WO2017206078A1 - Dispositif de combat aérien et procédé pour véhicule aérien sans pilote - Google Patents

Dispositif de combat aérien et procédé pour véhicule aérien sans pilote Download PDF

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Publication number
WO2017206078A1
WO2017206078A1 PCT/CN2016/084181 CN2016084181W WO2017206078A1 WO 2017206078 A1 WO2017206078 A1 WO 2017206078A1 CN 2016084181 W CN2016084181 W CN 2016084181W WO 2017206078 A1 WO2017206078 A1 WO 2017206078A1
Authority
WO
WIPO (PCT)
Prior art keywords
rubber band
air combat
blades
unmanned aerial
uav
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.)
Ceased
Application number
PCT/CN2016/084181
Other languages
English (en)
Chinese (zh)
Inventor
胡家祺
黄景旺
梁宏
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.)
Shenzhen Acceleration Tech Co Ltd
Original Assignee
Shenzhen Acceleration Tech 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 Shenzhen Acceleration Tech Co Ltd filed Critical Shenzhen Acceleration Tech Co Ltd
Priority to CN201680000459.9A priority Critical patent/CN106061840B/zh
Priority to PCT/CN2016/084181 priority patent/WO2017206078A1/fr
Publication of WO2017206078A1 publication Critical patent/WO2017206078A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft

Definitions

  • the present invention belongs to the field of aircraft technology, and in particular, to a UAV air combat device and a UAV air combat method.
  • Drone n Base which is a palm-sized quadrotor with an infrared transceiver on the body. Infrared transceivers achieve virtual shooting between multiple aircraft. If the infrared rays emitted by the other party are "shot”, they are considered to be “shot down”. This method does not actually shoot down the opponent during the air combat. It is reflected in the software score; the other is the tobyrich.vegas drone, which is a fixed-wing drone that uses a mobile phone to control and use augmented reality technology to simulate the launch and match of weapons between drones.
  • the way to use is also the way to simulate the number of hits, not to actually shoot down the opponent drones; the other is that the drone company Parrot has also introduced similar drone products, but both use augmented reality and infrared Techniques such as sending and receiving to achieve the simulated "shooting" do not actually shoot down the opponent drone.
  • An object of the present invention is to provide a rubber band emitting device, which aims to solve the technical problem that the weapon launching device in the unmanned aerial vehicle can not actually shoot down the other drone and has a lack of entertainment effect.
  • the present invention is implemented in such a manner that a UAV air combat device is used for at least two UAVs to conduct air combat and to determine the number of shots to be shot down and the number of shots to be defeated by each of the UAVs.
  • the man machine includes a fuselage, a lift mechanism mounted on the fuselage, and a rubber band launching device; the rubber band launching device is loaded with a rubber band for winding at least one lift mechanism of the other drone to shoot the other drone,
  • the rubber band emitting device includes a mount assembly fixedly mounted on the fuselage, a driving device fixedly mounted on the mount assembly and configured to receive a weapon transmitting signal, and transmitting the rubber band under the driving action of the driving device Going out of the launch component.
  • the UAV air combat device further includes a ground remote control device for controlling the flight of each of the UAVs and transmitting the weapon transmission signal to the driving device, and each of the UAVs further includes a remote control receiving device that receives a flight control signal from the ground remote control device and controls the flight state of the drone according to the flight control signal.
  • the ground remote control device is provided with a rubber band launching switch.
  • the UAV air combat device further includes a camera mounted on each of the UAVs and used for capturing image information of the operational status of each of the UAVs in the air combat, and is installed on each of the UAVs. And an image transmission device for receiving image information captured by the camera and an image display device for receiving image information transmitted by the image transmission device and performing image display.
  • the UAV air combat device further includes a detecting device installed on each of the UAVs and configured to detect the other drone to lock the attack target.
  • the detecting device is at least one of an inertial sensor, an infrared sensor, an ultrasonic sensor, and a radar.
  • the transmitting assembly includes a driving device that drives the rotation thereof and is used to wind the rubber band a driven wheel at one end, a reel for winding the other end of the rubber band, a fixing rod connected between the driven wheel and the reel to elongate the rubber band, and the rubber band from the A peeling mechanism that is detached from the driven wheel and the reel, and one end of the fixing rod is fixed to the driven wheel and the other end is fixedly mounted with the reel.
  • the driven wheel protrudes in a plurality of spaced apart first blades in a circumferential direction thereof, and the winding wheel is provided with a plurality of intervals in a circumferential direction thereof and corresponds to the first blade.
  • a second blade the rubber band being wound between the first blade and the second blade.
  • the rubber bands are symmetrically folded in half, and both end portions thereof are sleeved on the two first blades, and the intermediate folding portions are sleeved on the second blades.
  • the first blade surrounding the two ends of the rubber band is spaced apart from the first blade corresponding to the second blade around the intermediate folded portion of the rubber band .
  • each of the first blades is disposed along an axial direction of the driven wheel, and each of the first blades is curved along a bottom thereof to an end thereof, and each of the first blades faces in the same direction bending.
  • the driving device has an output shaft
  • the peeling mechanism further includes means for transmitting power generated by the driving device to the driven wheel and for using the rubber band from the driven wheel A rope that is peeled off to be emitted, the rope being connected between the output shaft and the driven wheel.
  • the peeling mechanism further includes a reel that is mounted on the output shaft and rotates with the output shaft for winding the string.
  • the UAV air combat device installs the rubber band launching device on each of the drones participating in the air combat and uses the launching component to launch the rubber band
  • the lift mechanism is stopped to be forced to land, and the number of shots and the number of shots are counted to determine the air combat outcome, which not only effectively shoots down the other drone, It is also very entertaining, giving users who participate in air combat a great entertainment experience, greatly enhancing the experience of drone air combat.
  • FIG. 1 is a structural view of a rubber band emitting device according to an embodiment of the present invention.
  • FIG. 2 is an exploded view of the rubber band emitting device of FIG. 1; [0025] FIG.
  • Figure 3 is a partial enlarged view of III in Figure 2;
  • Figure 4 is a structural view of the reel of Figure 1;
  • FIG. 5 is a structural view of the rubber band emitting device of FIG. 1 around which a rubber band is disposed;
  • FIG. 6 is a partial enlarged view of the rubber band emitting device with the rubber band around FIG. 5; [0029] FIG.
  • FIG. 7 is a structural diagram of a drone equipped with a rubber band launching device according to an embodiment of the present invention.
  • FIG. 8 is a structural view of the drone of FIG. 7 in another direction.
  • first and second are used for descriptive purposes only, and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated.
  • features defining “first” and “second” may explicitly or implicitly include one or more of the features.
  • the meaning of “plurality” is two or more, unless specifically defined otherwise.
  • the terms “installation”, “connected”, “connected”, “fixed” and the like should be understood broadly, and may be, for example, a fixed connection or a Removable connection, or integrated; can be mechanical connection or electrical connection; it can be directly connected or indirectly connected through an intermediate medium, which can be the internal connection of two elements or the interaction of two elements.
  • the meaning of the above terms in the present invention can be understood by those skilled in the art on a case-by-case basis.
  • the UAV air combat device provided by the embodiment of the present invention is used for at least two UAVs to perform air combat and determine the number of shots and the number of shots to be defeated by each of the UAVs.
  • Each of the drones includes a fuselage 10, a lift mechanism 20 mounted on the fuselage 10, and a rubber band launching device 4; the rubber band launching device 4 is loaded with at least one lift mechanism 20 for winding the other drone a rubber band 30 that is knocked down by the other drone, the rubber band emitting device 4 includes a mount assembly 40 fixedly mounted on the body 10, and a driving device fixedly mounted on the mount assembly 40 for receiving a weapon transmitting signal 60 and an emission assembly 50 that emits the rubber band 30 under the driving action of the driving device 60.
  • the UAV air combat device installs the rubber band launching device 4 on each of the drones participating in the air combat and uses the launching assembly 50 to launch the rubber band 30 to wrap around the other side.
  • At least one lifting mechanism 20 in the human machine causes the lifting mechanism 20 to stop rotating and is forced to land.
  • the rubber band 30 is a rubber band 30 or a rubber-like member 30 having an elastic member to wind the lifting mechanism 20 by ejection.
  • the drones of the combating parties are given different markings to distinguish them, for example, by applying different colors to the fuselage 10 of each of the drones, or by marking numbers and names. And so on, to distinguish between different combatant drones and judging scores.
  • the rubber bands 30 used by the combating parties can be distinguished by different colors and are simple to use.
  • the lift mechanism 20 may be a propeller, a wing, or a mechanism disposed on the drone to provide lift.
  • the unmanned aerial vehicle provided by each embodiment of the present invention is a multi-rotor aircraft, and the lifting mechanism 20 is a propeller, and the number of the propellers is three or more.
  • the drone may also be an aircraft having two or more rotors, and is not limited thereto.
  • the combatants involved in the air combat are divided into two or more parties, so that the air combat drone is at least two or more;
  • the selected air combat site is optimized with grass or soft ground to prevent the drone from being hit by the ground and causing damage to the drone.
  • the UAV air combat device further includes a ground remote control device for controlling the flight of each of the UAVs and transmitting the weapon transmission signal to the driving device 60.
  • each of the drones further includes a remote control receiving device (not shown) that receives a flight control signal from the ground remote control device and controls the flight state of the drone based on the flight control signal.
  • the controller of each of the drones transmits a flight control signal to the remote control receiving device by controlling the ground remote control device to control the flight direction, flight speed, flight state, etc.
  • the weapon transmitting signal is sent to the driving device 60 by the ground remote control device, and the driving device 60 drives the transmitting component 50 to emit the rubber band 30 after receiving the weapon transmitting signal, so that the rubber band 30 is wrapped around the other side.
  • the operator of each of the drones can continuously transmit a weapon transmission signal to the driving device 60 by controlling the ground remote control device, such that the transmitting assembly 50 will continuously launch the rubber band 30. Going out to increase the probability of shooting down, enhance the real experience of combat and improve the entertainment effect.
  • the ground remote control device is provided with a rubber band 30 launching switch, and the rubber band 30 is activated by a two-stage self-reset switch.
  • the operator of each of the drones continuously presses the rubber band 30 to launch a flag to continuously transmit a weapon transmission signal to the driving device 60, so that the rubber band 30 will be continuously emitted.
  • the operator intermittently presses the rubber band 30 to launch the brake, and the ground remote control device intermittently transmits a weapon transmission signal to the driving device 60, so that the rubber band 30 is intermittently emitted, thereby achieving no The man-machine's shot.
  • the rubber band 30 can be continuously or intermittently emitted by controlling the launch of the rubber band 30, which greatly improves the combat experience and entertainment effect.
  • the weapon transmitting signal that controls the firing assembly 50 to emit the rubber band 30 uses a pulse width modulated duty cycle signal, but is not limited to.
  • the UAV air combat device further includes a camera 70 mounted on each of the UAVs and used for capturing image information of the operational status of each of the UAVs in an air combat.
  • an image transmission device (not shown) mounted on each of the drones for receiving image information captured by the camera 70
  • an image display device for receiving image information transmitted by the image transmission device and displaying the image ( Not shown).
  • the image information captured by the camera 70 is transmitted to the On the image display device, it is easy to watch and watch, and enhance the participation of air combat audiences.
  • the image display device may be a virtual reality display device, a television screen, an outdoor display screen, or the like. The viewer can view the live video of the pilot's viewing angle through the image display device to enhance the viewing effect.
  • the UAV air combat device further includes a detecting device installed on each of the UAVs and configured to detect the other UAV to lock the attack target (not shown). Show). Setting the detecting device to detect the other party's drone and determining whether it is an offensive target, determining an attack target, transmitting a weapon launch signal by controlling the ground remote control device, and transmitting the rubber band 30 by using the launching component 50 It is shot down by winding the lift mechanism 20 of the other drone.
  • the detecting device is at least one of an inertial sensor, an infrared sensor, an ultrasonic sensor, and a radar.
  • the detecting device may be an inertial sensor, an infrared sensor, an ultrasonic sensor or a radar, or a combination thereof to enhance the detection intensity and ensure the accuracy of the target locking.
  • the mounting base assembly 40 includes a fixing base 42 fixedly mounted on the body 10 for fixedly mounting the driving device 60 and the transmitting component 50 .
  • the support base 44 and the connecting bracket 46 fixedly connected between the fixing base 42 and the support base 44 to change the mounting angle of the support base 44.
  • the rubber band emitting device 4 is fixedly mounted on the body 10 by the fixing base 42 and the mounting device 44 is mounted to mount the driving device 60 and the transmitting assembly 50, and in the fixing seat
  • the connecting bracket 46 is fixedly mounted between the support bracket 44 and the support bracket 44, and the mounting bracket 46 is used to change the mounting angle of the support base 44 relative to the fixing base 42 by providing the fixing base 42 and the support.
  • the seat 44 and the connecting bracket 46 cooperate to stably and securely mount the transmitting assembly 50 to the body 10, and the structure is simple.
  • the fixing base 42 is fixedly mounted on the body 10 by using the bolt.
  • the fixing structure of the fixing base 42 and the body 10 may be The manner in which the snap structure or the snap structure is combined with the bolt connection or the like is not limited thereto.
  • the connecting bracket 46 has plasticity.
  • the connecting bracket 46 has plasticity, on the one hand, the mounting angle of the transmitting assembly 50 can be changed, and on the other hand, the impact can be absorbed and the damage can be reduced during the falling of the drone.
  • the connecting bracket 46 is bent.
  • the transmitting assembly 50 includes a driven wheel 52 driven by the driving device 60 for winding the end of the rubber band 30, and is used for winding the rubber band 30.
  • a reel 54 at one end a fixing rod 55 connected between the driven wheel 52 and the reel 54 to lengthen the rubber band 30, and the rubber band 30 from the driven wheel 52 and the A peeling mechanism (not shown) that is peeled off and released from the reel 54 is attached, and one end of the fixing rod 55 is fixed to the support base 44 and the reel 54 is fixedly mounted at the other end.
  • the two ends of the rubber band 30 are respectively disposed around the driven wheel 52 and the reel 54 are disposed on the driven wheel 52 and the reel 54 by the peeling mechanism during rotation of the driven wheel 52 by the driving device 60. It is peeled off and launched, and has a simple structure and convenient use.
  • the fixing rod 55 is a hollow tubular structure, and the length thereof may depend on the tensile deformation of the rubber band 30 and the distance and speed of the required ejection.
  • the driven wheel 52 and the reel 54 are fixed to both ends of the fixed rod 55, and rotate together with the driving of the driving device 60.
  • the driven wheel 52 has a plurality of spaced-apart first blades 520 protruding in a circumferential direction thereof, and the reel 54 has a plurality of circumferentially protruding protrusions
  • the second blade 540 is disposed at intervals and corresponds to the first blade 520, and the rubber band 30 is wound between the first blade 520 and the second blade 540.
  • the number of the first blades 520 is the same as the number of the second blades 540, and may be, for example, three, four, five or any other number, and is not limited thereto.
  • the driven wheel 52 includes a first wheel body portion 522 fixed to the fixing rod 55, and the first blade portion 520 is along the first wheel body portion.
  • the circumferential direction of the 522 is protruded and is equally spaced outside the first wheel body 522; the first wheel body 522 is integrally formed with the first blade 520 to ensure its overall strength and simplification.
  • the reel 54 includes a second wheel body 542 fixed to the fixing rod 55, the second blade 540 is protruded along a circumferential direction of the second wheel body 542, and in the second The outer portions of the wheel body portion 542 are equally spaced; the second wheel body portion 542 is integrally formed with the second blade 540 to ensure its overall strength and simplify the manufacturing process.
  • the first wheel body portion 522, the fixing rod 55 and the second wheel body portion 542 are coaxially disposed.
  • the rubber band 30 is symmetrically folded and the two ends of the rubber band 30 are sleeved on the two first blades 520 and the intermediate folding portion is sleeved on the second blade 540.
  • the rubber band 30 is symmetrically folded on the first blade 520 and the second blade 540 such that the rubber band 30 forms an isosceles triangle on the first blade 520 and the second blade 540, and
  • the two ends of the rubber band 30 are hooked on the two first blades 520 and the intermediate folding portions are hooked on the second blades 540 to extend the stretched length of the rubber bands 30 to ensure a sufficient ejection distance and Speed, increase the strength of shooting down the other drone.
  • first blades 520 is interposed between the two first blades 520 with the rubber band 30, and the second blade 540 with the middle half-folded portion of the rubber band 30 is buckled. Located on the axis of symmetry of the two first blades 520.
  • the spacing between said ends is provided around the portion of the rubber string 30 has a first vane 520 and the intermediate rubber string 30 is provided around the folded portion
  • the second blade 540 corresponds to the The first blade 520. It can be understood that the first blade 520 is spaced between the two first blades 520 with the rubber band 30, and the second blade 540 with the middle half-folded portion of the rubber band 30 is located.
  • the symmetry axes of the two first blades 520 correspond to the first blades 520 that are spaced apart, thereby ensuring that the rubber bands 30 are in a symmetrically folded state.
  • the rubber band 30 may also be unilaterally hooked between the first blade 520 and the second blade 540.
  • each of the first blades 520 is disposed along an axial direction of the driven wheel 52 , and each of the first blades 520 is bent along a bottom thereof to an end thereof. And each of the first blades 52 0 is curved in the same direction.
  • Each of the first blades 520 includes a first bottom portion 524 and a first end portion 526, the first bottom portion 524 is coupled to the first wheel body portion 522, and the first end portion 526 is the first blade 52 0 Free end and away from the first bottom 524.
  • Each of the first blades 520 has a sheet-like structure, and each of the first blades 520 is curved along the first bottom portion 524 to the first end 526, and each of the first blades 520 is at the first The circumferential direction of the wheel body portion 522 is curved in the same direction.
  • each of the first vanes 520 has substantially the same axial width from the first bottom portion 524 to the first end portion 526 of the first wheel body portion 522.
  • the structure of each of the first blades 520 is not limited thereto, and each of the first blades 520 may also be a non-bending plate shape, so that the rubber bands 30 can be buckled.
  • each of the second blades 540 is disposed along the axial direction of the reel 54, and each of the second blades 540 is along the bottom to the end thereof.
  • the axial width of the reel 54 is gradually reduced.
  • Each of the second blades 540 includes a second bottom portion 544 and a second end portion 546.
  • the second bottom portion 544 is coupled to the second wheel body portion 542, and the second end portion 546 is free for the second blade 540. And away from the second bottom 544.
  • Each of the geothermal blades has a sheet-like structure, and each of the second blades 540 has a non-bending plate shape along the second bottom portion 544 to the second end 546, and each of the second blades 540 is from the first
  • the width from the bottom 544 to the second end 546 in the axial direction of the second wheel body 542 is gradually reduced, so that the rubber band 30 can be quickly detached from the second blade 540 after being ejected.
  • the resistance to the rubber band 30 is small.
  • each of the second vanes 540 is inclined along a bottom thereof toward a side away from the driven wheel 52.
  • Each of the second blades 540 is inclined along a side of the second bottom portion 544 to the second end 546 facing away from the driven wheel 52 to ensure the hook of the second blade 540 to the rubber band 30, The rubber band 30 is prevented from automatically falling off the second blade 540.
  • the driving device 60 is a steering gear fixedly mounted in the support base 44 and capable of receiving a control signal, the steering gear having an output shaft 62, the peeling
  • the mechanism includes a cord 80 for transmitting power generated by the steering gear to the driven wheel 52 and for stripping the rubber band 30 from the driven wheel 52 for launching, the string 80 Connected between the output shaft 62 and the driven wheel 52.
  • the driving force of the driven wheel 52 is provided by the steering gear.
  • One end of the wire 80 is wound around the output shaft 62 and the other end is wound around the driven wheel 52.
  • the driven wheel 52 is 52 Rotating to a certain position ⁇
  • the string 80 peels the rubber band 30 from the driven wheel 52, thereby enabling the rubber band 30 to be emitted.
  • the power outputted by the steering gear is transmitted to the driven wheel 52 by the rope 80, so that the driven and the reel 54 rotate with the output shaft 62, and the rubber band is driven. 30 turns.
  • the peeling mechanism further includes a wire shaft 92 protruding from the support base 44 , and the wire 80 is wound around the output shaft 62 .
  • the driven wheel 52 is disposed on the guiding shaft, and the wire shaft 92 is located between the driven wheel 52 and the output shaft 62, and in the height direction of the supporting base 44,
  • the wire shaft 92 is slightly higher than the driven wheel 52 and the output shaft 62, and the difference in height between the wire shaft 92 and the driven wheel 52 and the output shaft 62 is transferred to the wire shaft 9 2 attachment
  • the rubber band 30 is peeled off from the driven wheel 52.
  • the transmitting assembly 50 further includes a wire wheel 56 that rotates with the driven wheel 52 for guiding the wire 80.
  • the wire wheel 56 is sleeved. It is disposed on the fixing rod 55 and is close to the driven wheel 52.
  • the wire wheel 56 is mounted on the fixing rod 55 and rotates with the driven wheel 52 for guiding the rope 80.
  • the wire wheel 56 is integrally formed with the driven wheel 52.
  • the wire wheel 56 and the driven wheel 52 are respectively sleeved on the fixing rod 55 and are completely consistent during the rotation.
  • a gap 560 for accommodating the string 80 is formed between the driven wheel 52 and the wire wheel 56.
  • the slit 560 is formed between the driven wheel 52 and the wire wheel 56 to press one end of the wire 80 into the slit 560 such that the wire 80 is in the slave
  • the moving wheel 52 is disposed at a position where the radial direction of the driven wheel 52 is smaller than the radius of the driven wheel 52 to ensure that the driven wheel 52 rotates to be close to the guiding shaft accessory. 30 from the second The blade 540 is peeled off.
  • the wire wheel 56 protrudes in a circumferential direction thereof with a plurality of third blades 562 spaced apart from each other and corresponding to the first blade 520.
  • the bottom of the three blades 562 are disposed along the axial direction of the wire wheel 56, and each of the third blades 562 is curved along the bottom to the end thereof, and each of the third blades 562 is curved toward the same direction.
  • the number of the third blades 562 is the same as the number of the first blades 520, and the third blade 562 is disposed in a manner similar to that of the first blades 520.
  • the wire wheel 56 includes a third wheel body 564 that is sleeved on the fixing rod 55 and coaxial with the first wheel body 522, and each of the third blades 562 includes a third bottom portion 566 and a third end 568, A third bottom portion 566 is coupled to the third wheel body portion 564, and the third end portion 568 is a free end of the third blade 56 2 and away from the third bottom portion 566.
  • Each of the third blades 562 has a sheet-like structure, and each of the third blades 562 is curved along the third bottom portion 566 to the third end 568, and each of the third blades 562 is in the third shape.
  • each of the third vanes 562 has substantially the same axial width from the third bottom portion 566 to the third end portion 568 to the third wheel body portion 564.
  • the structure of each of the third blades 562 is not limited thereto, and each of the third blades 562 may also be a non-bending plate shape, so that the rubber bands 30 can be buckled.
  • the slit 560 is formed between the corresponding first blade 520 and the third blade 562, such that the wire 80 is pressed against the first blade 520 and the Between the third blades 562.
  • each of the third blades 562 is gradually reduced in width from the bottom to the end thereof in the axial direction of the wire wheel 56. And the width of each of the third blades 562 from the third bottom portion 566 to the third end portion 568 in the axial direction of the third wheel body portion 564 is gradually reduced, so that the rubber band 30 can be ejected. The detachment from the first blade 520 is quickly removed, and the retarding force against the rubber band 30 is reduced.
  • the peeling mechanism further includes a reel mounted on the output shaft 62 and rotated with the output shaft 62 for winding the string 80. 90.
  • a reel mounted on the output shaft 62 and rotated with the output shaft 62 for winding the string 80. 90.

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  • Aviation & Aerospace Engineering (AREA)
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Abstract

La présente invention concerne un dispositif de combat aérien pour un véhicule aérien sans pilote, utilisé dans un scénario dans lequel au moins deux véhicules aériens sans pilote effectuent des combats aériens, et une victoire ou une défaite est déterminée en fonction du nombre d'abattages de véhicules aériens sans pilote ou du nombre de véhicules aériens sans pilote abattus. Chaque véhicule aérien sans pilote comprend une cellule (10), et comprend un mécanisme de levage (20) et un dispositif de lancement de bande de caoutchouc (4) qui sont disposés sur la cellule (10). Une bande de caoutchouc (30) utilisée pour enrouler au moins un mécanisme de levage (20) dans un véhicule aérien sans pilote ennemi afin d'abattre le véhicule aérien sans pilote ennemi est disposée sur le dispositif de lancement de bande de caoutchouc (4). Le dispositif de lancement de bande de caoutchouc (4) comprend un ensemble base de montage (40) monté de manière fixe sur la cellule (10), un dispositif d'entraînement (60) monté de manière fixe sur l'ensemble base de montage (40) et utilisé pour recevoir un signal de lancement d'arme, et un ensemble de lancement (50) pour lancer la bande de caoutchouc (30) sous l'effet d'entraînement du dispositif d'entraînement (60). Selon le dispositif de combat aérien pour un véhicule aérien sans pilote, le dispositif de lancement de bande de caoutchouc (4) est monté sur chacun des véhicules aériens sans pilote participant à un combat aérien, et l'ensemble de lancement (50) est utilisé pour lancer la bande de caoutchouc (30) pour enrouler au moins un mécanisme de levage (20) dans le véhicule aérien sans pilote ennemi, de sorte que le mécanisme de levage (20) est amené à arrêter la rotation et le véhicule aérien sans pilote ennemi est poussé vers le sol, et la victoire ou la défaite du combat aérien est déterminée en calculant le nombre d'abattages de véhicules aériens sans pilote ou le nombre de véhicules aériens sans pilote abattus ; le dispositif de combat aérien pour un véhicule aérien sans pilote aide à abattre les véhicules aériens sans pilote ennemis, et le procédé présente un très bon effet de divertissement.
PCT/CN2016/084181 2016-05-31 2016-05-31 Dispositif de combat aérien et procédé pour véhicule aérien sans pilote Ceased WO2017206078A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201680000459.9A CN106061840B (zh) 2016-05-31 2016-05-31 无人机空战装置及方法
PCT/CN2016/084181 WO2017206078A1 (fr) 2016-05-31 2016-05-31 Dispositif de combat aérien et procédé pour véhicule aérien sans pilote

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Application Number Priority Date Filing Date Title
PCT/CN2016/084181 WO2017206078A1 (fr) 2016-05-31 2016-05-31 Dispositif de combat aérien et procédé pour véhicule aérien sans pilote

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WO2017206078A1 true WO2017206078A1 (fr) 2017-12-07

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Publication number Priority date Publication date Assignee Title
WO2017206081A1 (fr) * 2016-05-31 2017-12-07 深圳加创科技有限公司 Dispositif de lancement de bande de caoutchouc et véhicule aérien sans pilote
CN106683378A (zh) * 2016-12-30 2017-05-17 厦门安胜网络科技有限公司 一种无人机干扰方法及系统
CN106965931A (zh) * 2017-05-10 2017-07-21 佛山市神风航空科技有限公司 一种竞技用无人机
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