CN218839757U - Unmanned aerial vehicle bullet cabin and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle bullet cabin and unmanned aerial vehicle Download PDFInfo
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- CN218839757U CN218839757U CN202223235929.1U CN202223235929U CN218839757U CN 218839757 U CN218839757 U CN 218839757U CN 202223235929 U CN202223235929 U CN 202223235929U CN 218839757 U CN218839757 U CN 218839757U
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- 238000004891 communication Methods 0.000 claims description 19
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
The utility model relates to an unmanned aerial vehicle field discloses an unmanned aerial vehicle barrage and unmanned aerial vehicle, include: the device comprises a controller, an angle sensor, a motor, a lead screw with a connecting assembly and a magazine; wherein, the connecting component is connected with the magazine; the angle sensor is arranged at the magazine and connected with the controller to acquire inclination angle information of the magazine so as to be convenient for the controller to control the magazine; the controller is connected with the motor to generate a motor control instruction according to the projectile shooting instruction and the inclination angle information so as to control the motor to move; the motor sets up on unmanned aerial vehicle, and with screw connection to adjust coupling assembling position on the lead screw, thereby the launch angle of control barrage. Therefore, according to the technical scheme, the motor drives the screw rod to move so as to adjust the position of the connecting component on the screw rod, so that the launching angle of the missile bay is controlled, the accuracy of the launching angle is guaranteed through the angle sensor, and the unmanned aerial vehicle is guaranteed to be capable of sending the missile to a target point flexibly and accurately.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle aircraft field especially relates to an unmanned aerial vehicle capsule and unmanned aerial vehicle.
Background
With the increasing maturity of aircraft technology, unmanned aircraft are used in more and more fields (for example, military field, fire fighting field, police field, or criminal investigation field, etc.), such as: the unmanned aerial vehicle is used for launching fire extinguishing bombs to carry out fire extinguishing operation, and is used for spreading insecticide and the like. In order to reduce the equipment costs, the same drone is generally made to perform different tasks by varying the type of ammunition loaded in the cartridge bay of the drone.
At present unmanned aerial vehicle's bullet cabin is mostly the fixed bullet cabin of setting on the aircraft, and it only can launch the missile to the target point with fixed angle, when the target point position is special, may bring inconvenience for the transmission work of missile, influences unmanned aerial vehicle's normal work.
Therefore, how to provide an unmanned aerial vehicle bomb bay to enable an unmanned aerial vehicle to send a missile to a target point more flexibly and accurately is a problem which needs to be solved urgently by technical personnel in the field.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle bullet cabin and unmanned aerial vehicle to make unmanned aerial vehicle can with the more nimble accurate sending of missile to the target point, thereby improve the performance and the work efficiency of unmanned aerial vehicle operation.
In order to solve the technical problem, the application provides an unmanned aerial vehicle capsule, includes:
the device comprises a controller, an angle sensor, a motor, a lead screw with a connecting assembly and a magazine; wherein the connecting assembly is connected with the magazine;
the angle sensor is arranged at the magazine and connected with the controller to acquire inclination angle information of the magazine;
the controller is connected with the motor to generate a motor control instruction according to a missile throwing instruction and the inclination angle information so as to control the motor to move;
the motor sets up on unmanned aerial vehicle, and with screw connection, in order to adjust coupling assembling is in position on the lead screw, thereby control the launch angle of bullet case.
Preferably, the system further comprises a communication unit;
the controller is connected with the communication unit to acquire the projectile shooting instruction.
Preferably, the communication unit is a WiFi communication unit.
Preferably, the device further comprises a brake;
the brake is arranged at the first end of the motor to keep the shooting angle of the magazine.
Preferably, still include the capsule frame, the capsule frame is fixed in unmanned aerial vehicle is last, is used for accomodating the capsule.
Preferably, the motor sets up to include on unmanned aerial vehicle:
the motor is hinged with the magazine frame.
Preferably, the motor further comprises a speed reducer, and the speed reducer is connected with the second end of the motor.
Preferably, the connecting component is a nut arranged on the lead screw.
Preferably, the number of the magazine is at least 2.
In order to solve the technical problem, the application further provides an unmanned aerial vehicle, which comprises the unmanned aerial vehicle missile bay.
The application provides an unmanned aerial vehicle bullet cabin includes: the device comprises a controller, an angle sensor, a motor, a lead screw with a connecting assembly and a magazine; wherein, the connecting component is connected with the magazine; the angle sensor is arranged at the magazine and connected with the controller to acquire inclination angle information of the magazine so as to be convenient for the controller to control the magazine; the controller is connected with the motor to generate a motor control instruction according to the throwing instruction and the inclination angle information so as to control the motor to move; the motor sets up on unmanned aerial vehicle, and with lead screw connection to adjust coupling assembling position on the lead screw, thereby control the launch angle in bullet cabin. Therefore, according to the technical scheme provided by the application, the motor drives the screw rod to move so as to adjust the position of the connecting component on the screw rod, so that the launching angle of the missile cabin is controlled, the accuracy of the launching angle is guaranteed through the angle sensor, and the unmanned aerial vehicle is guaranteed to send the missile to a target point more flexibly and accurately.
In addition, this application still provides an unmanned aerial vehicle, including above-mentioned unmanned aerial vehicle bullet cabin, the effect is with the above.
Drawings
In order to illustrate the embodiments of the present invention more clearly, the drawings needed for the embodiments will be briefly described, it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained without inventive efforts.
Fig. 1 is a structural diagram of an unmanned aerial vehicle capsule provided in an embodiment of the present application;
fig. 2 is a schematic diagram of an unmanned aerial vehicle capsule working scene provided in an embodiment of the present application;
fig. 3 is a schematic view of another working scenario of a capsule of an unmanned aerial vehicle according to an embodiment of the present application;
the reference numbers are as follows: the device comprises a controller 1, an angle sensor 2, a motor 3, a screw rod 4, a connecting assembly 5, a bullet box 6, a brake 7 and a speed reducer 8.
Detailed Description
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, the ordinary skilled in the art can obtain all other embodiments without creative work, which all belong to the protection scope of the present invention.
The core of the utility model is to provide an unmanned aerial vehicle bullet cabin to make unmanned aerial vehicle can with the more nimble accurate sending of missile to the target point, thereby improve the performance and the work efficiency of unmanned aerial vehicle operation.
In order to make the technical field better understand the solution of the present invention, the following detailed description of the present invention is provided with reference to the accompanying drawings and the detailed description.
Fig. 1 is the structure diagram of an unmanned aerial vehicle barrage that this application embodiment provided, as shown in fig. 1, this unmanned aerial vehicle barrage includes:
the device comprises a controller 1, an angle sensor 2, a motor 3, a lead screw 4 with a connecting component 5 and a magazine 6; wherein, the connecting component 5 is connected with the bullet box 6; the angle sensor 2 is arranged at the magazine 6 and connected with the controller 1 to acquire inclination angle information of the magazine 6; the controller 1 is connected with the motor 3 to generate a motor 3 control instruction according to the projectile shooting instruction and the inclination angle information so as to control the motor 3 to move; motor 3 sets up on unmanned aerial vehicle, and is connected with lead screw 4 to adjust coupling assembling 5 position on lead screw 4, thereby control the launch angle in barrage.
It can be understood that controller 1 can be the treater of additional setting, also can multiplex unmanned aerial vehicle's treater, and this place is not restricted, chooses for use the latter scheme can show the reduction in equipment cost.
In specific implementation, the controller 1 determines the launch angle of the magazine 6 according to a shooting instruction, where the shooting instruction may be an instruction pre-stored in the controller 1, or an instruction received during the flight of the unmanned aerial vehicle, and is not limited herein. It can be understood that, in order to ensure that the launch angle of the magazine 6 is accurate, the inclination angle information of the magazine 6 needs to be collected by the angle sensor 2 and fed back to the controller 1, so that the controller 1 can adjust the angle of the magazine 6 in time. Wherein, angle sensor 2 can set up in the 6 departments of bullet case, confirms the 6 inclinations of bullet case through measuring the 6 orientation of bullet case and the contained angle of horizontal direction, also can set up in motor 3 department or lead screw department.
In specific implementation, when the controller 1 works, the controller 1 controls the motor 3 to move according to the missile throwing instruction and the inclination angle information, the motor 3 is connected with one end of the screw rod to drive the screw rod 4 to move, so that the relative position of the screw rod 4 and the connecting assembly 5 is changed, the bullet box 6 connected with the connecting assembly 5 is driven to move, and the inclination angle of the bullet box 6 is changed. Fig. 2 is a schematic diagram of a working scene of a missile bay of an unmanned aerial vehicle provided by an embodiment of the present application, and fig. 3 is a schematic diagram of another working scene of a missile bay of an unmanned aerial vehicle provided by an embodiment of the present application, as shown in fig. 2 or fig. 3, in an initial state (fig. 2), a missile box 6 is in a retracted state, and in a working state (fig. 3), the missile box 6 is driven by a connecting assembly 5 to be in an inclined state. The magazine 6 rotates to a post-rotation state as the actuator travels from an initial position to a maximum stroke at a constant speed. In a specific implementation, the connection assembly 5 may be a nut provided on the screw 4.
This embodiment provides an unmanned aerial vehicle capsule, includes: the device comprises a controller, an angle sensor, a motor, a lead screw with a connecting assembly and a magazine; wherein, the connecting component is connected with the magazine; the angle sensor is arranged at the magazine and connected with the controller to acquire inclination angle information of the magazine so as to be convenient for the controller to control the magazine; the controller is connected with the motor to generate a motor control instruction according to the throwing instruction and the inclination angle information so as to control the motor to move; the motor sets up on unmanned aerial vehicle, and with lead screw connection to adjust coupling assembling position on the lead screw, thereby control the launch angle in bullet cabin. Therefore, according to the technical scheme, the motor drives the screw rod to move so as to adjust the position of the connecting component on the screw rod, so that the launching angle of the missile bay is controlled, the accuracy of the launching angle is guaranteed through the angle sensor, and the unmanned aerial vehicle is guaranteed to be capable of sending the missile to a target point flexibly and accurately.
In a specific implementation, the missile applying instruction of the drone may be pre-stored in the controller 1 (for example, an operation point and an operation task are selected on a map in advance, and the drone performs the task according to the map by itself), or may be sent to the drone by a control person through the communication unit during the flight of the drone.
As a preferred embodiment, on the basis of the above embodiment, the unmanned aerial vehicle capsule further comprises a communication unit; the controller 1 is connected to a communication unit to acquire a projectile firing instruction. Generally, the wireless control signals of the unmanned aerial vehicle are divided into three categories: the communication mode of the unmanned aerial vehicle generally comprises radio communication, wiFi communication, operator network communication and the like. Furthermore, in consideration of the fact that the control instruction sent by the ground control personnel to the unmanned aerial vehicle comprises a task instruction, corresponding map information, route information and the like, and the data volume is large, a WiFi communication unit is selected as the communication unit. In specific implementation, the controller 1 receives a control instruction of an upper computer through a communication interface, collects inclination angle information returned by the angle sensor 2, generates a control signal through a control algorithm, sends the control signal to the driving circuit, controls the execution mechanism to output linear motion, and sends a real-time position signal of the execution mechanism to the upper computer through the communication interface.
In the concrete implementation, in order to guarantee the accuracy of unmanned aerial vehicle capsule launch angle, need to make unmanned aerial vehicle capsule can in time stop at angle adjustment in-process. In order to solve this problem, as a preferred embodiment, the unmanned aerial vehicle capsule further comprises a brake 7 and a speed reducer 8, wherein the brake 7 is arranged at the first end of the motor 3 to maintain the launch angle of the capsule. The brake 7 is arranged at the tail part of the motor 3, and when the brake 7 is selected, the brake force of the brake 7 is ensured to be larger than the maximum torque of the motor 3, so that self-locking is realized. To prevent inertia-induced inaccuracies in the adjustment of the orientation of the magazine. Further, in order to improve motor 3's angle modulation ability, the unmanned aerial vehicle barrage that this embodiment provided still includes reduction gear 8, and reduction gear 8 is connected with motor 3's second end.
In the concrete implementation, because unmanned aerial vehicle operational environment is more complicated, if the accident happens can lead to the magazine 6 breakage. On the basis of above-mentioned embodiment, the unmanned aerial vehicle single court still includes the capsule frame, and the capsule frame is fixed in on the unmanned aerial vehicle for accomodate the capsule. The magazine frame may be a steel frame structure, or may be a box lacking only the bottom surface and the front surface, which is not limited herein.
Further, in order to increase the movable dimension of unmanned aerial vehicle bomb bay to make unmanned aerial vehicle bomb bay more nimble, unmanned aerial vehicle bomb bay's motor 3 sets up specifically motor 3 and bomb bay frame hinge on unmanned aerial vehicle.
It will be appreciated that the greater the amount of ammunition loaded in the magazine, the greater the operational capacity of the drone and, therefore, at least 2 magazines 6 are included in each drone magazine.
In addition, this application still provides an unmanned aerial vehicle, including foretell unmanned aerial vehicle barrage. It can be understood that, in order to improve unmanned aerial vehicle's operational capability, can install a plurality of unmanned aerial vehicle barrages on unmanned aerial vehicle, each barrage can share same controller 1, also can set up a controller 1 for every barrage, does not do the restriction here.
The application provides an unmanned aerial vehicle, including foretell unmanned aerial vehicle cartridge bay, this unmanned aerial vehicle cartridge bay includes: the device comprises a controller, an angle sensor, a motor, a lead screw with a connecting assembly and a magazine; wherein, the connecting component is connected with the magazine; the angle sensor is arranged at the magazine and connected with the controller to acquire inclination angle information of the magazine so as to be convenient for the controller to control the magazine; the controller is connected with the motor to generate a motor control instruction according to the throwing instruction and the inclination angle information so as to control the motor to move; the motor sets up on unmanned aerial vehicle, and with screw connection to adjust coupling assembling position on the lead screw, thereby the launch angle of control barrage. Therefore, according to the technical scheme provided by the application, the motor drives the screw rod to move so as to adjust the position of the connecting component on the screw rod, so that the launching angle of the missile cabin is controlled, the accuracy of the launching angle is guaranteed through the angle sensor, and the unmanned aerial vehicle is guaranteed to send the missile to a target point more flexibly and accurately.
It is right above the utility model provides an unmanned aerial vehicle bullet cabin and unmanned aerial vehicle have carried out detailed introduction. The embodiments are described in a progressive manner in the specification, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other. The device disclosed by the embodiment corresponds to the method disclosed by the embodiment, so that the description is simple, and the relevant points can be referred to the method part for description. 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.
It is further noted that, in the present specification, 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. Also, 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. Without further limitation, an element defined by the phrase "comprising a … …" does not exclude the presence of another identical element in a process, method, article, or apparatus that comprises the element.
Claims (10)
1. An unmanned aerial vehicle capsule, comprising:
the device comprises a controller (1), an angle sensor (2), a motor (3), a lead screw (4) with a connecting component (5) and a magazine (6); wherein the connecting assembly (5) is connected with the magazine (6);
the angle sensor (2) is arranged at the magazine (6) and is connected with the controller (1) to acquire inclination angle information of the magazine (6);
the controller (1) is connected with the motor (3) to generate a motor (3) control instruction according to a throwing instruction and the inclination information so as to control the motor (3) to move;
motor (3) set up on unmanned aerial vehicle, and with lead screw (4) are connected, in order to adjust coupling assembling (5) are in position on lead screw (4), thereby control the launch angle of bullet case (6).
2. The unmanned aerial vehicle magazine of claim 1, further comprising a communication unit;
the controller (1) is connected with the communication unit to acquire the projectile shooting instruction.
3. The unmanned aerial vehicle capsule of claim 2, wherein the communication unit is a WiFi communication unit.
4. The unmanned aerial vehicle capsule of claim 1, further comprising a brake (7);
the brake (7) is arranged at the first end of the motor (3) to keep the shooting angle of the magazine (6).
5. The unmanned aerial vehicle capsule of claim 1, further comprising a capsule frame secured to the unmanned aerial vehicle for receiving the capsule.
6. The unmanned aerial vehicle capsule of claim 5, wherein the motor (3) disposed on the unmanned aerial vehicle comprises:
the motor (3) is hinged with the bullet cabin frame.
7. The unmanned aerial vehicle capsule of claim 1, further comprising a reducer (8), the reducer (8) being connected to a second end of the motor (3).
8. The unmanned aerial vehicle capsule according to any one of claims 1 to 7, wherein the connection assembly (5) is a nut provided on the lead screw (4).
9. Unmanned aerial vehicle capsule according to claim 1, characterized in that the number of said magazines (6) is at least 2.
10. A drone, comprising the drone pod of any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223235929.1U CN218839757U (en) | 2022-12-02 | 2022-12-02 | Unmanned aerial vehicle bullet cabin and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223235929.1U CN218839757U (en) | 2022-12-02 | 2022-12-02 | Unmanned aerial vehicle bullet cabin and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218839757U true CN218839757U (en) | 2023-04-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223235929.1U Active CN218839757U (en) | 2022-12-02 | 2022-12-02 | Unmanned aerial vehicle bullet cabin and unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN218839757U (en) |
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- 2022-12-02 CN CN202223235929.1U patent/CN218839757U/en active Active
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