CN215205419U

CN215205419U - Device based on unmanned vehicle platform launches unmanned aerial vehicle bee colony

Info

Publication number: CN215205419U
Application number: CN202121317569.2U
Authority: CN
Inventors: 胡中强; 王凯; 吴辉喜; 孙建峰; 卢凡
Original assignee: Haichuang Feilong Fujian Technology Co ltd
Current assignee: Haichuang Feilong Fujian Technology Co ltd
Priority date: 2021-06-11
Filing date: 2021-06-11
Publication date: 2021-12-17
Anticipated expiration: 2031-06-11

Abstract

The utility model discloses a device based on unmanned aerial vehicle platform transmission unmanned aerial vehicle bee colony, including unmanned aerial vehicle platform, bottom plate and backup pad, the backup pad sets up on a pair of leading truck of bottom plate, just the backup pad passes through cylinder control drive on the bottom plate, wherein, be equipped with an adjustment mechanism in the backup pad, adjustment mechanism includes electric putter, hinge bar, regulating plate and buffering subassembly, the hinge bar with electric putter's output is articulated, the buffering subassembly sets up in the mounting groove of backup pad. The utility model discloses can adjust the angle of launching platform before the transmission for location when unmanned aerial vehicle bee colony launches is more accurate.

Description

Device based on unmanned vehicle platform launches unmanned aerial vehicle bee colony

Technical Field

The utility model relates to an unmanned air vehicle technique field, concretely relates to device based on unmanned vehicle platform transmission unmanned aerial vehicle bee colony.

Background

Many unmanned aerial vehicles are behind forming the formation, when flying to the destination, can receive various air current influences, these influences derive from the weather conditions of nature, more come from unmanned aerial vehicle self among the formation vortex influence, this moment under the influence of various factors, unmanned aerial vehicle formation can take place various changes, in order to make unmanned aerial vehicle can adapt to self place environment more, still can keep good formation in the face of the influence of different environment, just need to introduce formation and keep the mechanism, the stability of formation is kept all the time. But current unmanned aerial vehicle bee colony transmission platform need adjust emission angle before the transmission, but current technique can not adjust the angle of transmission platform, has played certain hindrance to the transmission.

SUMMERY OF THE UTILITY MODEL

In view of this, the utility model provides a device based on unmanned vehicle platform transmission unmanned aerial vehicle bee colony to solve above-mentioned technical problem.

In order to achieve the above object, the utility model provides a following technical scheme:

an apparatus for launching drone swarm based on a drone vehicle platform, comprising:

an unmanned vehicle platform;

a base plate mounted on the unmanned vehicle platform;

the supporting plates are arranged on the pair of guide frames of the bottom plate and are driven by the cylinders on the bottom plate in a control mode;

wherein, be equipped with an adjustment mechanism in the backup pad, adjustment mechanism includes electric putter, hinge bar, regulating plate and buffer unit, electric putter articulates the upper end of backup pad, the regulating plate articulates the right-hand member of backup pad, the hinge bar with the lower extreme rigid coupling of regulating plate, just the hinge bar with electric putter's output is articulated, buffer unit sets up in the mounting groove of backup pad, just buffer unit's upper end with hinge bar's lower extreme is articulated.

Further, the buffer assembly comprises a cylinder, a piston rod and a piston, the cylinder is arranged in the mounting groove, the piston is connected with the inner wall of the cylinder in a sliding mode, and the piston rod is fixedly connected with the piston.

Furthermore, the upper end of the piston rod penetrates through the cylinder cover of the cylinder body and extends upwards, and the upper end of the piston rod is hinged with the lower end of the hinge rod.

Furthermore, a pair of buffer springs is arranged in the cylinder, and two ends of each buffer spring are respectively pressed between the piston and the inner bottom wall of the cylinder.

Furthermore, a connecting plate is embedded in the hinge rod and hinged with the output end of the electric push rod.

Furthermore, a launching box is installed on the adjusting plate.

Furthermore, the pair of guide frames are respectively movably arranged on the guide posts corresponding to the bottom plate, the guide posts are sleeved with a compression spring, and two ends of the compression spring are respectively pressed between the guide frames and the guide posts.

According to the above technical solution, the utility model has the advantages that: the utility model discloses can adjust the angle of launching platform before the transmission for location when unmanned aerial vehicle bee colony launches is more accurate.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this application, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification.

Fig. 1 is a schematic structural diagram of the present invention.

Fig. 2 is a partially enlarged view of a portion a of fig. 1.

Fig. 3 is a partially enlarged view of fig. 2 at B.

Fig. 4 is the utility model discloses an unmanned aerial vehicle bee colony's spatial structure schematic diagram.

Figure 5 is the utility model discloses an elevation view of unmanned aerial vehicle bee colony.

Fig. 6 is the utility model discloses an unmanned aerial vehicle bee colony does not expand the spatial structure sketch map of formula.

List of reference numerals: the unmanned vehicle comprises an unmanned vehicle platform 1, a bottom plate 2, a guide frame 3, a compression spring 31, a guide post 32, a cylinder 4, a supporting plate 5, a mounting groove 51, an adjusting mechanism 6, an electric push rod 61, a hinge rod 62, a connecting plate 63, an adjusting plate 64, a cylinder 65, a cylinder cover 651, a piston rod 66, a piston 67, a buffer spring 68, a launching box 7, a cylindrical top body 10, a flight control system 20, an electric regulator 21, a flight blade 22, a GPS module 30, a driving motor 40, a quick release mechanism 50, a micro camera 60 and an intelligent battery 70.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the following embodiments and accompanying drawings. The exemplary embodiments and descriptions of the present invention are provided to explain the present invention, but not to limit the present invention.

Referring to fig. 1 to 6, the device for launching drone swarm based on the unmanned vehicle platform shown in fig. 1 and 2 is composed of an unmanned vehicle platform 1, a bottom plate 2 and a support plate 5, wherein the bottom plate 2 is installed on the unmanned vehicle platform 1; the supporting plates 5 are arranged on a pair of guide frames 3 of the bottom plate 2, and the supporting plates 5 are driven by a cylinder 4 on the bottom plate 2; wherein, be equipped with an adjustment mechanism 6 on the backup pad 5, adjustment mechanism 6 includes electric putter 61, hinge bar 62, regulating plate 64 and buffer unit, electric putter 61 articulates the upper end of backup pad 5, regulating plate 64 articulates the right-hand member of backup pad 5, hinge bar 62 with the lower extreme rigid coupling of regulating plate 64, just hinge bar 62 with electric putter 61's output is articulated, buffer unit sets up in the mounting groove 51 of backup pad 5, just buffer unit's upper end with hinge bar 62's lower extreme is articulated.

Preferably, the buffering component comprises a cylinder 65, a piston rod 66 and a piston 67, the cylinder 65 is arranged in the mounting groove 51, the piston 67 is connected with the inner wall of the cylinder 65 in a sliding manner, and the piston rod 66 is fixedly connected with the piston 67.

Preferably, the upper end of the piston rod 66 penetrates through the cover 651 of the cylinder 65 and extends upward, and the upper end of the piston rod 66 is hinged to the lower end of the hinge rod 62.

As shown in fig. 3, a pair of buffer springs 68 are disposed in the cylinder 65, and both ends of the pair of buffer springs 68 are respectively pressed between the piston 67 and the inner bottom wall of the cylinder 65. With the above structure, when the piston 67 moves downward, the buffer spring 68 is compressed, and a good buffer effect is achieved in the whole adjusting process of the adjusting plate 64.

Preferably, a connecting plate 63 is embedded in the hinge rod 63, and the connecting plate 63 is hinged to the output end of the electric push rod 61.

Preferably, the adjusting plate 64 is provided with a transmitting box 7.

Preferably, the pair of guide frames 3 are movably disposed on guide posts 32 corresponding to the bottom plate 2, the guide posts 32 are sleeved with a compression spring 31, and two ends of the compression spring 31 respectively press against between the guide frames 3 and the guide posts 32.

The working principle is as follows: as shown in fig. 4, 5 and 6, when the aircraft is thrown by hand or on a mother aircraft, the intelligent battery 70 is started by remote control to enable the driving motor 40 to work, the flight blades 22 on the flight system 20 are rapidly unfolded, the flight blades 22 are locked by the quick release structure 50 to prevent shaking and resonance in flight, the orientation of the flight blades 22 is determined by adjusting the electric controller 21, and meanwhile, the flight control system realizes the stable flight attitude of the submachine in the air by positioning through the GPS module 30 in the cylindrical top body 10, calculating the flight algorithm and the like, so that the submachine can be controlled by the flyers, and can be shot by the micro camera 60; before launching, the output end of the air cylinder 4 is controlled to move upwards to enable the support plate 5 to move upwards, and then the support plate stops moving upwards after moving to a specified height, in the process of moving upwards, the guide frame 3 extrudes the compression spring 31 to enable the compression spring 31 to be compressed, good buffering performance is achieved in the moving process of the support plate 5, at the moment, the electric push rod 61 is controlled to drive the hinge rod 62 to move, the adjusting plate 64 is driven to rotate, the angle of the launching box 7 is adjusted, the hinge rod 62 drives the piston rod 66 at the lower end to move when moving, the piston 67 moves downwards to enable the buffer spring 68 to be compressed, and a good buffering effect is achieved in the whole adjusting process of the adjusting plate 64; to sum up, the utility model discloses can adjust the angle of transmission platform before the transmission for location when unmanned aerial vehicle bee colony launches is more accurate.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not intended to limit the present invention, and it will be apparent to those skilled in the art that various modifications and variations can be made in the embodiments of the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides a device based on unmanned vehicle platform transmission unmanned aerial vehicle bee colony which characterized in that includes:

an unmanned vehicle platform (1);

the bottom plate (2), the bottom plate (2) is installed on the unmanned vehicle platform (1);

the supporting plates (5) are arranged on the pair of guide frames (3) of the bottom plate (2), and the supporting plates (5) are controlled and driven by cylinders (4) on the bottom plate (2);

wherein, be equipped with an adjustment mechanism (6) on backup pad (5), adjustment mechanism (6) include electric putter (61), hinge bar (62), regulating plate (64) and buffering subassembly, electric putter (61) articulate the upper end of backup pad (5), regulating plate (64) articulate the right-hand member of backup pad (5), hinge bar (62) with the lower extreme rigid coupling of regulating plate (64), just hinge bar (62) with the output of electric putter (61) is articulated, the buffering subassembly sets up in mounting groove (51) of backup pad (5), just the upper end of buffering subassembly with the lower extreme of hinge bar (62) is articulated.

2. The unmanned aerial vehicle bee colony launching device based on the unmanned aerial vehicle platform of claim 1, wherein the buffering component comprises a cylinder (65), a piston rod (66) and a piston (67), the cylinder (65) is arranged in the mounting groove (51), the piston (67) is in sliding connection with the inner wall of the cylinder (65), and the piston rod (66) is fixedly connected with the piston (67).

3. The drone swarm launcher based on the drone platform of claim 2, wherein the upper end of the piston rod (66) protrudes upwards through a cylinder cover (651) of the cylinder (65), and the upper end of the piston rod (66) is hinged with the lower end of the hinge rod (62).

4. The drone swarm launching device based on the drone vehicle platform as claimed in claim 3, wherein a pair of buffer springs (68) are arranged in the cylinder (65), and two ends of the pair of buffer springs (68) are respectively pressed between the piston (67) and the inner bottom wall of the cylinder (65).

5. The drone swarm launcher based on the drone vehicle platform according to claim 4, characterized in that a connecting plate (63) is embedded in the hinge rod (62), and the connecting plate (63) is hinged to the output end of the electric push rod (61).

6. The drone swarm launcher based on the drone vehicle platform according to claim 5, characterized in that the regulating plate (64) has a launch box (7) mounted thereon.

7. The unmanned aerial vehicle platform-based unmanned aerial vehicle swarm launching device according to claim 1, wherein a pair of guide frames (3) are movably arranged on guide pillars (32) corresponding to the bottom plate (2), the guide pillars (32) are sleeved with a compression spring (31), and two ends of the compression spring (31) are respectively pressed between the guide frames (3) and the guide pillars (32).