CN220391540U

CN220391540U - Unmanned aircraft

Info

Publication number: CN220391540U
Application number: CN202321592758.XU
Authority: CN
Inventors: 袁侃
Original assignee: Jiangsu Hexiang Rongsheng Information Technology Co ltd
Current assignee: Jiangsu Hexiang Rongsheng Information Technology Co ltd
Priority date: 2023-06-21
Filing date: 2023-06-21
Publication date: 2024-01-26
Anticipated expiration: 2033-06-21

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle, which comprises a main body mechanism, a mounting mechanism and a camera shooting mechanism, wherein the mounting mechanism is positioned at the side of the lower end of the main body mechanism, the camera shooting mechanism is positioned at the inner side of the mounting mechanism, the camera shooting mechanism comprises a camera, a mounting block, a connecting groove, a movable rod, a clamp spring, a positioning groove, a connecting spring, a positioning block and a limiting block, the mounting block is fixedly arranged at the left end and the right end of the camera, the connecting groove is fixedly arranged in the middle of the outer end of the mounting block, the movable groove is fixedly arranged at the lower end of the mounting block and is communicated with the connecting groove, and the movable rod is movably arranged in the movable groove. This unmanned aircraft, compression set of jump ring makes the inner of movable rod contract to the inside of movable groove below during operation, increases movable rod simple operation from this, and the setting of movable rod, makes the camera more convenient when the dismouting.

Description

Unmanned aircraft

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle.

Background

Unmanned aircraft are also known as drones, and drones are unmanned planes that are operated by radio remote control devices and self-contained programming, or are operated autonomously, either entirely or intermittently.

Because unmanned aerial vehicle unmanned, consequently unmanned aerial vehicle all can carry the camera when flying in the air, the real-time observation of operating personnel of being convenient for, the camera of carrying on the unmanned aerial vehicle generally, the angle is fixed after the installation, can not adjust from top to bottom according to special circumstances, has restricted the suitability of camera in the air from this.

In order to solve the above problems, the prior art has the advantages that the camera can be adjusted up and down under special conditions by arranging the adjustable structure, but in actual operation, parts such as fixing bolts are required to be used for installing the camera, the disassembly is inconvenient, the parts such as bolts lose the grasping property after repeated disassembly, and therefore the safety of the use of the camera after subsequent installation is improved.

Disclosure of Invention

(one) solving the technical problems

The utility model aims to provide an unmanned aerial vehicle, which solves the problems that in the prior art, parts such as a fixing bolt are required to be used for installing a camera and the like, and the disassembly is very inconvenient.

(II) technical scheme

In order to achieve the above purpose, the present utility model provides the following technical solutions: unmanned aircraft, including main part mechanism, installation mechanism and camera mechanism, installation mechanism is located the avris of main part mechanism lower extreme, camera mechanism is located the inboard of installation mechanism, camera mechanism is including camera, installation piece, spread groove, movable rod, jump ring, constant head tank, coupling spring, locating piece and stopper, installation piece fixed mounting is at the left and right sides both ends of camera, the fixed middle part that sets up at the installation piece outer end of spread groove, the fixed lower extreme that sets up at the installation piece of movable groove and with the spread groove intercommunication, movable rod movable mounting is in the inside of movable groove, jump ring fixed mounting is in the below of movable rod middle part and with the inner fixed connection of movable groove, the fixed inside that sets up the movable rod top of constant head tank, coupling spring movable mounting is in the inside of constant head tank, locating piece movable mounting is in the inside of constant head tank and the outer fixed connection of coupling spring, stopper fixed setting is in the upper end of installation piece and is located the avris of movable groove.

Preferably, the main part mechanism is including aircraft main part, aircraft, support frame, built-in groove, buffer spring, horizontal pole and protection piece, aircraft fixed mounting is in the avris of aircraft main part upper end, support frame fixed mounting is in the avris of aircraft main part lower extreme, the inside of built-in groove fixed setting in the support frame below, buffer spring fixed mounting is in the top of built-in inslot end, horizontal pole movable mounting is in the inside of built-in groove and with buffer spring's lower extreme fixed connection, protection piece fixed mounting is in the avris of horizontal pole lower extreme, through setting up buffer spring, when the device falls to the ground, but buffer support frame and the contact force on ground avoid hard contact to cause gravity impact damage.

Preferably, the installation mechanism comprises an assembly frame, an adjusting groove, a rotating shaft, a screw rod, a connecting block and a clamping groove, wherein the adjusting groove is fixedly arranged in the middle of the assembly frame, the rotating shaft is fixedly arranged on the upper side and the lower side of the inside of the adjusting groove, the screw rod is fixedly arranged at the inner end of the rotating shaft, the connecting block is movably arranged at the outer end of the screw rod, the clamping groove is fixedly arranged in the inside of the connecting block, the rotating shaft can drive the screw rod to drive the connecting block to move in an up-down thread manner, therefore, a part connected with the connecting block can be adjusted in use, and the arrangement of the structure increases the applicability of the device in air flight.

Preferably, the camera movable mounting is in the middle part of aircraft main part lower extreme, the installation piece is the symmetric distribution in the left and right sides both ends of camera, the middle part of movable rod is cross structure, the jump ring is the symmetric distribution in the left and right sides of movable rod middle part below, through setting up the jump ring, the compression set of jump ring makes the inside of movable rod shrink to the inside of movable groove below in the time of the operation, increase movable rod simple operation nature from this.

Preferably, the locating piece is T type structure, the locating piece is symmetrical distribution in the left and right sides both ends of connecting spring, locating piece and stopper looks adaptation, the stopper is annular structure, and the setting of locating piece makes movable rod be fixed after connecting block and installation piece, avoids the device to do both separation when big action in the sky.

Preferably, the number of the supporting frames is four, the buffer springs are equidistantly distributed above the inner ends of the built-in grooves, the lower ends of the protection blocks are arc-shaped structures, and the arc-shaped structures are better in applicability on contact surfaces.

Preferably, the assembly frame is fixedly installed at the lower end of the aircraft main body and is positioned at the inner side of the supporting frame, the connecting block and the screw rod are in threaded connection, the connecting block is of a T-shaped structure, the clamping grooves are matched with the inner ends of the movable rods, the connecting block is of a T-shaped structure, the connecting block is enabled to be connected with the mounting blocks at the two ends of the camera, and then the stability of the assembly frame is maintained, so that the stability of the connection of the camera is further improved.

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

1. according to the unmanned aircraft, the inner end of the movable rod is contracted to the inside below the movable groove by compression deformation of the clamp spring during operation, so that the operation convenience of the movable rod is improved, and the movable rod is arranged, so that the camera can keep good convenience during assembly;

2. according to the unmanned aircraft, the connecting block is of the T-shaped structure, so that the connecting block is connected with the mounting blocks at the two ends of the camera to keep the stability of the assembly frame, the stability of the connection of the camera is further improved, meanwhile, the screw rod is connected with the connecting block through threads, the camera can be adjusted up and down according to the requirement, and the use convenience of the camera is improved;

3. this unmanned aircraft sets up the lower extreme of protection piece into arc structure, and arc structure suitability is better on the contact surface to can nimble change the contact surface, increase the protectiveness when the device falls to the ground from this.

Drawings

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

FIG. 2 is a schematic cross-sectional view of the present utility model;

FIG. 3 is an enlarged schematic view of the structure of FIG. 2A according to the present utility model;

fig. 4 is an enlarged view of the structure of fig. 2B according to the present utility model.

In the figure: 1. a main body mechanism; 101. an aircraft body; 102. an aircraft; 103. a support frame; 104. a built-in groove; 105. a buffer spring; 106. a cross bar; 107. a protective block; 2. a mounting mechanism; 201. an assembly frame; 202. an adjustment tank; 203. a rotating shaft; 204. a screw rod; 205. a connecting block; 206. a clamping groove; 3. an image pickup mechanism; 301. a camera; 302. a mounting block; 303. a connecting groove; 304. a movable groove; 305. a movable rod; 306. clamping springs; 307. a positioning groove; 308. a connecting spring; 309. a positioning block; 310. and a limiting block.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-4, the present utility model provides the following technical solutions: the unmanned aerial vehicle comprises a main body mechanism 1, a mounting mechanism 2 and a camera shooting mechanism 3, wherein the mounting mechanism 2 is positioned at the side of the lower end of the main body mechanism 1, the camera shooting mechanism 3 is positioned at the inner side of the mounting mechanism 2, the camera shooting mechanism 3 comprises a camera 301, a mounting block 302, a connecting groove 303, a movable groove 304, a movable rod 305, a clamp spring 306, a positioning groove 307, a connecting spring 308, a positioning block 309 and a limiting block 310, the mounting block 302 is fixedly arranged at the left end and the right end of the camera 301, the connecting groove 303 is fixedly arranged in the middle of the outer end of the mounting block 302, the movable groove 304 is fixedly arranged at the lower end of the mounting block 302 and is communicated with the connecting groove 303, the movable rod 305 is movably arranged in the inside of the movable groove 304, the clamp spring 306 is fixedly arranged below the middle of the movable rod 305 and is fixedly connected with the inner end of the movable groove 304, the positioning groove 307 is fixedly arranged in the inside of the upper part of the movable rod 305, the positioning spring 308 is movably arranged in the positioning groove 307, the positioning block 309 is movably arranged in the positioning groove 307 is fixedly connected with the outer end of the connecting spring 308, and the limiting block 310 is fixedly arranged at the upper end of the mounting block 302 and is positioned at the side of the movable groove 304;

the main body mechanism 1 comprises an aircraft main body 101, an aircraft 102, a support frame 103, a built-in groove 104, a buffer spring 105, a cross rod 106 and a protection block 107, wherein the aircraft 102 is fixedly arranged on the side of the upper end of the aircraft main body 101, the support frame 103 is fixedly arranged on the side of the lower end of the aircraft main body 101, the built-in groove 104 is fixedly arranged in the lower part of the support frame 103, the buffer spring 105 is fixedly arranged above the inner end of the built-in groove 104, the cross rod 106 is movably arranged in the built-in groove 104 and is fixedly connected with the lower end of the buffer spring 105, the protection block 107 is fixedly arranged on the side of the lower end of the cross rod 106, and by arranging the buffer spring 105, when the device falls to the ground, the contact force between the support frame 103 and the ground can be buffered, and gravity impact damage caused by hard contact is avoided; the installation mechanism 2 comprises an assembly frame 201, an adjusting groove 202, a rotating shaft 203, a screw rod 204, a connecting block 205 and a clamping groove 206, wherein the adjusting groove 202 is fixedly arranged in the middle of the assembly frame 201, the rotating shaft 203 is fixedly arranged on the upper side and the lower side of the inside of the adjusting groove 202, the screw rod 204 is fixedly arranged at the inner end of the rotating shaft 203, the connecting block 205 is movably arranged at the outer end of the screw rod 204, the clamping groove 206 is fixedly arranged in the inside of the connecting block 205, the rotating shaft 203 can drive the screw rod 204 to drive the connecting block 205 to move up and down in a threaded manner, therefore, the components connected with the connecting block 205 can be adjusted in use, and the arrangement of the structure increases the applicability of the components of the device in air flight;

the camera 301 is movably arranged in the middle of the lower end of the aircraft main body 101, the mounting blocks 302 are symmetrically distributed at the left end and the right end of the camera 301, the middle of the movable rod 305 is of a cross-shaped structure, the clamp springs 306 are symmetrically distributed at the left side and the right side below the middle of the movable rod 305, and the inner end of the movable rod 305 is contracted inwards to the inside below the movable groove 304 by the compression deformation of the clamp springs 306 during operation through arranging the clamp springs 306, so that the operation convenience of the movable rod 305 is improved, and the movable rod 305 is arranged, so that the camera 301 can keep better convenience during assembly; the positioning block 309 is of a T-shaped structure, the positioning block 309 is symmetrically distributed at the left end and the right end of the connecting spring 308, the positioning block 309 is matched with the limiting block 310, the limiting block 310 is of an annular structure, the movable rod 305 is fixed after connecting the connecting block 205 with the mounting block 302, the two are prevented from being separated when the device performs large actions in the air, and the positioning block 309 of the T-shaped structure cannot be separated from the positioning groove 307 when playing a role, so that the mounting stability of the camera 301 is improved; the number of the supporting frames 103 is four, the buffer springs 105 are equidistantly distributed above the inner end of the built-in groove 104, the lower end of the protection block 107 is of an arc-shaped structure, the arc-shaped structure has better applicability on a contact surface, and the contact surface can be flexibly changed, so that the protection performance of the device in landing is improved; the assembly frame 201 is fixedly installed at the lower end of the aircraft main body 101 and is located at the inner side of the supporting frame 103, the connecting block 205 and the screw rod 204 are in threaded connection, the connecting block 205 is of a T-shaped structure, the clamping groove 206 is matched with the inner end of the movable rod 305, the connecting block 205 is of a T-shaped structure, the connecting block is enabled to be connected with the mounting blocks 302 at the two ends of the camera 301, stability of connection of the camera 301 is further improved, meanwhile, the screw rod 204 and the connecting block 205 are in threaded connection, the camera 301 can be adjusted up and down according to requirements, and convenience in use of the camera 301 is improved.

Working principle: according to the technical scheme, the unmanned aircraft is characterized in that an adjusting groove 202 is arranged in an assembly frame 201, a rotating shaft 203 and a screw rod 204 are installed in the adjusting groove 202, a connecting block 205 with a T-shaped structure is inserted through the adjusting groove 202 and the screw rod 204 in a threaded mode, at the moment, the camera 301 is placed corresponding to the inner side of the assembly frame 201, the connecting block 205 is correspondingly inserted into a connecting groove 303 in a mounting block 302 arranged at the left end and the right end of the camera 301, the movable rod 305 is manually forced downwards during insertion, the inner end of the movable rod 305 is contracted to the inner side below a movable groove 304 through compression deformation of a clamp spring 306, when a clamping groove 206 arranged in the connecting block 205 corresponds to the movable rod 305, the camera 301 can be fixedly installed in the middle of the lower end of the aircraft body 101 through rapid reset of the clamping groove 206, in the structure, the positioning block 309 is arranged, the movable rod 305 is fixedly connected with the connecting block 302, the two positioning blocks are prevented from being separated when the device is in large motion, the space 309 is not separated from the rotating shaft 205, and the connecting block 205 is not separated from the rotating shaft 203 when the connecting block is in the space, and the space is fixedly arranged on the connecting block body, and the connecting block is stably connected with the connecting block 204.

Finally, it should be noted that the above description is only for illustrating the technical solution of the present utility model, and not for limiting the scope of the present utility model, and that the simple modification and equivalent substitution of the technical solution of the present utility model can be made by those skilled in the art without departing from the spirit and scope of the technical solution of the present utility model.

Claims

1. Unmanned aircraft, including main part mechanism (1), installation mechanism (2) and mechanism (3) of making a video recording, its characterized in that: the installation mechanism (2) is positioned at the side of the lower end of the main body mechanism (1), the camera shooting mechanism (3) is positioned at the inner side of the installation mechanism (2), the camera shooting mechanism (3) comprises a camera (301), an installation block (302), a connecting groove (303), a movable groove (304), a movable rod (305), a clamp spring (306), a positioning groove (307), a connecting spring (308), a positioning block (309) and a limiting block (310), the installation block (302) is fixedly arranged at the left end and the right end of the camera (301), the connecting groove (303) is fixedly arranged in the middle of the outer end of the installation block (302), the movable groove (304) is fixedly arranged at the lower end of the installation block (302) and is communicated with the connecting groove (303), the movable rod (305) is movably arranged in the movable groove (304), the clamp spring (306) is fixedly arranged below the middle of the movable rod (305) and is fixedly connected with the inner end of the movable groove (304), the positioning groove (307) is fixedly arranged in the upper part of the movable rod (305), the connecting spring (307) is fixedly arranged at the inner end of the positioning groove (308) and is fixedly connected with the inner end of the positioning block (308), the limiting block (310) is fixedly arranged at the upper end of the mounting block (302) and is positioned at the side of the movable groove (304).

2. The unmanned aerial vehicle of claim 1, wherein: the main body mechanism (1) comprises an aircraft main body (101), an aircraft (102), a supporting frame (103), an inner groove (104), a buffer spring (105), a cross rod (106) and a protection block (107), wherein the aircraft (102) is fixedly arranged on the side of the upper end of the aircraft main body (101), the supporting frame (103) is fixedly arranged on the side of the lower end of the aircraft main body (101), the inner groove (104) is fixedly arranged in the lower part of the supporting frame (103), the buffer spring (105) is fixedly arranged above the inner end of the inner groove (104), the cross rod (106) is movably arranged in the inner groove (104) and is fixedly connected with the lower end of the buffer spring (105), and the protection block (107) is fixedly arranged on the side of the lower end of the cross rod (106).

3. The unmanned aerial vehicle of claim 2, wherein: the mounting mechanism (2) comprises an assembly frame (201), an adjusting groove (202), a rotating shaft (203), a screw rod (204), a connecting block (205) and a clamping groove (206), wherein the adjusting groove (202) is fixedly arranged in the middle of the assembly frame (201), the rotating shaft (203) is fixedly arranged on the upper side and the lower side of the inner portion of the adjusting groove (202), the screw rod (204) is fixedly arranged at the inner end of the rotating shaft (203), the connecting block (205) is movably arranged at the outer end of the screw rod (204), and the clamping groove (206) is fixedly arranged in the inner side of the connecting block (205).

4. An unmanned aerial vehicle according to claim 3, wherein: the camera (301) movable mounting is in the middle of aircraft main part (101) lower extreme, installation piece (302) are symmetrical distribution in the left and right sides both ends of camera (301), the middle part of movable rod (305) is cross structure, jump ring (306) are symmetrical distribution in the left and right sides of movable rod (305) middle part below.

5. The unmanned aerial vehicle of claim 4, wherein: the positioning block (309) is of a T-shaped structure, the positioning block (309) is symmetrically distributed at the left end and the right end of the connecting spring (308), the positioning block (309) is matched with the limiting block (310), and the limiting block (310) is of an annular structure.

6. The unmanned aerial vehicle of claim 5, wherein: the number of the supporting frames (103) is four, the buffer springs (105) are distributed above the inner ends of the built-in grooves (104) at equal intervals, and the lower ends of the protection blocks (107) are arc-shaped structures.

7. The unmanned aerial vehicle of claim 6, wherein: the assembly frame (201) is fixedly arranged at the lower end of the aircraft main body (101) and is positioned at the inner side of the supporting frame (103), the connecting block (205) and the screw rod (204) are in threaded connection, the connecting block (205) is of a T-shaped structure, and the clamping groove (206) is matched with the inner end of the movable rod (305).