CN216509029U

CN216509029U - Aerial photography device for state and soil resource monitoring pipe

Info

Publication number: CN216509029U
Application number: CN202220077707.2U
Authority: CN
Inventors: 时维方; 朱瑞利; 时维军
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-01-13
Filing date: 2022-01-13
Publication date: 2022-05-13
Anticipated expiration: 2032-01-13

Abstract

The utility model discloses an aerial photography device for a national soil resource monitoring in the technical field of aerial photography equipment, which comprises an unmanned aerial vehicle main body, wherein the bottom end of the unmanned aerial vehicle main body is symmetrically and fixedly provided with a support frame, the bottom end of the support frame is embedded with a buffer rod in a sliding manner, the outer side of the buffer rod is sleeved with an upper buffer spring, the bottom end of the buffer rod is fixedly connected with a contact bottom rod, and the lower position of the outer side of the contact bottom rod is fixedly provided with a buffer seat. The moisture protection of the camera is improved.

Description

Aerial photography device for state and soil resource monitoring pipe

Technical Field

The utility model relates to the technical field of aerial photography equipment, in particular to an aerial photography device for a national resource monitoring device.

Background

The national soil resource is a material foundation which is relied on by the nation and residents thereof to live, and is a material entity composed of natural resources and social and economic resources, the narrowly defined national soil resource only comprises natural resources such as land, rivers, lakes and seas, mineral resources, organisms, climate and the like, the generalized national soil resource also comprises population resources and social and economic resources, and in China, the national soil resource generally adopts the narrowly defined resource and mainly comprises land, mineral resources, ocean and surveying and mapping geographic information resources, so that an aerial photography device is required to be used when the national soil resource is supervised, and in the Chinese patent with the patent number of 202020535766.0, the aerial photography device for the national soil resource supervision is specifically mentioned, so that the whole device can be more conveniently carried and used, the practicability of the whole device is improved, and the better use prospect is brought.

However, when the aerial photography device for monitoring the homeland resources is used, the aerial photography device descends and falls off accidentally, the support cannot perform good buffer protection on the aerial photography device, so that the vibration is transmitted to the aerial photography device too much, and the subsequent use of the aerial photography device is influenced.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an aerial photographing device for a national resource monitoring pipe, and aims to solve the problems that when the aerial photographing device provided by the background technology is descended and accidentally falls, a support cannot perform good buffering protection on the aerial photographing device, so that excessive vibration is transmitted to the aerial photographing device, and the subsequent use of the aerial photographing device is affected.

In order to achieve the purpose, the utility model provides the following technical scheme: an aerial photography device for a state soil resource monitoring pipe comprises an unmanned aerial vehicle main body, wherein a buffering support mechanism is mounted at the bottom end of the unmanned aerial vehicle main body, and the buffering support mechanism is mainly formed by combining a support frame, a buffering rod for buffering protection, an upper buffering spring, a contact base and a lower buffering spring;

the bottom end of the unmanned aerial vehicle main body is provided with a shooting protection mechanism, and the shooting protection mechanism is mainly formed by combining a camera, a first protection bin, a second protection bin and an activated carbon plate, wherein the first protection bin, the second protection bin and the activated carbon plate are used for moisture protection;

counterweight adjustment mechanism is installed to the bottom of unmanned aerial vehicle main part, counterweight adjustment mechanism mainly forms by the counter weight storehouse and be used for pressing down stable spring telescopic link and pressing the platen combination.

Preferably, the buffer support mechanism comprises a support frame, a buffer rod, an upper buffer spring, a contact bottom rod, a buffer seat, a buffer groove, a contact seat, a buffer connecting rod, a buffer moving plate and a lower buffer spring;

the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle main part, buffer spring, buffer seat, buffer connecting rod, buffer seat, buffer connecting rod, buffer spring, buffer rod's bottom fixedly connected with contact sill bar, the outside below position department fixed mounting of support frame, buffer seat has been seted up in the outside of buffer sill, the contact seat has been placed to the inboard of buffer seat, the even symmetrical fixed mounting in top inner wall of buffer seat has the buffering connecting rod, the top inner wall of contact seat corresponds the inboard position department fixedly connected with buffering of buffer seat and moves the board, the outside of buffering connecting rod corresponds buffering and moves board top position department and has cup jointed lower buffer spring.

Preferably, the bottom end of the buffer connecting rod penetrates through the buffer moving plate to be fixedly connected with the inner wall of the bottom end of the contact base, and the buffer moving plate is in sliding connection with the buffer connecting rod.

Preferably, the shooting protection mechanism comprises a camera, a first protection bin, a second protection bin, an embedded plate and an activated carbon plate;

the camera is installed to the bottom of unmanned aerial vehicle main part, first protection storehouse has been placed in the outside of camera, the outside of camera corresponds first protection storehouse one side position department and has placed second protection storehouse, the embedding board is installed in the one end embedding in second protection storehouse, the one end of embedding board corresponds the inboard position department in second protection storehouse and has attached the active carbon board.

Preferably, the embedded plate and the second protection bin are fixed through bolts, and a sealing gasket is arranged at the joint of the first protection bin and the second protection bin.

Preferably, the counterweight adjusting mechanism comprises a fixed plate, a counterweight bin, a spring telescopic rod, a pressing plate and a counterweight block;

the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle main part, counterweight storehouse, spring telescopic link, counterweight storehouse, fixed plate's bottom symmetry fixed mounting has the fixed plate, counterweight storehouse has been placed to the bottom of fixed plate, the even fixedly connected with spring telescopic link in bottom of fixed plate, spring telescopic link's bottom fixedly connected with presses the clamp plate, the balancing weight has evenly been placed to counterweight storehouse's inside.

Preferably, a rubber gasket is attached to the bottom end of the pressing plate, and the fixing plate and the counterweight cabin are fixed through bolts.

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

1. through the buffering supporting mechanism who sets up, can be to the twice buffering of vibrations when unmanned aerial vehicle main part contacts with ground to reduced the vibrations that transmit to the unmanned aerial vehicle main part, be convenient for carry out the buffering protection to the unmanned aerial vehicle main part, reduced when reducing the descending vibrations to the inside damage that causes of unmanned aerial vehicle main part.

2. Through the shooting protection mechanism who sets up, can use first protection storehouse and second protection storehouse to protect the camera to can carry out moisture absorption protection around the camera, increase the outside protection when the camera uses, also reduce the surrounding gas humidity when the camera uses, improve the dampproofing protection to the camera.

3. Through the counterweight adjustment mechanism who sets up, can press the balancing weight after placing, guaranteed the stability after the balancing weight is placed, be convenient for carry out the counter weight adjustment when using this aerial photography device for homeland resource monitoring, also improved the stability after the configuration replay.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.

FIG. 1 is a schematic structural diagram of an aerial photography device for a national resource monitoring of the present invention;

FIG. 2 is a schematic illustration of an explosive structure of the present invention;

FIG. 3 is a schematic structural view of the cushion support mechanism of the present invention;

FIG. 4 is a schematic view of the mounting arrangement of the damping link and the damping mount of the present invention;

FIG. 5 is a schematic view of the construction of the photographing protecting mechanism according to the present invention;

FIG. 6 is a schematic structural view of the counterweight adjustment mechanism of the present invention;

in the drawings, the components represented by the respective reference numerals are listed below:

1. an unmanned aerial vehicle main body;

2. a buffer support mechanism; 201. a support frame; 202. a buffer rod; 203. an upper buffer spring; 204. a contact bottom bar; 205. a buffer seat; 206. a buffer tank; 207. a contact base; 208. a buffer connecting rod; 209. buffering the moving plate; 210. a lower buffer spring;

3. a shooting protection mechanism; 301. a camera; 302. a first protection bin; 303. a second protection bin; 304. a built-in plate; 305. an activated carbon plate;

4. a counterweight adjustment mechanism; 401. a fixing plate; 402. a counterweight cabin; 403. a spring telescopic rod; 404. a pressing plate; 405. and a balancing weight.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The utility model provides a technical scheme that: an aerial photography device for a territorial resource monitoring, as shown in fig. 1, fig. 2, fig. 3 and fig. 4, comprises an unmanned aerial vehicle main body 1, wherein a buffering support mechanism 2 is installed at the bottom end of the unmanned aerial vehicle main body 1, and the buffering support mechanism 2 comprises a support frame 201, a buffering rod 202, an upper buffering spring 203, a contact bottom rod 204, a buffering seat 205, a buffering groove 206, a contact seat 207, a buffering connecting rod 208, a buffering moving plate 209 and a lower buffering spring 210;

the bottom end of the unmanned aerial vehicle main body 1 is symmetrically and fixedly provided with a supporting frame 201, the bottom end of the supporting frame 201 is embedded into a buffer rod 202 in a sliding manner, the outer side of the buffer rod 202 is sleeved with an upper buffer spring 203, the bottom end of the buffer rod 202 is fixedly connected with a contact bottom rod 204, the lower position of the outer side of the contact bottom rod 204 is fixedly provided with a buffer seat 205, the bottom end of the buffer seat 205 is provided with a buffer groove 206, the inner side of the buffer groove 206 is provided with a contact seat 207, the inner wall of the top end of the buffer seat 205 is uniformly and symmetrically and fixedly provided with a buffer connecting rod 208, the inner wall of the top end of the contact seat 207 is fixedly connected with a buffer moving plate 209 corresponding to the inner side position of the buffer groove 206, the outer side of the buffer connecting rod 208 is sleeved with a lower buffer spring 210 corresponding to the top end of the buffer moving plate 209, the bottom end of the buffer connecting rod 208 penetrates through the buffer moving plate 209 to be fixedly connected with the inner wall of the bottom end of the contact seat 207, the buffer moving plate 209 is in a sliding manner, the buffer moving plate 209 can move along the buffer connecting rod 208, and the lower buffer spring 210 can be driven to contract.

This aerial photography device for territory resource monitoring uses during the use, unmanned aerial vehicle main part 1 descends to subaerial back, contact base 207 at first can with ground contact, it moves board 209 along buffering connecting rod 208 to move up to drive the buffering, make buffer spring 210 shrink down, can cushion the vibrations when unmanned aerial vehicle main part 1 contacts with ground, combine buffer beam 202 to get into in the support frame 201, can drive the shrink of buffer spring 203, further cushion the vibrations when contacting with ground to unmanned aerial vehicle main part 1, can reduce the vibrations that transmit to unmanned aerial vehicle main part 1, thereby carry out the buffer protection to unmanned aerial vehicle main part 1, the damage of vibrations to the inside of unmanned aerial vehicle main part 1 that causes when having reduced to descend.

As shown in fig. 5, the bottom end of the main body 1 of the unmanned aerial vehicle is provided with a shooting protection mechanism 3, and the shooting protection mechanism 3 comprises a camera 301, a first protection cabin 302, a second protection cabin 303, an embedded plate 304 and an activated carbon plate 305;

camera 301 is installed to unmanned aerial vehicle main part 1's bottom, first protection storehouse 302 has been placed in camera 301's the outside, second protection storehouse 303 has been placed to the outside of camera 301 corresponding first protection storehouse 302 one side position department, the embedding board 304 is installed in the one end embedding of second protection storehouse 303, the inboard position department of the one end corresponding second protection storehouse 303 of embedding board 304 is pasted and is had activated carbon plate 305, it fixes through the bolt between board 304 and the second protection storehouse 303 to embed, seal ring is installed with the junction of second protection storehouse 303 to first protection storehouse 302, be convenient for embed the installation and the dismantlement between board 304 and the second protection storehouse 303.

When this aerial photography device for homeland resource monitoring uses, can use camera 301 to take photo by plane, and first protection storehouse 302 and the second protection storehouse 303 in the accessible camera 301 outside, protect camera 301, combine the activated carbon board 305 of embedding board 304 one end, can protect the gas between storehouse 302 and the second protection storehouse 303 and carry out moisture absorption protection, outside protection when having increased camera 301 and using, the surrounding gas humidity when also having reduced camera 301 and using, the dampproofing protection to camera 301 has been improved.

As shown in fig. 6, a counterweight adjusting mechanism 4 is installed at the bottom end of the main body 1 of the unmanned aerial vehicle, and the counterweight adjusting mechanism 4 includes a fixing plate 401, a counterweight cabin 402, a spring telescopic rod 403, a pressing plate 404 and a counterweight 405;

there is fixed plate 401 bottom symmetry fixed mounting of unmanned aerial vehicle main part 1, counter weight storehouse 402 has been placed to fixed plate 401's bottom, the even fixedly connected with spring telescopic link 403 in bottom of fixed plate 401, the bottom fixedly connected with of spring telescopic link 403 presses down board 404, counter weight 405 has evenly been placed to the inside in counter weight storehouse 402, the bottom of pressing down board 404 is attached to have the rubber packing piece, fix through the bolt between fixed plate 401 and the counter weight storehouse 402, the frictional force when having improved and pressing down board 404 bottom and the contact of counter weight 405.

Before this homeland resources are monitored and are used with device of taking photo by plane, can take off counter weight storehouse 402, arrange balancing weight 405 in counter weight storehouse 402, fix between counter weight storehouse 402 and fixed plate 401 again, make and press down board 404 and balancing weight 405 contact, drive spring telescopic link 403 shrink, can press down balancing weight 405, the stability after balancing weight 405 has been guaranteed, be convenient for carry out the counter weight adjustment when using this homeland resources are monitored and are used with device of taking photo by plane, the stability after balancing weight 405 has also been improved.

In the description herein, references to the description of "one embodiment," "an example," "a specific example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

The preferred embodiments of the utility model disclosed above are intended to be illustrative only. The preferred embodiments are not intended to be exhaustive or to limit the utility model to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best utilize the utility model. The utility model is limited only by the claims and their full scope and equivalents.

Claims

1. The utility model provides a device of taking photo by plane for homeland resource monitoring, includes unmanned aerial vehicle main part (1), its characterized in that: the bottom end of the unmanned aerial vehicle main body (1) is provided with a buffering support mechanism (2), and the buffering support mechanism (2) is mainly formed by combining a support frame (201), a buffering rod (202) for buffering protection, an upper buffering spring (203), a contact seat (207) and a lower buffering spring (210);

the bottom end of the unmanned aerial vehicle main body (1) is provided with a shooting protection mechanism (3), and the shooting protection mechanism (3) is mainly formed by combining a camera (301), a first protection cabin (302) for damp-proof protection, a second protection cabin (303) and an activated carbon plate (305);

counterweight adjusting mechanism (4) are installed to the bottom of unmanned aerial vehicle main part (1), counterweight adjusting mechanism (4) mainly by counterweight storehouse (402) and be used for pressing stable spring telescopic link (403) and press board (404) combination to form.

2. The aerial photography device for the territorial resource monitoring according to claim 1, wherein: the buffer support mechanism (2) comprises a support frame (201), a buffer rod (202), an upper buffer spring (203), a contact bottom rod (204), a buffer seat (205), a buffer groove (206), a contact seat (207), a buffer connecting rod (208), a buffer moving plate (209) and a lower buffer spring (210);

the bottom end of the unmanned aerial vehicle main body (1) is symmetrically and fixedly provided with supporting frames (201), the bottom end of the supporting frame (201) is embedded with a buffer rod (202) in a sliding way, the outer side of the buffer rod (202) is sleeved with an upper buffer spring (203), the bottom end of the buffer rod (202) is fixedly connected with a contact bottom rod (204), a buffer seat (205) is fixedly arranged at the lower position of the outer side of the contact bottom rod (204), the bottom end of the buffer seat (205) is provided with a buffer groove (206), the inner side of the buffer groove (206) is provided with a contact seat (207), the inner wall of the top end of the buffer seat (205) is uniformly and symmetrically fixedly provided with buffer connecting rods (208), a buffer moving plate (209) is fixedly connected to the inner wall of the top end of the contact seat (207) at a position corresponding to the inner side of the buffer groove (206), the outer side of the buffer connecting rod (208) is sleeved with a lower buffer spring (210) corresponding to the top end of the buffer moving plate (209).

3. The aerial photography device for the territorial resource monitoring according to claim 2, wherein: the bottom end of the buffer connecting rod (208) penetrates through the buffer moving plate (209) to be fixedly connected with the inner wall of the bottom end of the contact seat (207), and the buffer moving plate (209) is in sliding connection with the buffer connecting rod (208).

4. The aerial photography device for the territorial resource monitoring according to claim 1, wherein: the shooting protection mechanism (3) comprises a camera (301), a first protection cabin (302), a second protection cabin (303), an embedded plate (304) and an activated carbon plate (305);

camera (301) are installed to the bottom of unmanned aerial vehicle main part (1), first protection storehouse (302) have been placed in the outside of camera (301), the outside of camera (301) corresponds first protection storehouse (302) one side position department and has placed second protection storehouse (303), the one end embedding in second protection storehouse (303) is installed and is inlayed board (304), the one end of inlaying board (304) corresponds second protection storehouse (303) inboard position department and pastes and have activated carbon plate (305).

5. The aerial photography device for the territorial resource monitoring according to claim 4, wherein: the embedded plate (304) and the second protection bin (303) are fixed through bolts, and a sealing gasket is arranged at the joint of the first protection bin (302) and the second protection bin (303).

6. The aerial photography device for the territorial resource monitoring according to claim 1, wherein: the counterweight adjusting mechanism (4) comprises a fixing plate (401), a counterweight bin (402), a spring telescopic rod (403), a pressing plate (404) and a counterweight (405);

the bottom symmetry fixed mounting of unmanned aerial vehicle main part (1) has fixed plate (401), counter weight storehouse (402) have been placed to the bottom of fixed plate (401), the even fixedly connected with spring telescopic link in bottom of fixed plate (401) spring telescopic link (403), the bottom fixedly connected with of spring telescopic link (403) presses clamp plate (404), balancing weight (405) have evenly been placed to the inside in counter weight storehouse (402).

7. The aerial photography device for the territorial resource monitoring of claim 6, wherein: the bottom end of the pressing plate (404) is attached with a rubber gasket, and the fixing plate (401) and the counterweight cabin (402) are fixed through bolts.