CN218400970U - Self-destruction type attack unmanned aerial vehicle - Google Patents
Self-destruction type attack unmanned aerial vehicle Download PDFInfo
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- CN218400970U CN218400970U CN202223059295.9U CN202223059295U CN218400970U CN 218400970 U CN218400970 U CN 218400970U CN 202223059295 U CN202223059295 U CN 202223059295U CN 218400970 U CN218400970 U CN 218400970U
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Abstract
The utility model relates to a self-destruction attack unmanned aerial vehicle, including fuselage and remote control unit, the fuselage sets up flight module, control module and combat module, and the fuselage bilateral symmetry sets up a plurality of flight modules, and flight module includes motor and screw, and combat module includes grenade, cartridge carrier and unlocking device, and grenade sets up in the fuselage through cartridge carrier, and unlocking device sets up in cartridge carrier and unlocking device's action end is connected with the safety pin of grenade, and control module and unlocking device and motor communication are connected; the remote control equipment is in communication connection with the control module, the remote control equipment is used for a user to send a flight instruction and a combat instruction to the control module, and the control module is used for controlling the unlocking device to pull out a safety pin of the grenade when the combat instruction is obtained; it is visible through adopting the less grenade of volume, weight as killing the part, can realize unmanned aerial vehicle's miniaturized lightweight, makes its portable and use, reaches the purpose that provides quick convenient aerial striking means for first-line ground troops.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to unmanned aerial vehicle is attacked to self-destruction formula.
Background
The unmanned aerial vehicle size weight that is used for military striking at present is all great, and difficult transportation needs to distribute special haulage vehicle, and need be equipped with runway or dedicated firing equipment and just can take off, can't distribute to even rank ground army, makes a ray of ground army lack quick convenient aerial striking means.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is attacked to self-destruction formula to make it can miniaturize, lightweight, portable and use, thereby provide quick convenient aerial striking means for an ray of ground army.
In order to achieve the above object, the utility model provides a following technical scheme:
a self-destructing attacking drone, comprising:
the device comprises a machine body, wherein the machine body is provided with a flight module, a control module and a combat module, a plurality of flight modules are symmetrically arranged on two sides of the machine body, each flight module comprises a motor and a propeller, the propellers are arranged at the driving end of the motor, the combat module comprises a grenade, a grenade carrier and an unlocking device, the grenade is arranged on the machine body through the grenade carrier, the unlocking device is arranged on the grenade carrier, the action end of the unlocking device is connected with a safety pin of the grenade, and the control module is in communication connection with the unlocking device and the motor;
remote control unit, remote control unit with control module communication connection, remote control unit be used for the user to control module sends flight instruction and operation instruction, control module is used for acquireing control when the operation instruction unlocking device extracts the safety catch of grenade.
Optionally, unlocking device includes steering wheel, cam link mechanism and swing arm, the steering wheel set up in carry the bullet frame, the swing arm rotationally set up in carry the bullet frame, cam link mechanism's cam set up in the output of steering wheel, cam link mechanism's connecting rod keep away from the cam one end with the first end rotatable coupling of swing arm, the second end of swing arm with the safety pin rotatable coupling of grenade.
Optionally, the fuselage bilateral symmetry sets up a plurality of horn, the one end of horn rotationally set up in the fuselage, the horn can for the fuselage expandes and is first gesture, just the horn can for the fuselage draws in and is the second gesture, the horn with be provided with between the fuselage and be used for making the horn keeps the limit structure of first gesture, flight module with the horn one-to-one sets up, flight module set up in the horn is kept away from the one end of fuselage.
Optionally, the horn or the fuselage is provided with a landing gear.
Optionally, the undercarriage is rotatably disposed on the horn, the undercarriage is rotatable to a retracted position attached to the horn, and the undercarriage is rotatable to a support position where the horn satisfies a vertical condition.
Optionally, the body is further provided with an image acquisition module, the image acquisition module is in communication connection with the control module, and the remote control device is provided with a screen to display the image acquired by the image acquisition module.
Optionally, the image acquisition module includes an image recognition component, and the control module recognizes a target according to the image recognition component and controls the flight module to act so that the self-destruction attack unmanned aerial vehicle tracks the target.
Optionally, the fuselage still is provided with the ranging module, the ranging module with control module communication connection, the ranging module is used for measuring the distance of self-destruction formula attack unmanned aerial vehicle and target, control module is in the ranging module detects when the distance of self-destruction formula attack unmanned aerial vehicle and target is less than or equal to preset distance, to unlocking device sends the operation instruction or to remote control equipment feeds back.
Optionally, the body is further provided with a communication module, and the control module is in communication connection with the remote control device through the communication module.
Optionally, the fuselage still is provided with power module, power module respectively with the flight module, control module the operation module the image acquisition module, the range finding module and communication module electricity is connected.
According to the technical scheme, the utility model discloses a self-destruction attack unmanned aerial vehicle, this self-destruction attack unmanned aerial vehicle includes fuselage and remote control equipment, wherein, the fuselage sets up flight module, control module and combat module, the fuselage bilateral symmetry sets up a plurality of flight modules, flight module includes motor and screw, the screw sets up in the drive end of motor, each flight module is used for driving self-destruction attack unmanned aerial vehicle flight and move, combat module includes grenade, carry bullet rack and unlocking device, grenade passes through the bullet rack and sets up in the fuselage, unlocking device sets up in carrying the bullet rack and the action end of unlocking device is connected with the safety catch of grenade, control module and unlocking device and motor communication connection; the remote control equipment is in communication connection with the control module, the remote control equipment is used for a user to send a flight instruction and a combat instruction to the control module, and the control module is used for controlling the unlocking device to pull out a safety pin of the grenade when the combat instruction is obtained; when the self-destruction type attack unmanned aerial vehicle is applied, a user sends a signal to the control module through the remote control device to remotely control the flight module of the self-destruction type attack unmanned aerial vehicle to act so as to drive the self-destruction type attack unmanned aerial vehicle to fly, when the self-destruction type attack unmanned aerial vehicle flies to a preset distance away from a target, the preset distance L = the flight speed v x the delay time t of the grenade of the unmanned aerial vehicle, a combat instruction is sent to the control module through the remote control device or the control module can independently send the combat instruction so as to control the unlocking device to act to pull out the safety pin of the grenade, and therefore the self-destruction type attack is realized when the self-destruction type attack unmanned aerial vehicle flies to a target position; it is thus clear that above-mentioned self-destruction formula attacks unmanned aerial vehicle adopts grenade as killing parts, because of grenade volume, weight is less, consequently, allow to design less unmanned aerial vehicle platform, realize unmanned aerial vehicle's miniaturization, the lightweight, make it can hand-carry, need not to be equipped with special haulage vehicle, conveniently carry, and adopt many rotor structures, take off and need not with the help of runway or dedicated device of flying, can directly take off by hand, convenient to use, thereby reach the purpose that provides quick convenient aerial striking means for an ray of ground force army.
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 schematic structural diagram of a self-destruction attack unmanned aerial vehicle provided by an embodiment of the present invention;
fig. 2 is a schematic structural diagram of a combat module of the self-destruction attack unmanned aerial vehicle according to an embodiment of the present invention;
fig. 3 is a schematic view of an automatic tracking flight path of the self-destruction attack unmanned aerial vehicle provided by the embodiment of the present invention;
fig. 4 is the embodiment of the utility model provides an automatic tracking flight attitude adjustment schematic diagram of self-destruction formula attack unmanned aerial vehicle.
Wherein:
1 is a machine body; 2 is a machine arm; 3 is a motor; 4 is a propeller; 5 is a power supply module; 6 is a control module; 7 is a communication module; 8 is a combat module; 810 is a missile carrier; 820 is a grenade; 821 is a safety pin; 830 is an unlocking device; 831 is a steering engine; 832 is a cam; 833 is a connecting rod; 834 is a swing arm; 9 is an image acquisition module; reference numeral 10 denotes a landing gear.
Detailed Description
The core of the utility model is to provide a self-destruction formula attacks unmanned aerial vehicle, this self-destruction formula attacks unmanned aerial vehicle structural design and makes it can miniaturize, lightweight, portable and use to provide quick convenient aerial striking means for an ray of ground troops.
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in 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 belong to the protection scope of the present invention.
Please refer to fig. 1 and fig. 2, fig. 1 is a schematic structural diagram of a self-destruction type unmanned aerial vehicle, and fig. 2 is a schematic structural diagram of a combat module of a self-destruction type unmanned aerial vehicle.
The embodiment of the utility model provides an in disclose an unmanned aerial vehicle is attacked to self-destruction formula, this unmanned aerial vehicle is attacked to self-destruction formula includes fuselage 1 and remote control equipment.
The unmanned aerial vehicle comprises a fuselage 1, a control module 6 and a combat module 8, wherein a plurality of flight modules are symmetrically arranged on two sides of the fuselage 1, each flight module comprises a motor 3 and a propeller 4, the propellers 4 are arranged at the driving end of the motors 3, each flight module is used for driving a self-destruction type attack unmanned aerial vehicle to fly and move, each combat module 8 comprises a grenade 820, a grenade carrier 810 and an unlocking device 830, the grenade 820 is arranged on the fuselage 1 through the grenade carrier 810, the unlocking device 830 is arranged on the grenade carrier 810, the action end of the unlocking device 830 is connected with a safety pin 821 of the grenade 820, and the control module 6 is in communication connection with the unlocking device 830 and the motors 3; the remote control device is in communication connection with the control module 6, the remote control device is used for a user to send a flight instruction and a combat instruction to the control module 6, and the control module 6 is used for controlling the unlocking device 830 to pull out the safety pin 821 of the grenade 820 when the combat instruction is obtained.
Compared with the prior art, the embodiment of the utility model provides a self-destruction type attack unmanned aerial vehicle is when using, the user sends the flight module action of signal remote control self-destruction type attack unmanned aerial vehicle to control module 6 through remote control equipment and drives the flight of self-destruction type attack unmanned aerial vehicle, when self-destruction type attack unmanned aerial vehicle flies to the predetermined distance apart from the target, predetermined distance L = unmanned aerial vehicle flight speed v x grenade 820 delay time t, grenade 820 delay time t is the self parameter of grenade 820, generally between 8 seconds-15 seconds, the mode of delay detonation is known technology, can adopt different modes such as electronic timer, built-in fuse cord to realize, do not restrict here, send the operation instruction to control module 6 through remote control equipment or control module 6 can send the operation instruction independently, extract the safety pin 821 of grenade 820 with control unlocking device 830 action, thereby realize self-destruction type attack when self-destruction type attack flies to the target position; it is thus clear that above-mentioned self-destruction formula attacks unmanned aerial vehicle adopts grenade 820 as the killer part, because of grenade 820 volume, weight is less, consequently, allow the design less unmanned aerial vehicle platform, realize unmanned aerial vehicle's miniaturization, the lightweight, make it can hand-carry, need not to be equipped with special haulage vehicle, conveniently carry, and adopt many rotor structures, take off and need not with the help of runway or dedicated device of flying away, can directly take off by hand, convenient to use, thereby reach the purpose that provides quick convenient aerial striking means for an ray of ground force army.
As shown in fig. 2, specifically, in the embodiment of the present invention, the unlocking device 830 includes a steering engine 831, a cam link mechanism and a swing arm 834, the steering engine 831 is disposed in the missile carrying frame 810, the swing arm 834 is rotatably disposed in the missile carrying frame 810, the cam link mechanism includes a cam 832 and a connecting rod 833, one end of the connecting rod 833 is rotatably connected to the cam 832, the cam 832 of the cam link mechanism is disposed at an output end of the steering engine 831, one end of the connecting rod 833 of the cam link mechanism, which is far away from the cam 832, is rotatably connected to a first end of the swing arm 834, a second end of the swing arm 834 is rotatably connected to a safety pin 821 of the grenade 820, when the steering engine 831 rotates, the cam link mechanism drives the swing arm 834 to rotate, so as to extract the safety pin 821 of the grenade 820.
As shown in fig. 1, in the embodiment of the utility model provides an, 1 bilateral symmetry of fuselage sets up a plurality of horn 2, the one end of horn 2 rotationally sets up in fuselage 1, horn 2 can expand for fuselage 1 and be first gesture, and horn 2 can draw in for fuselage 1 and be the second gesture, be provided with the limit structure who is used for making horn 2 keep first gesture between horn 2 and the fuselage 1, flight module sets up with horn 2 one-to-one, flight module sets up in the one end that fuselage 1 was kept away from to horn 2, through the structure, when carrying above-mentioned self-destruction formula attack unmanned aerial vehicle, can draw in above-mentioned each horn 2 to fuselage 1 to the second gesture, in order to reduce the volume that self-destruction formula attacked unmanned aerial vehicle, and is convenient to carry, when using, can make horn 2 open to first gesture, so as to fly.
Further optimize above-mentioned technical scheme, in the embodiment of the utility model provides an, above-mentioned horn 2 or fuselage 1 are provided with undercarriage 10.
Specifically, as shown in fig. 1, above-mentioned undercarriage 10 rotationally sets up in horn 2, and undercarriage 10 can rotate to the retracting position with the horn 2 laminating, and undercarriage 10 can rotate and satisfy the support position of vertical condition for horn 2, when needs use this self-destruction formula attack unmanned aerial vehicle, the user can expand undercarriage 10 to support position from retracting position to in order to place self-destruction formula attack unmanned aerial vehicle steadily on ground.
In order to carry out the remote control to self-destruction formula attack unmanned aerial vehicle for the sake of convenience, in the embodiment of the utility model, above-mentioned fuselage 1 still is provided with image acquisition module 9, image acquisition module 9 includes one or more camera, image acquisition module 9 and control module 6 communication connection, remote control unit sets up the screen in order to show the image that image acquisition module 9 gathered, the whole self-destruction formula of shooing of each camera attacks unmanned aerial vehicle the place ahead image, and real-time transmission to the remote control unit on ground, ground control personnel are according to the image of gathering, attack unmanned aerial vehicle to self-destruction formula and control.
Further optimize above-mentioned technical scheme the embodiment of the utility model provides an in, above-mentioned image acquisition module 9 includes the image recognition subassembly, and control module 6 is according to image recognition subassembly discernment target and control flight module action so that the unmanned aerial vehicle tracking target is attacked to the self-destruction formula.
Based on above-mentioned image acquisition module 9 and image recognition subassembly, can carry out automatic or manual form's control to unmanned aerial vehicle. In a manual mode, aiming marks such as crosses and circles are generated in the center of a screen of the remote control device corresponding to the position right in front of the self-destruction type attack unmanned aerial vehicle, an operator controls the self-destruction type attack unmanned aerial vehicle to move up and down, left and right in the flying process of the self-destruction type attack unmanned aerial vehicle, the aiming marks are kept to be always aligned with a target, and the self-destruction type attack unmanned aerial vehicle can keep flying towards the target; in an automatic mode, after the self-destruction type attack unmanned aerial vehicle is aligned to a target, an operator presses a locking button, the self-destruction type attack unmanned aerial vehicle can identify the target through an image identification component, automatically tracks the target through a corresponding image identification algorithm, controls a flight module to adjust the flight track of the self-destruction type attack unmanned aerial vehicle, keeps the target located right in front of the self-destruction type attack unmanned aerial vehicle, and the corresponding image identification and target tracking algorithm is a disclosed technology and is not limited herein.
In the automatic mode, as shown in fig. 3, the relative angle θ between the flight axis of the aircraft and the target and the distance D from the target are calculated in real time. Preferably, the self-destruction attack unmanned aerial vehicle can turn to the target according to a circular arc track, and the radius of the circular arc is r = (D/2)/sin theta.
As shown in fig. 4, the self-destruction unmanned drone can calculate the roll angle β of the fuselage 1 and the tension T of each rotor according to the following formula (T is the tension of each rotor alone): tsin β = mg/4, tcos β = mv 2 And v (4 r), wherein m is the weight of the unmanned aerial vehicle, and g is the gravity acceleration, so that the flight attitude of the self-destruction type attacking unmanned aerial vehicle can be adjusted conveniently.
As preferably, in the utility model discloses can the embodiment, above-mentioned fuselage 1 still is provided with the ranging module, ranging module and control module 6 communication connection, and the ranging module is used for measuring the distance that self-destruction formula attacked unmanned aerial vehicle and target, and control module 6 sends the operation instruction or feeds back to remote control equipment to unlocking device 830 when ranging module detects that the distance that self-destruction formula attacked unmanned aerial vehicle and target is less than or equal to and predetermines distance L.
Specifically, the ranging module measures the distance D between the self-destruction attack unmanned aerial vehicle and the target, when the distance D between the self-destruction attack unmanned aerial vehicle and the target is measured, and the flying speed v of the unmanned aerial vehicle meets t 1 = D ÷ v, when t 1 When t is less than or equal to t, namely D is less than or equal to L, a signal is sent to the remote control equipment or the unlocking device 830, and the user passes through the remote control equipmentThe unlocking means 830 are activated manually or automatically by the control module 6. The distance measuring module includes, but is not limited to, a laser distance meter and an image distance meter, and the manner of measuring the distance by the distance measuring module is known in the art and is not limited herein.
Further optimize above-mentioned technical scheme, in the embodiment of the utility model provides an, as shown in fig. 1, above-mentioned fuselage 1 still is provided with communication module 7, and control module 6 passes through communication module 7 and remote control unit communication connection.
As shown in fig. 1, the fuselage 1 is further provided with a power module 5, and the power module 5 is electrically connected with the flight module, the control module 6, the operation module 8, the image acquisition module 9, the distance measurement module and the communication module 7 respectively to supply power to the flight module, the control module 6, the operation module 8, the image acquisition module 9, the distance measurement module and the communication module 7.
It should be noted that, in the present specification, the embodiments are all described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments may be referred to each other.
It should be understood that the use of "system," "device," "unit," and/or "module" herein is merely one way to distinguish between different components, elements, components, parts, or assemblies of different levels. However, other words may be substituted by other expressions if they accomplish the same purpose.
As used in this application and the appended claims, the terms "a," "an," "the," and/or "the" are not intended to be inclusive in the singular, but rather are intended to be inclusive in the plural unless the context clearly dictates otherwise. In general, the terms "comprises" and "comprising" are intended to cover only the explicitly identified steps or elements as not constituting an exclusive list and that the method or apparatus may comprise further steps or elements. An element defined by the phrase "comprising a … …" does not exclude the presence of additional identical elements in a process, method, article, or apparatus that comprises the element.
Wherein in the description of the embodiments of the present application, "/" indicates an inclusive meaning, for example, a/B may indicate a or B; "and/or" herein is merely an association describing an associated object, and means that there may be three relationships, e.g., a and/or B, which may mean: a exists alone, A and B exist simultaneously, and B exists alone. In addition, in the description of the embodiments of the present application, "a plurality" means two or more than two.
In the following, the terms "first", "second" are used for descriptive purposes only and are not to be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature.
If used in this application, the flowcharts are intended to illustrate operations performed by the system according to embodiments of the present application. It should be understood that the preceding or following operations are not necessarily performed in the exact order in which they are performed. Rather, the various steps may be processed in reverse order or simultaneously. Meanwhile, other operations may be added to the processes, or a certain step or several steps of operations may be removed from the processes.
It is also noted that, in this document, terms such as "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that an 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 article or apparatus. Without further limitation, an element defined by the phrase "comprising a … …" does not exclude the presence of another identical element in an article or apparatus that comprises the element.
The principles and embodiments of the present invention have been explained herein using specific examples, and the above descriptions of the embodiments are only used to help understand the core concepts of the present invention. It should be noted that, for those skilled in the art, without departing from the principle of the present invention, the present invention can be further modified and modified, and such modifications and modifications also fall within the protection scope of the appended claims.
Claims (10)
1. The utility model provides a self-destruction formula attack unmanned aerial vehicle which characterized in that includes:
the device comprises a machine body, wherein the machine body is provided with a flight module, a control module and a combat module, a plurality of flight modules are symmetrically arranged on two sides of the machine body, each flight module comprises a motor and a propeller, the propellers are arranged at the driving end of the motor, the combat module comprises a grenade, a grenade carrier and an unlocking device, the grenade is arranged on the machine body through the grenade carrier, the unlocking device is arranged on the grenade carrier, the action end of the unlocking device is connected with a safety pin of the grenade, and the control module is in communication connection with the unlocking device and the motor;
remote control equipment, remote control equipment with control module communication connection, remote control equipment be used for supplying the user to control module sends flight instruction and operation instruction, control module is used for acquireing control when the operation instruction unlocking device extracts the safety catch of grenade.
2. The unmanned aerial vehicle is attacked to self-destruction formula of claim 1, characterized in that, unlocking device includes steering wheel, cam link mechanism and swing arm, the steering wheel set up in the missile carrying frame, the swing arm rotationally set up in the missile carrying frame, cam link mechanism's cam set up in the output of steering wheel, cam link mechanism's connecting rod keep away from the one end of cam with the first end rotatable coupling of swing arm, the second end of swing arm with the safety pin rotatable coupling of grenade.
3. The unmanned aerial vehicle is attacked to self-destruction formula of claim 1, characterized in that, the fuselage bilateral symmetry sets up a plurality of horn, the one end of horn rotationally set up in the fuselage, the horn can expand for the fuselage and be first gesture, just the horn can for the fuselage draws in and is the second gesture in, the horn with be provided with between the fuselage and be used for making the horn keeps the limit structure of first gesture, flight module with the horn one-to-one sets up, flight module set up in the horn is kept away from the one end of fuselage.
4. The unmanned self-destructing attack aerial vehicle according to claim 3, wherein the horn or the fuselage is provided with a landing gear.
5. The unmanned self-destructive attack vehicle according to claim 4, wherein the undercarriage is rotatably disposed on the horn, the undercarriage is rotatable to a retracted position in which the undercarriage fits the horn, and the undercarriage is rotatable to a support position in which the horn satisfies a vertical condition.
6. The unmanned aerial vehicle of any one of claims 1-5, wherein the fuselage is further provided with an image acquisition module, the image acquisition module is in communication with the control module, and the remote control device is provided with a screen to display images acquired by the image acquisition module.
7. The unmanned self-destructive attack system according to claim 6, wherein the image acquisition module comprises an image recognition component, and the control module recognizes a target according to the image recognition component and controls the flight module to act so that the unmanned self-destructive attack system tracks the target.
8. The unmanned aerial vehicle is attacked to self-destruction formula of claim 6, characterized in that, the fuselage still is provided with range finding module, range finding module with control module communication connection, range finding module is used for measuring the distance of unmanned aerial vehicle is attacked to self-destruction formula and target, control module is when range finding module detects that the distance of unmanned aerial vehicle is attacked to self-destruction formula and target is less than or equal to preset distance, to unlocking device sends out the operation instruction or to remote control equipment feeds back.
9. The unmanned aerial vehicle is attacked to self-destruction formula according to claim 8, characterized in that, the fuselage still is provided with communication module, control module through communication module with remote control equipment communication connection.
10. The unmanned aerial vehicle is attacked to self-destruction formula of claim 9, characterized in that, the fuselage still is provided with power module, power module respectively with the flight module, control module, operation module, image acquisition module, range module and communication module electricity are connected.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202223059295.9U CN218400970U (en) | 2022-11-17 | 2022-11-17 | Self-destruction type attack unmanned aerial vehicle |
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| CN202223059295.9U CN218400970U (en) | 2022-11-17 | 2022-11-17 | Self-destruction type attack unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL304352B1 (en) * | 2023-07-10 | 2024-07-01 | Convex Designed Eng Ltd | A system and a method for safe and remote activation of a grenade |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL304352B1 (en) * | 2023-07-10 | 2024-07-01 | Convex Designed Eng Ltd | A system and a method for safe and remote activation of a grenade |
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