CN220010123U - Combined type fixed wing unmanned aerial vehicle - Google Patents

Abstract

The utility model discloses a combined type fixed wing unmanned aerial vehicle, in particular to the technical field of fixed wing unmanned aerial vehicles, which comprises a machine body and a connecting device, wherein wings are arranged on two sides of the machine body, the machine body is provided with a supporting device by means of the connecting device, the supporting device comprises a connecting plate, one end of the connecting plate is in threaded connection with a bolt, the surface of the bolt is in threaded connection with a square tube, one end of the square tube is fixedly connected with a placing plate, one end of the placing plate, which is far away from the square tube, is fixedly connected with a spring, and one end of the spring, which is far away from the placing plate, is fixedly connected with a special-shaped block.

Description

Combined type fixed wing unmanned aerial vehicle

Technical Field

The utility model relates to the technical field of fixed wing unmanned aerial vehicles, in particular to a combined fixed wing unmanned aerial vehicle.

Background

The fixed wing unmanned aerial vehicle is an unmanned aerial vehicle with wings and is widely applied to the professions of surveying and mapping, geology, petroleum, agriculture and forestry and the like.

The inventor finds that the fixed wing unmanned aerial vehicle can combine parts such as wings when using, make unmanned aerial vehicle take off after the combination, when unmanned aerial vehicle descends, can use the support to support. When the unmanned aerial vehicle falls to the ground with uneven sundries, the unmanned aerial vehicle can be caused to topple over, so that the wing is damaged in contact with the ground, and the problem of affecting the use of the unmanned aerial vehicle occurs.

In order to solve the problems, the prior art adopts a mode of processing landing places before the unmanned aerial vehicle lands, so that the landing places are leveled. The present utility model provides another solution.

Disclosure of Invention

The utility model provides a combined type fixed wing unmanned aerial vehicle, which aims to solve the problem that when an unmanned aerial vehicle falls on the ground with uneven sundries, the unmanned aerial vehicle can topple over, and the contact between wings and the ground is damaged, so that the use of the unmanned aerial vehicle is affected.

In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides a modular fixed wing unmanned aerial vehicle, includes fuselage and connecting device, the both sides of fuselage are equipped with the wing, the fuselage is equipped with strutting arrangement with the help of connecting device, strutting arrangement includes the connecting plate, the one end threaded connection of connecting plate has the bolt, the surface threaded connection of bolt has the square tube, the one end fixedly connected with of square tube places the board, place the board and keep away from the one end fixedly connected with spring of square tube, the one end fixedly connected with dysmorphism piece of placing the board is kept away from to the spring.

The effects achieved by the components are as follows: when the unmanned aerial vehicle is used, the wings and the fuselage are combined, then the rest parts are combined with the fuselage, and then the unmanned aerial vehicle is used. When using unmanned aerial vehicle, can remove the square tube earlier and adjust the distance of fuselage and ground, then rotate the bolt and lead to together with the connecting plate is fixed, then when unmanned aerial vehicle falls to have debris uneven ground, can block together with subaerial debris through special-shaped block, the spring makes the height of special-shaped block adaptation different debris, then through the special-shaped block together with ground debris card, avoid unmanned aerial vehicle to take place to empty, make wing and ground contact impaired, lead to taking place the condition that influences unmanned aerial vehicle and use to promote unmanned aerial vehicle's result of use.

Preferably, the inside cover of spring is equipped with the telescopic link, the both ends of telescopic link are respectively with place board and dysmorphism piece fixed connection.

The effects achieved by the components are as follows: when the spring is used, the shape of the spring can be limited through the telescopic rod in the spring, and the situation that the spring is bent and the use of the spring is influenced is avoided.

Preferably, the surface of the square tube is fixedly connected with a rubber sleeve, and the size of the rubber sleeve is matched with the size of the square tube.

The effects achieved by the components are as follows: when the square tube is moved, the friction force between the hands of an operator and the square tube can be increased through the rubber sleeve on the surface of the square tube, so that the operator can move the square tube conveniently.

Preferably, the surface of the square tube is fixedly connected with a reinforcing plate, and one end of the reinforcing plate, which is far away from the square tube, is fixedly connected with the placing plate.

The effects achieved by the components are as follows: when using to place the board, can increase the joint strength of placing between board and the square through placing the reinforcing plate on the board, avoid square to take place with the condition of placing the board and break away from.

Preferably, the connecting device comprises a fixed block, the fixed block is fixedly connected with the machine body, a sliding rail is fixedly connected with the surface of the fixed block, a clamping block is slidably connected with the inside of the sliding rail, and the clamping block is clamped with the connecting plate.

The effects achieved by the components are as follows: when using strutting arrangement, can insert inside the fixed block with the connecting plate, then remove the inside fixture block of slide rail, make the fixture block fix the connecting plate, then make the connecting plate quick with the fuselage fixed to make things convenient for strutting arrangement to use, and then promote strutting arrangement's result of use.

Preferably, the surface of the clamping block is fixedly connected with a control handle, and the section of the control handle is T-shaped.

The effects achieved by the components are as follows: when the clamping block is used, the clamping block can be moved by an operator more easily through the control handle on the surface of the clamping block, so that the using effect of the clamping block is improved.

Preferably, the surface of the fixed block is connected with guide plates, and two guide plates and the fixed block form an oblique angle.

The effects achieved by the components are as follows: when the connecting plate is inserted into the inside of the fixed block, the position of the connecting plate can be guided through the guide plate on the surface of the fixed block, so that the connecting plate can more easily reach the inside of the fixed block.

In summary, the beneficial effects of the utility model are as follows: can avoid falling to have debris uneven ground in unmanned aerial vehicle through the dysmorphism piece together with ground debris card, unmanned aerial vehicle takes place to empty when unmanned aerial vehicle, makes wing and ground contact impaired, leads to taking place to influence unmanned aerial vehicle's condition of use to promote unmanned aerial vehicle's result of use.

Drawings

Fig. 1 is a schematic perspective view of the present utility model.

Fig. 2 is a schematic perspective view of the supporting device of the present utility model.

Fig. 3 is an enlarged view of fig. 2 at a in accordance with the present utility model.

Fig. 4 is a schematic perspective view of the connecting device of the present utility model.

Reference numerals illustrate: 1. a body; 2. a wing; 3. a support device; 31. a connecting plate; 32. a bolt; 33. square communication; 34. placing a plate; 35. a spring; 36. a special-shaped block; 37. a telescopic rod; 38. a rubber sleeve; 39. a reinforcing plate; 4. a connecting device; 41. a fixed block; 42. a slide rail; 43. a clamping block; 44. a control handle; 45. and a guide plate.

Detailed Description

Referring to fig. 1 to 4, the present embodiment discloses a combined fixed wing unmanned aerial vehicle, which comprises a fuselage 1 and a connecting device 4, wherein wings 2 are arranged on two sides of the fuselage 1, and the fuselage 1 is provided with a supporting device 3 by means of the connecting device 4.

Referring to fig. 1 to 4, the present embodiment discloses that the supporting device 3 includes a connecting plate 31, one end of the connecting plate 31 is screwed with a bolt 32, a square tube 33 is screwed on the surface of the bolt 32, one end of the square tube 33 is fixedly connected with a placing plate 34, one end of the placing plate 34 far from the square tube 33 is fixedly connected with a spring 35, and one end of the spring 35 far from the placing plate 34 is fixedly connected with a special-shaped block 36. When using the unmanned aerial vehicle, the wing 2 and the fuselage 1 are combined, then the rest parts are combined with the fuselage 1, and then the unmanned aerial vehicle is used. When the unmanned aerial vehicle is used, the square 33 can be moved firstly to adjust the distance between the unmanned aerial vehicle body 1 and the ground, then the square 33 and the connecting plate 31 are fixed together by the rotating bolts 32, then when the unmanned aerial vehicle falls on the ground with uneven sundries, the irregular block 36 can be clamped with the sundries on the ground, the spring 35 enables the irregular block 36 to adapt to the heights of different sundries, then the irregular block 36 clamped with the sundries on the ground can prevent the unmanned aerial vehicle from toppling over, the wing 2 is damaged in contact with the ground, and the use condition of the unmanned aerial vehicle is affected, so that the use effect of the unmanned aerial vehicle is improved.

Referring to fig. 1 to 4, this embodiment discloses that the spring 35 is internally sleeved with a telescopic rod 37, and both ends of the telescopic rod 37 are fixedly connected with the placing plate 34 and the special-shaped block 36, respectively. When the spring 35 is used, the shape of the spring 35 can be limited by the telescopic rod 37 inside the spring 35, so that the spring 35 is prevented from being bent, and the use of the spring 35 is prevented from being influenced. The surface of the square tube 33 is fixedly connected with a rubber sleeve 38, and the size of the rubber sleeve 38 is matched with the size of the square tube 33. When the square tube 33 is moved, the friction force between the hands of the operator and the square tube 33 can be increased through the rubber sleeve 38 on the surface of the square tube 33, so that the operator can move the square tube 33 conveniently. The surface of the square tube 33 is fixedly connected with a reinforcing plate 39, and one end, far away from the square tube 33, of the reinforcing plate 39 is fixedly connected with the placing plate 34. When the placing plate 34 is used, the connection strength between the placing plate 34 and the square tube 33 can be increased through the reinforcing plate 39 on the placing plate 34, so that the situation that the square tube 33 is separated from the placing plate 34 is avoided.

Referring to fig. 1 to 4, the present embodiment discloses a connecting device 4 including a fixing block 41, wherein the fixing block 41 is fixedly connected with a machine body 1, a sliding rail 42 is fixedly connected with a surface of the fixing block 41, a clamping block 43 is slidably connected with an inside of the sliding rail 42, and the clamping block 43 is clamped with the connecting plate 31. When using strutting arrangement 3, can insert inside fixed block 41 with connecting plate 31, then remove the inside fixture block 43 of slide rail 42, make fixture block 43 fix connecting plate 31, then make connecting plate 31 fixed with fuselage 1 fast to make things convenient for strutting arrangement 3 to use, and then promote strutting arrangement 3's result of use.

Referring to fig. 1 to 4, the present embodiment discloses that a control handle 44 is fixedly connected to a surface of a clamping block 43, and a cross section of the control handle 44 is T-shaped. When the clamping block 43 is used, the clamping block 43 can be moved more easily by an operator through the control handle 44 on the surface of the clamping block 43, so that the using effect of the clamping block 43 is improved. The surface of the fixed block 41 is connected with guide plates 45, and the two guide plates 45 are at an oblique angle with the fixed block 41. When the connection plate 31 is inserted into the inside of the fixing block 41, the position of the connection plate 31 may be guided by the guide plate 45 on the surface of the fixing block 41, thereby making it easier for the connection plate 31 to reach the inside of the fixing block 41.

The working principle is as follows: when using the unmanned aerial vehicle, the wing 2 and the fuselage 1 are combined, then the rest parts are combined with the fuselage 1, and then the unmanned aerial vehicle is used. When the unmanned aerial vehicle is used, the square 33 with the rubber sleeve 38 and the reinforcing plate 39 is moved firstly to adjust the distance between the machine body 1 and the ground, then the square 33 and the connecting plate 31 are fixed together by the rotating bolts 32, and then when the unmanned aerial vehicle falls on the ground with uneven sundries, the unmanned aerial vehicle can be clamped together with the sundries on the ground through the special-shaped blocks 36, and the springs 35 and the telescopic rods 37 on the surface of the placing plate 34 are arranged to enable the special-shaped blocks 36 to adapt to the heights of different sundries. Through using strutting arrangement 3, can avoid unmanned aerial vehicle to take place to empty through the dysmorphism piece 36 that blocks together with ground debris, make wing 2 and ground contact impaired, lead to taking place to influence unmanned aerial vehicle's condition of use to promote unmanned aerial vehicle's result of use.

When the supporting device 3 is used, the connecting plate 31 can be inserted into the fixing block 41 with the guide plate 45, and then the clamping block 43 in the sliding rail 42 can be moved by the control handle 44, so that the clamping block 43 fixes the connecting plate 31. Through using connecting device 4, can make connecting plate 31 fixed with fuselage 1 fast to make things convenient for strutting arrangement 3 to use, and then promote strutting arrangement 3's result of use.

Claims (7)

1. The utility model provides a modular fixed wing unmanned aerial vehicle, includes fuselage (1) and connecting device (4), its characterized in that: the both sides of fuselage (1) are equipped with wing (2), fuselage (1) are equipped with strutting arrangement (3) with the help of connecting device (4), strutting arrangement (3) are including connecting plate (31), the one end threaded connection of connecting plate (31) has bolt (32), the surface threaded connection of bolt (32) has square tube (33), the one end fixedly connected with of square tube (33) places board (34), place board (34) and keep away from the one end fixedly connected with spring (35) of square tube (33), the one end fixedly connected with dysmorphism piece (36) of placing board (34) are kept away from to spring (35).

2. The combination fixed wing unmanned aerial vehicle of claim 1, wherein: the inside cover of spring (35) is equipped with telescopic link (37), the both ends of telescopic link (37) are respectively with place board (34) and dysmorphism piece (36) fixed connection.

3. The combination fixed wing unmanned aerial vehicle of claim 1, wherein: the surface of the square tube (33) is fixedly connected with a rubber sleeve (38), and the size of the rubber sleeve (38) is matched with the size of the square tube (33).

4. The combination fixed wing unmanned aerial vehicle of claim 1, wherein: the surface of the square tube (33) is fixedly connected with a reinforcing plate (39), and one end, far away from the square tube (33), of the reinforcing plate (39) is fixedly connected with the placing plate (34).

5. The combination fixed wing unmanned aerial vehicle of claim 1, wherein: the connecting device (4) comprises a fixed block (41), the fixed block (41) is fixedly connected with the machine body (1), a sliding rail (42) is fixedly connected with the surface of the fixed block (41), a clamping block (43) is slidably connected inside the sliding rail (42), and the clamping block (43) is clamped with the connecting plate (31).

6. The combination fixed wing unmanned aerial vehicle of claim 5, wherein: the surface of the clamping block (43) is fixedly connected with a control handle (44), and the cross section of the control handle (44) is T-shaped.

7. The combination fixed wing unmanned aerial vehicle of claim 5, wherein: the surface of the fixed block (41) is connected with guide plates (45), and two guide plates (45) form an oblique angle with the fixed block (41).