CN213892904U

CN213892904U - Unmanned aerial vehicle for architectural design takes photo by plane with collision avoidance

Info

Publication number: CN213892904U
Application number: CN202022445216.2U
Authority: CN
Inventors: 林旭萍
Original assignee: Shanghai Tongyi Architectural Design Co ltd
Current assignee: Shanghai Tongyi Architectural Design Co ltd
Priority date: 2020-10-28
Filing date: 2020-10-28
Publication date: 2021-08-06
Anticipated expiration: 2030-10-28

Abstract

The utility model discloses an unmanned aerial vehicle takes photo by plane for architectural design with anticollision protection, which comprises a bod, the bottom fixed mounting of organism has first support, the bottom fixed mounting of first support has the connecting rod, the bottom fixed mounting of connecting rod has the roof, the outside fixed mounting of roof has the cushion frame, the bottom fixed mounting of roof has the sleeve, the telescopic outside is provided with first spring, telescopic bottom fixed mounting has the base. This architectural design is with unmanned aerial vehicle that takes photo by plane with collision avoidance, the frame construction that first support and connecting rod are constituteed, reduce the resistance that unmanned aerial vehicle flies, through the distance between connecting rod and the camera, the camera receives the collision when preventing unmanned aerial vehicle from falling, the contact surface of crashproof pad increase and ground, it is stable when making unmanned aerial vehicle put, when unmanned aerial vehicle descends, the buffer frame will be pushed down to the sudden atress of connecting rod, the buffer frame kick-backs under the effect of second spring and first spring, the effect of buffer protection when playing the striking.

Description

Unmanned aerial vehicle for architectural design takes photo by plane with collision avoidance

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle takes photo by plane for architectural design with collision avoidance.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Most unmanned aerial vehicle protective effect that has now is not good, and the majority adopts the plastics pole to protect, and unmanned aerial vehicle falls and produces huge impact, and the plastics pole is very easily broken, makes unmanned aerial vehicle and camera all receive the damage, and the blade does not have the anticollision protection when flying, damages when making the blade collision.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle takes photo by plane for architectural design with anticollision protection to it is not good to provide current most unmanned aerial vehicle protective effect in solving above-mentioned background art, and the majority adopts the plastics pole to protect, and unmanned aerial vehicle falls and produces huge impact, and the plastics pole is very easily broken, makes unmanned aerial vehicle and camera all receive the damage, and the blade does not have the anticollision protection when flying, the problem of damage when making the blade collision.

In order to achieve the above object, the utility model provides a following technical scheme: an aerial photography unmanned aerial vehicle with anti-collision protection for architectural design comprises a body, wherein a first support is fixedly mounted at the bottom of the body, a connecting rod is fixedly mounted at the bottom of the first support, a top plate is fixedly mounted at the bottom of the connecting rod, a buffer frame is fixedly mounted at the outer side of the top plate, a sleeve is fixedly mounted at the bottom of the top plate, a first spring is arranged at the outer side of the sleeve, a base is fixedly mounted at the bottom of the sleeve, one side of the base, which is close to the buffer frame, is fixedly connected with one end of a second spring, an anti-collision pad is fixedly mounted at the bottom of the base, a camera is arranged at the bottom of the body, a gliding wing is fixedly mounted at the outer side of the body, a clamping groove is reserved at the outer side of the gliding wing, a fixing nail is arranged at the inner side of the clamping groove, an air vent is arranged inside the fixing nail, and a connecting rope is fixedly connected with the outer side of the fixing nail, the inside fixed mounting of glide wing has driving motor, driving motor's output shaft fixedly connected with flight blade, the top fixed mounting of glide wing has the second support, the top fixed mounting of second support has the annular frame, the outside fixedly connected with third spring's of annular frame one end, the other end fixedly connected with anticollision frame of third spring.

Preferably, the connecting rods are located below the camera, the number of the first supports is four, and the two connecting rods are symmetrically arranged on the front side and the rear side of the first support.

Preferably, the bottom fixedly connected with one end of the first spring of roof, the other end fixedly connected with base of first spring, the roof is provided with four, the crash pad adopts the rubber material, the crash pad is trapezium structure.

Preferably, the glider is provided with four, the glider is forty-five degrees angular distribution with the organism, driving motor is located the one end that the organism was kept away from to the glider, the glider is the trapezium structure.

Preferably, the vent holes are of inverted funnel-shaped structures, and the number of the fixing nails is four.

Preferably, the third spring is equidistantly arranged on the annular frame, the diameter of the anti-collision frame is larger than that of the annular frame, the height of the second support is larger than that of the flying blade, and the diameter of the annular frame is larger than that of the flying blade.

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

1. the aerial photography unmanned aerial vehicle with anti-collision protection for building design has the advantages that the frame structure consisting of the first support and the connecting rod reduces the flying resistance of the unmanned aerial vehicle, the distance between the connecting rod and the camera prevents the camera from being collided when the unmanned aerial vehicle falls, the anti-collision pad increases the contact surface with the ground, so that the unmanned aerial vehicle is stable when being placed, when the unmanned aerial vehicle descends, the connecting rod suddenly bears the force to extrude the buffer frame downwards, and the buffer frame rebounds under the action of the second spring and the first spring to play a role in buffering protection during collision;

2. this unmanned aerial vehicle takes photo by plane for architectural design with anticollision protection will fix through the staple, and when unmanned aerial vehicle normally flies to descend, gaseous spills from the air vent, but when unmanned aerial vehicle descends rapidly, gaseous not reaching to spill and take out the staple from the air vent, makes the umbrella shell open, makes the parachute expand, prevents that unmanned aerial vehicle from falling, through the setting of anticollision frame, makes the flight blade obtain the protection when the striking, plays the purpose of buffering through inboard third spring simultaneously.

Drawings

Fig. 1 is a schematic top view of the present invention;

FIG. 2 is a schematic view of the front cross-sectional structure of the present invention;

FIG. 3 is a schematic view of the three-dimensional structure of the fixing nail of the present invention;

fig. 4 is a schematic view of the three-dimensional structure of the crash pad of the present invention.

In the figure: 1. a body; 2. a first bracket; 3. a connecting rod; 4. a top plate; 5. a buffer frame; 6. a sleeve; 7. a first spring; 8. a base; 9. a second spring; 10. an anti-collision pad; 11. a camera; 12. a glider wing; 13. a card slot; 14. fixing nails; 15. a vent hole; 16. connecting ropes; 17. a drive motor; 18. a flight blade; 19. a second bracket; 20. an annular frame; 21. a third spring; 22. an anti-collision frame; 23. an umbrella shell; 24. a parachute is provided.

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, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution: an aerial photography unmanned aerial vehicle with anti-collision protection for architectural design comprises a machine body 1, a first support 2, a connecting rod 3, a top plate 4, a buffer frame 5, a sleeve 6, a first spring 7, a base 8, a second spring 9, an anti-collision pad 10, a camera 11, a glider 12, a clamping groove 13, fixing nails 14, vent holes 15, a connecting rope 16, a driving motor 17, flight blades 18, a second support 19, an annular frame 20, a third spring 21, an anti-collision frame 22, an umbrella shell 23 and a parachute 24, wherein the bottom of the machine body 1 is fixedly provided with the first support 2, the bottom of the first support 2 is fixedly provided with the connecting rod 3, the bottom of the connecting rod 3 is fixedly provided with the top plate 4, the outer side of the top plate 4 is fixedly provided with the buffer frame 5, the bottom of the top plate 4 is fixedly provided with the sleeve 6, the outer side of the sleeve 6 is provided with the first spring 7, the bottom of the sleeve 6 is fixedly provided with the base 8, one end of the second spring 9 is fixedly connected to one side of the base 8, which is close to the buffer frame 5, base 8's bottom fixed mounting has crash pad 10, organism 1's bottom is provided with camera 11, organism 1's outside fixed mounting has glider 12, the outside reservation of glider 12 has draw-in groove 13, the inboard of draw-in groove 13 is provided with staple 14, air vent 15 has been seted up to staple 14's inside, staple 14's outside fixedly connected with connects rope 16, the inside fixed mounting of glider 12 has driving motor 17, driving motor 17's output shaft fixedly connected with flight blade 18, the top fixed mounting of glider 12 has second support 19, the top fixed mounting of second support 19 has annular frame 20, the outside fixedly connected with third spring 21's of annular frame 20 one end, the other end fixedly connected with anticollision frame 22 of third spring 21.

Further, connecting rod 3 is located the below of camera 11, and first support 2 is provided with four, and connecting rod 3 bilateral symmetry is provided with two around first support 2, and the frame construction that first support 2 and connecting rod 3 are constituteed reduces the resistance that unmanned aerial vehicle flies, through the distance between connecting rod 3 and the camera 11, camera 11 receives the collision when preventing that unmanned aerial vehicle from falling.

Further, the bottom fixedly connected with one end of the first spring 7 of roof 4, the other end fixedly connected with base 8 of first spring 7, roof 4 is provided with four, crash pad 10 adopts the rubber material, crash pad 10 is the trapezium structure, the contact surface of crash pad 10 increase and ground, it is stable when making unmanned aerial vehicle put, will cushion 5 extrude down when connecting rod 3 atress suddenly, cushion 5 kick-backs under the effect of second spring 9 and first spring 7, the effect of buffer protection when playing the striking.

Further, the glider 12 is provided with four, and the glider 12 is forty-five degrees angular distributions with organism 1, and driving motor 17 is located the one end that the organism 1 was kept away from to the glider 12, and the glider 12 is the trapezium structure, and the trapezium structure through the glider 12 reduces the flight resistance, starts driving motor 17, and driving motor 17 drives flight blade 18 clockwise or anticlockwise rotation to reach the effect that unmanned aerial vehicle flies.

Further, air vent 15 is for falling funnel shape structure, and staple 14 is provided with four, fixes umbrella shell 23 through staple 14, and when unmanned aerial vehicle normal flight descends, gas spills from air vent 15, but when unmanned aerial vehicle descends rapidly, gas does not come to spill and take out staple 14 from air vent 15, makes umbrella shell 23 open, makes parachute 24 expand, prevents that unmanned aerial vehicle from falling.

Furthermore, a plurality of third springs 21 are equidistantly arranged on the annular frame 20, the diameter of the anti-collision frame 22 is larger than that of the annular frame 20, the height of the second support 19 is larger than that of the flight blade 18, the diameter of the annular frame 20 is larger than that of the flight blade 18, the flight blade 18 is protected during collision through the arrangement of the anti-collision frame 22, and meanwhile, the purpose of buffering is achieved through the third springs 21 on the inner side.

The working principle is as follows: firstly, the unmanned aerial vehicle is horizontally placed on the ground, the remote controller is operated, the driving motor 17 is started, the driving motor 17 drives the flight blades 18 to rotate clockwise or anticlockwise, so that the flying effect of the unmanned aerial vehicle is achieved, the flight blades 18 are protected during collision through the arrangement of the anti-collision frame 22, meanwhile, the purpose of buffering is achieved through the third springs 21 on the inner side, the umbrella shell 23 is fixed through the fixing nails 14, when the unmanned aerial vehicle descends in normal flight, gas leaks out of the vent holes 15, but when the unmanned aerial vehicle descends rapidly, the gas does not leak out of the vent holes 15 and carries out of the fixing nails 14, the umbrella shell 23 is opened, the parachute 24 is unfolded, the unmanned aerial vehicle is prevented from falling, when the unmanned aerial vehicle descends, the buffer frame 5 is extruded downwards due to the sudden stress of the connecting rod 3, the buffer frame 5 rebounds under the action of the second springs 9 and the first springs 7, the buffering protection effect during collision is achieved, through the distance between connecting rod 3 and camera 11, camera 11 receives the collision when preventing unmanned aerial vehicle from falling.

It should be finally noted that the above only serves to illustrate the technical solution of the present invention, and not to limit the scope of the present invention, and that simple modifications or equivalent replacements performed by those skilled in the art to the technical solution of the present invention do not depart from the spirit and scope of the technical solution of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle takes photo by plane for architectural design with collision avoidance, includes organism (1), its characterized in that: the bottom fixed mounting of organism (1) has first support (2), the bottom fixed mounting of first support (2) has connecting rod (3), the bottom fixed mounting of connecting rod (3) has roof (4), the outside fixed mounting of roof (4) has buffer bracket (5), the bottom fixed mounting of roof (4) has sleeve (6), the outside of sleeve (6) is provided with first spring (7), the bottom fixed mounting of sleeve (6) has base (8), one end that one side fixedly connected with second spring (9) that base (8) are close to buffer bracket (5), the bottom fixed mounting of base (8) has crashproof pad (10), the bottom of organism (1) is provided with camera (11), the outside fixed mounting of organism (1) has glide wing (12), the outside of glide wing (12) is reserved has draw-in groove (13), the inboard of draw-in groove (13) is provided with staple (14), air vent (15) have been seted up to the inside of staple (14), outside fixedly connected with of staple (14) connects rope (16), the inside fixed mounting of glider (12) has driving motor (17), the output shaft fixedly connected with flight blade (18) of driving motor (17), the top fixed mounting of glider (12) has second support (19), the top fixed mounting of second support (19) has annular frame (20), the one end of the outside fixedly connected with third spring (21) of annular frame (20), the other end fixedly connected with anticollision frame (22) of third spring (21), the top of organism (1) is provided with umbrella shell (23), the top fixed mounting of organism (1) has parachute (24).

2. The aerial photography unmanned aerial vehicle with anti-collision protection for architectural design of claim 1, characterized in that: the connecting rod (3) is located below the camera (11), the number of the first supports (2) is four, and the connecting rods (3) are symmetrically arranged on the front side and the rear side of the first supports (2).

3. The aerial photography unmanned aerial vehicle with anti-collision protection for architectural design of claim 1, characterized in that: the bottom fixedly connected with one end of a first spring (7) of roof (4), the other end fixedly connected with base (8) of first spring (7), roof (4) are provided with four, crashproof pad (10) adopt the rubber material, crashproof pad (10) are the trapezium structure.

4. The aerial photography unmanned aerial vehicle with anti-collision protection for architectural design of claim 1, characterized in that: the utility model discloses a glider, including glider (12), body (1), driving motor (17), gliding wing (12) are four, gliding wing (12) are forty-five degrees angular distribution with organism (1), the one end that organism (1) was kept away from in gliding wing (12), gliding wing (12) are the trapezium structure.

5. The aerial photography unmanned aerial vehicle with anti-collision protection for architectural design of claim 1, characterized in that: the vent holes (15) are of inverted funnel-shaped structures, and four fixing nails (14) are arranged.

6. The aerial photography unmanned aerial vehicle with anti-collision protection for architectural design of claim 1, characterized in that: the third springs (21) are arranged on the annular frame (20) at equal intervals, the diameter of the anti-collision frame (22) is larger than that of the annular frame (20), the height of the second support (19) is larger than that of the flying blade (18), and the diameter of the annular frame (20) is larger than that of the flying blade (18).