
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