CN217260681U

CN217260681U - Protective structure for aircraft shell

Info

Publication number: CN217260681U
Application number: CN202220036526.5U
Authority: CN
Inventors: 毛子荐
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-01-07
Filing date: 2022-01-07
Publication date: 2022-08-23
Anticipated expiration: 2032-01-07

Abstract

The utility model belongs to the technical field of aircrafts, in particular to a protective structure for an aircraft shell, which comprises an unmanned aerial vehicle body, wherein a protective component is arranged on the unmanned aerial vehicle body; the protection component has been set up on this device, the user is through this protection component, can realize aerifing the gasbag, thereby make the gasbag can play fine protection to the unmanned aerial vehicle body, thereby can avoid the unmanned aerial vehicle body to receive outside striking and cause the damage, can improve the life of unmanned aerial vehicle body, and the supporting component has been added in this mechanism, can further improve the protecting effect, make the unmanned aerial vehicle body in the striking, buffering through the spring, protect the shell, and through the bracing piece, can be when the unmanned aerial vehicle body lands, support unmanned aerial vehicle through the bracing piece, avoid unmanned aerial vehicle directly to land and cause the damage.

Description

Protective structure for aircraft shell

Technical Field

The utility model belongs to the technical field of the aircraft, concretely relates to protective structure for aircraft shell.

Background

The unmanned aerial vehicle aircraft is more and more commonly applied in production and life at present, not only can be used for aerial photography, but also can be used for transporting goods, but at present, the shells of most unmanned aerial vehicles generally lack necessary protective structures, so that the aircraft is easy to be impacted by the outside when in use, and the aircraft is damaged;

in order to solve the above problem, a protective structure for an aircraft shell is proposed in the present application.

SUMMERY OF THE UTILITY MODEL

To solve the problems set forth in the background art described above. The utility model provides an aircraft is protective structure for shell has the characteristics of protecting aircraft shell.

In order to achieve the above object, the utility model provides a following technical scheme: a protective structure for an aircraft shell comprises an unmanned aerial vehicle body, wherein a protective component is mounted on the unmanned aerial vehicle body;

the protection component comprises an air pump, an air inlet pipe, an air inlet valve and an air bag, the surface of the unmanned aerial vehicle body is fixedly connected with the air pump, the air inlet pipe is fixedly connected with the air inlet valve, the air inlet valve is fixedly connected with the air bag, and the air bag is fixedly connected with the unmanned aerial vehicle body.

As the utility model relates to an aircraft is that protective structure is preferred for shell, the protective component still includes spring, telescopic link and guard plate, the unmanned aerial vehicle body with spring fixed connection, the inboard sliding connection of spring has the telescopic link, the telescopic link with unmanned aerial vehicle body fixed connection, telescopic link other end fixed connection has the guard plate, the guard plate with spring fixed connection.

As the utility model relates to an aircraft is preferred for protective structure of shell, still include supporting component, supporting component includes fixed block, mounting, motor, dwang, guide arm, slider, rotation piece and bracing piece, the fixed block with air pump fixed connection, two the mounting with fixed block fixed connection, mounting outside fixedly connected with the motor, the motor rotates through the transmission shaft and is connected with the dwang, two the guide arm with the dwang rotates to be connected, the guide arm other end rotates and is connected with the slider, the slider with mounting sliding connection, the slider with it rotates to connect to rotate, rotate the piece with the mounting rotates to be connected, rotate the piece with bracing piece fixed connection.

Compared with the prior art, the beneficial effects of the utility model are that:

set up the protective assembly on this device, the user is through this protective assembly, can realize aerifing the gasbag, thereby make the gasbag can play fine protection to the unmanned aerial vehicle body, thereby can avoid the unmanned aerial vehicle body to receive outside striking and cause the damage, can improve the life of unmanned aerial vehicle body, and the supporting component has been added in this mechanism, can further improve the protecting effect, make the unmanned aerial vehicle body in the striking, buffering through the spring, protect the shell, and through the bracing piece, can be when the unmanned aerial vehicle body lands, support unmanned aerial vehicle through the bracing piece, avoid unmanned aerial vehicle directly to land and cause the damage.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic structural view of the protection assembly of the present invention;

FIG. 3 is a schematic view of the structure of the spring of the present invention;

fig. 4 is a schematic structural view of the middle support assembly of the present invention.

In the figure:

1. an unmanned aerial vehicle body;

2. a guard assembly; 21. an air pump; 22. an air inlet pipe; 23. an intake valve; 24. an air bag; 25. a spring; 26. a telescopic rod; 27. a protection plate;

3. a support assembly; 31. a fixed block; 32. a fixing member; 33. a motor; 34. rotating the rod; 35. a guide bar; 36. a slider; 37. a rotating member; 38. a support rod.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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.

As shown in fig. 1:

the utility model provides an aircraft is protective structure for shell, includes unmanned aerial vehicle body 1.

In this embodiment: at present, the shell of most unmanned aerial vehicle body 1 that has now lacks necessary protective structure more, and unmanned aerial vehicle body 1 that is exactly like this causes the damage of unmanned aerial vehicle body 1 because outside striking more when using to make unmanned aerial vehicle body 1's life greatly reduced.

Further, the method comprises the following steps:

install protection component 2 on unmanned aerial vehicle body 1.

Further, the method comprises the following steps:

as shown in fig. 2 and 3:

with the above in mind: this protection component 2 includes air pump 21, intake pipe 22, admission valve 23 and gasbag 24, and fixed surface is connected with air pump 21 under the unmanned aerial vehicle body 1, six intake pipe 22 and air pump 21 fixed connection, intake pipe 22 and admission valve 23 fixed connection, admission valve 23 and gasbag 24 fixed connection, gasbag 24 and unmanned aerial vehicle body 1 fixed connection.

In this embodiment: the electric appliance that this device was used all supplies power through the inside lithium cell of unmanned aerial vehicle body 1, in the time of using, can be through starting air pump 21 to in the gasbag 24 that discharges into through intake pipe 22 with gas, thereby can aerify gasbag 24, just so can aerify through gasbag 24, carry out effectual protection to unmanned aerial vehicle body 1, thereby can make unmanned aerial vehicle body 1 can effectual impact outside.

It should be noted that: an air bag 24 is connected to the upper surface of each air inlet pipe 22, the six air bags 24 are arranged at equal intervals, and the air bags 24 are made of rubber materials and have good buffering performance.

It should be noted that: the air inlet valve 23 is provided with an air vent, and when the air bag 24 is not used for swelling, the air bag 24 can be deflated by opening the air vent on the air inlet valve 23.

Further, the method comprises the following steps of;

in an optional embodiment, the protection component 2 further includes a spring 25, a telescopic rod 26 and a protection plate 27, the unmanned aerial vehicle body 1 is fixedly connected with the spring 25, the telescopic rod 26 is slidably connected to the inner side of the spring 25, the telescopic rod 26 is fixedly connected with the unmanned aerial vehicle body 1, the protection plate 27 is fixedly connected to the other end of the telescopic rod 26, and the protection plate 27 is fixedly connected with the spring 25.

In this embodiment: when protection plate 27 receives outside striking, can cause the extrusion to spring 25 to can make telescopic link 26 can stretch out and draw back, telescopic link 26 can improve the stability when protection plate 27 removes like this, thereby can improve the effect of buffering through telescopic link 26 and spring 25's cooperation, makes the protective capacities better.

It should be noted that: the number of guard plate 27 is total six, and guard plate 27 is the equidistance and arranges, can follow the all-round unmanned aerial vehicle body 1 through guard plate 27 like this and protect, and guard plate 27 is made by elastic material's protection pad moreover.

It should be noted that: three spring 25 is all installed to every guard plate 27 upper surface, and spring 25 is the equidistance and arranges to can be through the more even buffering external impact force of three spring 25, thereby can make the protecting effect better.

As shown in fig. 4:

this protective structure for aircraft shell still includes supporting component 3, supporting component 3 includes fixed block 31, mounting 32, motor 33, dwang 34, guide arm 35, slider 36, rotate piece 37 and bracing piece 38, fixed block 31 and air pump fixed connection, two mounting 32 and fixed block 31 fixed connection, mounting 32 outside fixedly connected with motor 33, motor 33 rotates through the transmission shaft and is connected with dwang 34, two guide arms 35 rotate with dwang 34 to be connected, the guide arm 35 other end rotates and is connected with slider 36, slider 36 and mounting 32 sliding connection, slider 36 rotates with rotating piece 37 to be connected, it rotates with mounting 32 to rotate to be connected, it 37 and bracing piece 38 fixed connection to rotate piece.

In this embodiment: when in use, can be through starter motor 33, thereby drive dwang 34 and rotate, can drive guide arm 35 through dwang 34 and rotate like this, thereby can be through the rotation of guide arm 35, it removes to drive slider 36, slider 36 moves on the spout of seting up on mounting 32 this moment, just can drive and rotate a 37 and rotate, it just can drive bracing piece 38 and rotate to rotate 37 this moment, thereby can adjust the angle of bracing piece 38, thereby can make bracing piece 38 become the tilt state from the horizontality, thereby can utilize bracing piece 38 to contact with ground earlier, play the effect of support.

It should be noted that: the rotation direction of the support rod 38 is related to the rotation direction of the rotation piece 37, the rotation direction of the rotation piece 37 is related to the movement direction of the slider 36, the movement direction of the slider 36 is related to the movement direction of the guide rod 35, the movement direction of the guide rod 35 is related to the rotation direction of the rotation rod 34, and the rotation direction of the rotation rod 34 is related to the rotation direction of the transmission shaft of the motor 33.

It should be noted that: the supporting rod 38 is connected with a supporting head made of rubber at the tail end, so that the supporting and fixing effects are better.

It should be noted that: the rotatable member 37 is 7-shaped, so that the specific shape of the rotatable member 37 can be utilized, and the rotatable member 37 can drive the support rod 38 to rotate.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. 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 an aircraft is protective structure for shell, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle body (1) is provided with a protection component (2);

protection component (2) include air pump (21), intake pipe (22), admission valve (23) and gasbag (24), fixed surface is connected with under unmanned aerial vehicle body (1) air pump (21), six intake pipe (22) with air pump (21) fixed connection, intake pipe (22) with admission valve (23) fixed connection, admission valve (23) with gasbag (24) fixed connection, gasbag (24) with unmanned aerial vehicle body (1) fixed connection.

2. The protective structure for aircraft skin according to claim 1, characterized in that: protection component (2) still include spring (25), telescopic link (26) and guard plate (27), unmanned aerial vehicle body (1) with spring (25) fixed connection, spring (25) inboard sliding connection has telescopic link (26), telescopic link (26) with unmanned aerial vehicle body (1) fixed connection, telescopic link (26) other end fixedly connected with guard plate (27), guard plate (27) with spring (25) fixed connection.

3. The protective structure for aircraft skin according to claim 1, characterized in that: still include supporting component (3), supporting component (3) include fixed block (31), mounting (32), motor (33), dwang (34), guide arm (35), slider (36), rotate piece (37) and bracing piece (38), fixed block (31) with air pump (21) fixed connection, two mounting (32) with fixed block (31) fixed connection, mounting (32) outside fixed connection has motor (33), motor (33) rotate through the transmission shaft and are connected with dwang (34), two guide arm (35) with dwang (34) rotate and are connected, guide arm (35) other end rotates and is connected with slider (36), slider (36) with mounting (32) sliding connection, slider (36) with rotate piece (37) and rotate and be connected, the rotating part (37) is rotatably connected with the fixing part (32), and the rotating part (37) is fixedly connected with the supporting rod (38).