CN215205367U

CN215205367U - Handheld throwing type unmanned aerial vehicle for individual soldier

Info

Publication number: CN215205367U
Application number: CN202121317995.6U
Authority: CN
Inventors: 卢凡; 卢思成; 刘中玲; 阮梅仙; 黎绿英
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 hand-held throwing type unmanned aerial vehicle for individual soldiers, which comprises an unmanned aerial vehicle main body and a plurality of supporting plates; an anti-collision mechanism is arranged between the unmanned aerial vehicle main body and the supporting plate, the anti-collision mechanism comprises an anti-collision barrel, a guide rail slider mechanism, a first anti-collision part and a second anti-collision part, and the anti-collision barrel is fixed at the bottom of the unmanned aerial vehicle main body; the guide rail sliding block mechanism is accommodated in the anti-collision barrel and is fixedly connected with the supporting legs of the supporting plate; the first anti-collision part is arranged in a first buffer cavity of the anti-collision barrel and can be abutted against the upper end of the guide rail sliding block mechanism; the second anti-collision part is arranged in a second buffer cavity of the anti-collision barrel body and is abutted against the inner part of the guide rail sliding block mechanism. The utility model is not only simple in operation, it is swift convenient to use to possess very strong security when using.

Description

Handheld throwing type unmanned aerial vehicle for individual soldier

Technical Field

The utility model relates to an anticollision institution, concretely relates to formula unmanned aerial vehicle is thrown in handheld of individual soldier.

Background

Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than for airplanes that are piloted by humans. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology. But current unmanned aerial vehicle is when landing because the bottom lacks protection machanism for thereby the unmanned aerial vehicle bottom easily produces the friction with ground and damages.

SUMMERY OF THE UTILITY MODEL

In view of this, the utility model provides a formula unmanned aerial vehicle is thrown in handheld of individual soldier to solve above-mentioned technical problem.

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

an individual soldier hand-held jettisoning drone, comprising:

a body of a human-machine;

a plurality of support plates;

wherein, the unmanned aerial vehicle main part with be equipped with an anticollision institution between the backup pad, anticollision institution includes:

the anti-collision barrel is fixed at the bottom of the unmanned aerial vehicle main body;

the guide rail sliding block mechanism is accommodated in the anti-collision barrel and is fixedly connected with the supporting legs of the supporting plate;

the first anti-collision part is arranged in a first buffer cavity of the anti-collision barrel and can be abutted against the upper end of the guide rail sliding block mechanism;

and the second anti-collision part is arranged in a second buffer cavity of the anti-collision barrel body and is abutted against the inner part of the guide rail sliding block mechanism.

Further, guide rail slider mechanism includes guide rail, slider and arch, the guide rail is installed on the inner wall of anticollision barrel, the slider with the inner wall sliding connection of guide rail, just the slider with the upper end rigid coupling of supporting leg, the arch with slider formula structure as an organic whole.

Furthermore, the first anti-collision part comprises a pair of connecting pieces, an upper elastic pad and a pair of first compression springs, the upper elastic pad is fixedly connected with the inner top wall of the anti-collision barrel, the pair of connecting pieces are installed in the upper elastic pad, the connecting pieces penetrate through the upper elastic pad and extend downwards, and the pair of first compression springs are connected to the lower ends of the corresponding connecting pieces.

Furthermore, the upper end of the sliding block is fixedly connected with a top block.

Furthermore, two ends of the pair of first compression springs respectively press against the lower end of the corresponding connecting piece and the top block.

Furthermore, the second anticollision portion comprises a swing rod, a bending plate and a second compression spring, the swing rod is hinged to the inner wall of the second buffer cavity, the swing rod penetrates through the guide rail and the protrusion to be abutted to the second buffer cavity, the bending plate is fixedly connected with the hinged end of the swing rod, two ends of the second compression spring are arranged in the second buffer cavity through spring seats, and the left spring seat can be abutted to the second buffer cavity to be pressed on the bending plate.

Furthermore, a gap is reserved between the vertical section of the bending plate and the partition plate of the anti-collision barrel.

Furthermore, an anti-skid wear-resistant pad is laid at the bottom of the supporting plate.

According to the above technical solution, the utility model has the advantages that: the utility model is not only simple in operation, it is swift convenient to use to possess very strong security when using.

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 structural sectional view of the present invention.

Fig. 2 is a structural sectional view of the anti-collision mechanism of the present invention.

Fig. 3 is a partially enlarged view of a portion a of fig. 2.

Fig. 4 is a side view of the slider of the present invention.

Fig. 5 is the utility model discloses an unmanned aerial vehicle bee colony's spatial structure schematic diagram.

Figure 6 is the utility model discloses an elevation view of unmanned aerial vehicle bee colony.

Fig. 7 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: unmanned aerial vehicle main part 1, backup pad 2, anti-skidding wear pad 21, supporting leg 22, anticollision institution 3, anticollision barrel 31, baffle 311, first cushion chamber 312, second cushion chamber 313, guide rail 32, slider 33, protruding 331, kicking block 332, pendulum rod 34, first compression spring 35, connection piece 351, go up bullet pad 36, second compression spring 37, the board 38 of bending, cylinder type top 10, intelligent battery 20, GPS module 30, driving motor 40, quick detach mechanism 50, miniature camera 60, flight control system 70, electricity accent 71, flight paddle 72.

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 7, an individual soldier hand-held throwing unmanned aerial vehicle as shown in fig. 1, 2 and 4 comprises a unmanned main body 1 and a plurality of support plates 2; an anti-collision mechanism 3 is arranged between the unmanned aerial vehicle main body 1 and the supporting plate 2, the anti-collision mechanism 3 comprises an anti-collision cylinder 31, a guide rail slider mechanism, a first anti-collision part and a second anti-collision part, and the anti-collision cylinder 31 is fixed at the bottom of the unmanned aerial vehicle main body 1; the guide rail sliding block mechanism is accommodated in the anti-collision barrel body 31 and is fixedly connected with the supporting legs 22 of the supporting plate 2; the first anti-collision part is arranged in the first buffer cavity 312 of the anti-collision barrel 31 and can be pressed against the upper end of the guide rail slider mechanism; the second anti-collision part is arranged in the second buffer cavity 313 of the anti-collision barrel body 31, and the second anti-collision part is abutted against the inner part of the guide rail sliding block mechanism.

Preferably, the guide rail and slider mechanism comprises a guide rail 32, a slider 33 and a protrusion 331, the guide rail 32 is installed on the inner wall of the anti-collision barrel body 31, the slider 33 is connected with the inner wall of the guide rail 32 in a sliding manner, the slider 33 is fixedly connected with the upper end of the supporting leg 22, and the protrusion 331 and the slider 33 are of an integrated structure.

Preferably, the first anti-collision part includes a pair of connection pieces 351, an upper elastic pad 36 and a pair of first compression springs 35, the upper elastic pad 36 is fixedly connected with the inner top wall of the anti-collision cylinder 31, the pair of connection pieces 351 are both installed in the upper elastic pad 36, the connection pieces 351 penetrate through the upper elastic pad 36 and extend downwards, and the pair of first compression springs 35 are both connected at the lower end of the corresponding connection pieces 351. With the above structure, when the slider 33 moves upward, the top block 332 is driven to move upward, so that the first compression spring 35 is compressed, and the top block 332 is buffered.

As shown in fig. 3, a top block 332 is fixedly connected to the upper end of the sliding block 33.

Preferably, both ends of the pair of first compression springs 35 are respectively pressed between the lower ends of the corresponding connecting pieces 351 and the top block 332.

Preferably, the second anti-collision part comprises a swing rod 34, a bending plate 38 and a second compression spring 37, the swing rod 34 is hinged to the inner wall of the second buffer cavity 313, the swing rod 34 penetrates through the guide rail 32 and the protrusion 331 to be abutted, the bending plate 38 is fixedly connected with the hinged end of the swing rod 34, two ends of the second compression spring 37 are arranged in the second buffer cavity 313 through spring seats, and the left spring seat can be abutted to the bending plate 38.

Preferably, a gap is left between the vertical section of the bent plate 38 and the partition 311 of the anti-collision cylinder 31.

Preferably, the bottom of the supporting plate 2 is laid with an anti-skid wear-resistant pad 21. The structure more than setting up can provide good anti-skidding wear-resisting effect for the bottom of backup pad 2.

The working principle is as follows: as shown in fig. 5, 6 and 7, when the aircraft is thrown by hand or on a mother aircraft, the intelligent battery 20 is turned on by remote control to enable the driving motor 40 to work, a plurality of flight blades 72 on the flight system 70 are rapidly unfolded, the flight blades 72 are locked by the quick release structure 50 to prevent shaking and resonance in flight, the orientation of the flight blades 72 is determined by adjusting the electric controller 71, 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 flyer to reach a mission area and can be shot by the micro camera 60; when landing, the anti-collision barrel 31 is pressed to move downwards and drives the guide rail 32 to move downwards, so that the protrusion 331 on the sliding block 33 gradually abuts against the left end of the swing rod 34 and drives the left end of the swing rod 34 to move upwards, so that the swing rod 34 drives the lower end of the bending plate 38 to move leftwards, the upper end of the bending plate 38 moves rightwards, the second compression spring 37 is compressed, the upper end of the bending plate 38 is buffered, and meanwhile, a good buffering effect is achieved in the whole anti-collision mechanism 3; when the sliding block 33 moves upwards, the ejecting block 332 is driven to move upwards so that the pair of first compression springs 35 are compressed, and the ejecting block 332 has a buffering effect, so that the whole anti-collision mechanism 3 further has a good buffering effect; to sum up, the utility model is not only simple in operation, it is swift convenient to use to possess very strong security when using.

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 formula unmanned aerial vehicle is thrown in handheld of individual soldier which characterized in that includes:

an unmanned aerial vehicle body (1);

a plurality of support plates (2);

wherein, unmanned aerial vehicle main part (1) with be equipped with an anticollision institution (3) between backup pad (2), anticollision institution (3) include:

the anti-collision barrel (31), the anti-collision barrel (31) is fixed at the bottom of the unmanned aerial vehicle main body (1);

the guide rail sliding block mechanism is accommodated in the anti-collision barrel body (31) and is fixedly connected with the supporting legs (22) of the supporting plate (2);

the first anti-collision part is arranged in a first buffer cavity (312) of the anti-collision barrel (31), and can be abutted against the upper end of the guide rail sliding block mechanism;

the second anti-collision part is arranged in a second buffer cavity (313) of the anti-collision barrel (31) and is abutted against the inner part of the guide rail sliding block mechanism.

2. The individual soldier hand-held throwing unmanned aerial vehicle of claim 1, wherein the guide rail slider mechanism comprises a guide rail (32), a slider (33) and a protrusion (331), the guide rail (32) is mounted on the inner wall of the anti-collision barrel body (31), the slider (33) is slidably connected with the inner wall of the guide rail (32), the slider (33) is fixedly connected with the upper end of the supporting leg (22), and the protrusion (331) and the slider (33) are of an integrated structure.

3. The individual soldier hand-held throwing type unmanned aerial vehicle of claim 2, wherein the first anti-collision part comprises a pair of connecting pieces (351), an upper elastic cushion (36) and a pair of first compression springs (35), the upper elastic cushion (36) is fixedly connected with the inner top wall of the anti-collision barrel body (31), the pair of connecting pieces (351) are installed in the upper elastic cushion (36), the connecting pieces (351) penetrate through the upper elastic cushion (36) and extend downwards, and the pair of first compression springs (35) are connected to the lower ends of the corresponding connecting pieces (351).

4. The individual soldier hand-held throwing unmanned aerial vehicle of claim 3, wherein an ejector block (332) is fixedly connected to the upper end of the slider (33).

5. The individual soldier hand-held throwing unmanned aerial vehicle of claim 4, wherein both ends of a pair of first compression springs (35) are respectively pressed between the lower end of the corresponding connecting piece (351) and the top block (332).

6. The individual soldier handheld throwing unmanned aerial vehicle of claim 5, wherein the second anti-collision part comprises a swing rod (34), a bending plate (38) and a second compression spring (37), the swing rod (34) is hinged to the inner wall of the second buffer cavity (313), the swing rod (34) penetrates through the guide rail (32) and abuts against the protrusion (331), the bending plate (38) is fixedly connected with the hinged end of the swing rod (34), two ends of the second compression spring (37) are arranged in the second buffer cavity (313) through spring seats, and the spring seat on the left side can abut against the bending plate (38).

7. The individual soldier hand-held throwing unmanned aerial vehicle of claim 6, wherein a gap is left between the vertical section of the bent plate (38) and the partition plate (311) of the anti-collision cylinder (31).

8. Individual soldier hand-held throwing unmanned aerial vehicle according to claim 1, wherein a non-slip wear pad (21) is laid on the bottom of the support plate (2).