CN213502896U

CN213502896U - Effectual exploration unmanned aerial vehicle of shock attenuation

Info

Publication number: CN213502896U
Application number: CN202022258461.2U
Authority: CN
Inventors: 李�瑞
Original assignee: Hainan Hongsheng Survey And Design Co Ltd
Current assignee: Hainan Hongsheng Survey And Design Co Ltd
Priority date: 2020-10-12
Filing date: 2020-10-12
Publication date: 2021-06-22
Anticipated expiration: 2030-10-12

Abstract

The utility model discloses an effectual exploration unmanned aerial vehicle of shock attenuation, including the bearing plate, the equal fixed mounting in both sides of bearing plate bottom has the soft area of connection, the bottom fixedly connected with mounting panel in the soft area of connection, the slide rail has been seted up to the inner chamber of mounting panel, the inner chamber movable mounting of slide rail has first slider, the inboard fixedly connected with connecting plate of first slider. The utility model discloses a spring can play the cushioning effect effectively, can prevent through the buffer beam that the spring from the phenomenon of skew about the absorbing in-process appears, this unmanned aerial vehicle's security has been strengthened, can prevent through connecting soft area that not hard up phenomenon from appearing in the mounting panel, be convenient for fix control box and connecting plate through threaded rod and nut, produce vibrations and make the connection position produce not hard up when preventing to descend, can prevent through the baffle that first slider breaks away from the slide rail, the common problem that the unmanned aerial vehicle of exploration ubiquitous shock attenuation effect is not good on the market has been solved simultaneously.

Description

Effectual exploration unmanned aerial vehicle of shock attenuation

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an effectual exploration unmanned aerial vehicle of shock attenuation.

Background

Unmanned aircraft is called unmanned aerial vehicle for short, and is called UAV in short in English, and is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, compared with the unmanned aircraft, the unmanned aircraft is more suitable for tasks too 'fool, dirty or dangerous', the unmanned aircraft can be divided into military and civil according to the application field, and the unmanned aircraft can be divided into reconnaissance aircraft and target aircraft in the military, and the unmanned aircraft can be applied to the industry in the civil field, and is really just needed by the unmanned aircraft; at present, in the application of fields such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news report, electric power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the phenomenon that the common exploration unmanned aerial vehicle in the market is poor in damping effect generally exists, and the unmanned aerial vehicle is easy to be damaged in the process of landing.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an effectual exploration unmanned aerial vehicle of shock attenuation possesses the effectual advantage of shock attenuation, has solved the common unmanned aerial vehicle of exploration on the market ubiquitous problem that the shock attenuation effect is not good.

In order to achieve the above object, the utility model provides a following technical scheme: an exploration unmanned aerial vehicle with good damping effect comprises a bearing plate, wherein soft connecting belts are fixedly arranged on two sides of the bottom of the bearing plate, a mounting plate is fixedly connected to the bottom of each soft connecting belt, a slide rail is arranged in an inner cavity of the mounting plate, a first slide block is movably mounted in the inner cavity of the slide rail, a connecting plate is fixedly connected to the inner side of the first slide block, a baffle is fixedly mounted at the bottom of the mounting plate, a cushion is fixedly mounted at the bottom of the baffle, a spring is fixedly mounted at the top of the connecting plate, a buffer rod is fixedly mounted at the top of the connecting plate and positioned on the inner side of the spring, a fixed plate is fixedly connected to the top of the spring, the fixed plate is fixedly connected with the bearing plate, a control box is fixedly mounted in the middle of the top of the bearing plate, a transverse plate, the both sides of connecting plate bottom and the equal swing joint of inner chamber that extends to the control box have a threaded rod, threaded rod and nut threaded connection.

Preferably, the sliding grooves are formed in two sides of the inner cavity of the control box, and the second sliding blocks are movably mounted on the inner sides of the sliding grooves.

Preferably, the second sliding block is fixedly connected with the transverse plate, and the two sides of the top of the bearing plate are fixedly provided with the support.

Preferably, a rotating device is fixedly mounted at the top of the bracket, and a mounting block is fixedly mounted at the top of the rotating device.

Preferably, screws are arranged on two sides of the front face of the top of the mounting block, and propellers are fixedly mounted at the bottoms of the screws and located at the top of the mounting block.

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

1. the utility model discloses a spring can play the cushioning effect effectively, can prevent through the buffer beam that the spring from the phenomenon of skew about the absorbing in-process appears, this unmanned aerial vehicle's security has been strengthened, can prevent through connecting soft area that not hard up phenomenon from appearing in the mounting panel, be convenient for fix control box and connecting plate through threaded rod and nut, produce vibrations and make the connection position produce not hard up when preventing to descend, can prevent through the baffle that first slider breaks away from the slide rail, the common problem that the unmanned aerial vehicle of exploration ubiquitous shock attenuation effect is not good on the market has been solved simultaneously.

2. The utility model discloses a screw can fix the screw, is convenient for take out and in time change the diaphragm from the control box through spout and second slider.

Drawings

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

FIG. 2 is a sectional view of the structure of the control box of the present invention;

fig. 3 is a top view of the rotating device of the present invention.

In the figure: 1. a bearing plate; 2. connecting a soft belt; 3. mounting a plate; 4. a slide rail; 5. a first slider; 6. a connecting plate; 7. a baffle plate; 8. a soft cushion; 9. a spring; 10. a buffer rod; 11. a fixing plate; 12. a control box; 13. a transverse plate; 14. a nut; 15. a threaded rod; 16. a chute; 17. a second slider; 18. a support; 19. a rotating device; 20. mounting blocks; 21. a screw; 22. a propeller.

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.

In the description herein, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings to facilitate the description of the patent and to simplify the description, but do not indicate or imply that the referenced device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus are not to be considered limiting of the patent. In the description of the present application, it should be noted that unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can, for example, be fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.

Referring to fig. 1-3, an exploration unmanned aerial vehicle with good damping effect comprises a bearing plate 1, wherein soft connecting belts 2 are fixedly installed on both sides of the bottom of the bearing plate 1, a mounting plate 3 is fixedly connected to the bottom of the soft connecting belts 2, a slide rail 4 is arranged in an inner cavity of the mounting plate 3, a first slide block 5 is movably installed in the inner cavity of the slide rail 4, a connecting plate 6 is fixedly connected to the inner side of the first slide block 5, a baffle 7 is fixedly installed at the bottom of the mounting plate 3, a cushion 8 is fixedly installed at the bottom of the baffle 7, a spring 9 is fixedly installed at the top of the connecting plate 6, a buffer rod 10 is fixedly installed at the top of the connecting plate 6 and positioned at the inner side of the spring 9, a fixing plate 11 is fixedly connected to the top of the spring 9, the fixing plate 11 is fixedly connected to the bearing plate 1, a, the transverse plate 13 is convenient to take out from the control box 12 and timely replace through the sliding groove 16 and the second sliding block 17, the second sliding block 17 is movably mounted on the inner side of the sliding groove 16, the second sliding block 17 is fixedly connected with the transverse plate 13, the two sides of the top of the bearing plate 1 are both fixedly mounted with the brackets 18, the top of the bracket 18 is fixedly mounted with the rotating device 19, the top of the rotating device 19 is fixedly mounted with the mounting block 20, the two sides of the front surface of the top of the mounting block 20 are both provided with the screws 21, the screws 22 can be fixed through the screws 21, the bottom of the screws 21 is fixedly mounted with the screws 22 at the top of the mounting block 20, the transverse plate 13 is fixedly mounted in the inner cavity of the control box 12, the nuts 14 are both fixedly mounted at the two sides of the top of the transverse plate 13, the two sides of the bottom of the connecting plate 6 and the inner cavity extending to the, can prevent through buffer beam 10 that spring 9 from appearing controlling the phenomenon of skew in absorbing process, this unmanned aerial vehicle's security has been strengthened, can prevent through connecting soft area 2 that the not hard up phenomenon from appearing in mounting panel 3, be convenient for fix control box 12 and connecting plate 6 through threaded rod 15 and nut 14, produce vibrations and make the connection position produce not hard up when preventing to descend, can prevent through baffle 7 that first slider 5 from breaking away from slide rail 4, the common problem that the unmanned aerial vehicle of exploration ubiquitous shock attenuation effect is not good on the market has been solved simultaneously.

All the components in the utility model are universal standard components or components known by technicians in the field, the structure and principle of the components are known by technicians in the technical manual or known by conventional experimental methods, standard parts used in the application document can be purchased from the market, the components in the application document can be customized according to the description of the specification and the accompanying drawings, the specific connection mode of each component adopts conventional means such as bolts, rivets, welding and the like mature in the prior art, machines, parts and equipment adopt conventional models in the prior art, the control mode is automatically controlled by a controller, a control circuit of the controller can be realized by simple programming of technicians in the field, the components belong to the common knowledge in the field, and the application document is mainly used for protecting mechanical devices, so the control mode and circuit connection are not explained in detail in the application document, no specific description will be made herein.

During the use, drive screw 22 through rotary device 19 and rotate, can play the cushioning effect when unmanned aerial vehicle falls to the ground through spring 9, can prevent through buffer beam 10 that spring 9 from appearing the phenomenon of left and right sides skew at the absorbing in-process, can prevent through connecting soft area 2 that mounting panel 3 from appearing not hard up phenomenon, can prevent through slide rail 4 and first slider 5 that connecting plate 6 from appearing the skew, can fix control box 12 and connecting plate 6 through threaded rod 15 and nut 14, can prevent through baffle 7 that first slider 5 breaks away from slide rail 4 in spring 9 shock attenuation in-process.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an effectual exploration unmanned aerial vehicle of shock attenuation, includes bearing plate (1), its characterized in that: the utility model discloses a bearing plate, including bearing plate (1), slide rail (4), inner chamber movable mounting have first slider (5), the inboard fixedly connected with connecting plate (6) of first slider (5), the bottom fixed mounting of mounting panel (3) has been seted up to the equal fixed mounting in both sides of bearing plate (1) bottom has the soft area of connection (2), the bottom fixedly connected with mounting panel (3) of connecting soft area (2), slide rail (4) have been seted up to the inner chamber of mounting panel (3), the inner chamber movable mounting of slide rail (4) has first slider (5), the inboard fixedly connected with connecting plate (6) of first slider (5), the bottom fixed mounting of mounting panel (3) has baffle (7), the bottom fixed mounting of baffle (7) has cushion (8), the top fixed mounting of connecting plate (6) has spring (9), the top of connecting plate (6) just is located the inboard fixed mounting of spring (, the middle fixed mounting at bearing plate (1) top has control box (12), the inner chamber fixed mounting of control box (12) has diaphragm (13), the equal fixed mounting in both sides at diaphragm (13) top has nut (14), the both sides of connecting plate (6) bottom and the equal swing joint in inner chamber that extends to control box (12) have threaded rod (15), threaded rod (15) and nut (14) threaded connection.

2. The exploration unmanned aerial vehicle with good shock absorption effect as claimed in claim 1, wherein: the both sides of control box (12) inner chamber have all seted up spout (16), the inboard movable mounting of spout (16) has second slider (17).

3. The exploration unmanned aerial vehicle with good shock absorption effect as claimed in claim 2, wherein: the second sliding block (17) is fixedly connected with the transverse plate (13), and the two sides of the top of the bearing plate (1) are fixedly provided with a support (18).

4. The exploration unmanned aerial vehicle with good shock absorption effect of claim 3, wherein: the top of support (18) fixed mounting has rotary device (19), the top fixed mounting of rotary device (19) has installation piece (20).

5. The exploration unmanned aerial vehicle with good shock absorption effect as claimed in claim 4, wherein: screws (21) are arranged on two sides of the front face of the top of the mounting block (20), and propellers (22) are fixedly mounted at the bottoms of the screws (21) and the top of the mounting block (20).