CN212980525U

CN212980525U - Floated device of taking photo by plane

Info

Publication number: CN212980525U
Application number: CN202021583719.XU
Authority: CN
Inventors: 汪宗成
Original assignee: Harbin Zerenxin Technology Co ltd
Current assignee: Harbin Zerenxin Technology Co ltd
Priority date: 2020-08-03
Filing date: 2020-08-03
Publication date: 2021-04-16
Anticipated expiration: 2030-08-03

Abstract

The utility model discloses a floated device of taking photo by plane, its structure includes automatically controlled box, frame, organism, frame, lubricating structure, pivot, conduction axle, the frame that falls to the ground, many rotors, the utility model discloses an unmanned aerial vehicle flies through the many rotors of conduction axle combination, and conduction axle surface recess is equipped with embedded lubricating structure, and the supporter combination of rigid coupling installed part is equipped with the oiling pipe, and the outer end opening passes through the closing cap involution, and lubricating oil is stored inside the oiling pipe, when exporting to the guiding gutter of the integrative constitution of wide structure between spacing piece on both sides, spills over through the constant current piece trace before flowing out from the oil-out, has fluid current-limiting effect, can effectively improve the lubricating property of rotating part operation, and then improves the performance of unmanned aerial vehicle part.

Description

Floated device of taking photo by plane

Technical Field

The utility model relates to a floated device of taking photo by plane belongs to unmanned air vehicle technique field.

Background

Unmanned aerial vehicle uses extensively and uses in a plurality of fields, and aerial operation adopts unmanned aerial vehicle to carry out work like taking photo by plane, scouting or search and rescue, and floated unmanned aerial vehicle that takes photo by plane provides the flight power energy through the battery.

The device that takes photo by plane of current floated utilizes the rotor flight aloft, and the high-speed turning force increases the part friction, accelerates blade rotation loss easily, and then influences unmanned aerial vehicle's that takes photo by plane suspension performance.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art exists, the utility model aims at providing a floated device of taking photo by plane to solve current floated device of taking photo by plane and utilize the rotor flight aloft, fast-speed turning force increases the part friction, accelerates blade rotation loss easily, and then influences the problem of unmanned aerial vehicle's suspension performance of taking photo by plane.

In order to achieve the above purpose, the present invention is realized by the following technical solution: the utility model provides a floated device of taking photo by plane, its structure includes automatically controlled box, frame, organism, frame, lubricating structure, pivot, conduction axle, the frame that falls, many rotors, be equipped with the embedded frame that is located the structure groove between two parties on the organism, automatically controlled box sets the cross middle part position department that corresponds the frame, conduction axle surface groove looks joint pivot, the pivot correspondence sets many rotors surface groove, the frame both sides diapire position has installed the frame that falls, conduction axle surface recess is equipped with embedded lubricating structure.

Further, lubricating structure includes closed cover, notes oil pipe, supporter, spacing piece, guiding gutter, constant current piece, oil-out, installed part, closed cover establishes soon on the outer groove in notes oil pipe surface, notes oil pipe opening looks rigid coupling is on the local recess of supporter, the supporter passes through the installation part combination wall and connects the conduction axle, spacing piece surface local position is equipped with continuous constant current piece, constant current piece combination oil-out looks rigid coupling, the guiding gutter comprises the wide structure an organic whole between the spacing piece in both sides, the oil-out is linked together the conduction axle inner wall.

Further, the multiple rotors are mounted on corresponding outer end groove surfaces of the frame structure.

Furthermore, the frame combination electric control box is assembled and connected into a whole.

Furthermore, the position of the outer end groove corresponding to the rack is provided with a conduction shaft.

Further, the frame mount is located at a frame structure centering groove.

Furthermore, the diversion trench is communicated with the inner channel of the oil injection pipe.

Further, the flow-fixing piece is a liquid-filled overflow accessory.

Advantageous effects

The utility model relates to a floated device of taking photo by plane, unmanned aerial vehicle flies through many rotors of conduction axle combination, conduction axle surface recess is equipped with embedded lubricating structure, the supporter combination of rigid coupling installed part is equipped with the oiling pipe, the outer end opening passes through the closing cap involution, lubricating oil is stored inside the oiling pipe, when exporting by the integrative guiding gutter that constitutes of the spacing interbody in both sides wide structure, spill over through the constant current piece trace before the oil-out flows, fluid current limiting effect has, can effectively improve the lubricating property of rotating part operation, and then improve the performance of unmanned aerial vehicle part of taking photo by plane.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

fig. 1 is a schematic structural view of a suspension type aerial photography device of the present invention;

fig. 2 is the assembly schematic diagram of the lubricating structure of the present invention.

In the figure: the device comprises an electric control box-1, a frame-2, a machine body-3, a machine frame-4, a lubricating structure-5, a closed cover-30, an oil filling pipe-31, a support body-32, a limiting piece-33, a flow guide groove-34, a constant flow piece-35, an oil outlet-36, a mounting piece-37, a rotating shaft-6, a transmission shaft-7, a landing frame-8 and a multi-rotor wing-9.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

Referring to fig. 1-2, the present invention provides a technical solution: a suspension type aerial photography device structurally comprises an electric control box 1, a frame 2, a machine body 3, a machine frame 4, a lubricating structure 5, a rotating shaft 6, a conducting shaft 7, a grounding frame 8 and a plurality of rotors 9, wherein the machine body 3 is provided with the embedded frame 2 located at a groove in the middle of the structure, the electric control box 1 is arranged at the position of the middle of the cross part of the corresponding machine frame 4, the surface groove of the conducting shaft 7 is clamped with the rotating shaft 6, the rotating shaft 6 is correspondingly arranged at the groove on the surface of the plurality of rotors 9, the grounding frames 8 are arranged at the positions of the bottom walls at two sides of the machine frame 4, the surface groove of the conducting shaft 7 is provided with the embedded lubricating structure 5, the lubricating structure 5 comprises a closed cover 30, an oil filling pipe 31, a supporting body 32, a limiting piece 33, a flow guide groove 34, a flow determining piece 35, an oil outlet 36 and an installing piece 37, the closed cover 30 is rotatably arranged on the outer groove, the supporter 32 connects conduction axle 7 through installed part 37 combination wall, spacing piece 33 surface local position is equipped with continuous constant current piece 35, constant current piece 35 combination oil-out 36 looks rigid coupling, guiding gutter 34 comprises the wide structure an organic whole between two limit pieces 33 on both sides, oil-out 36 is linked together conduction axle 7 inner wall, many rotors 9 are installed on the frame 4 structure corresponds outer end recess surface, frame 2 combination automatically controlled box 1 assembles an organic whole mutually, frame 4 corresponds outer end recess position and has been installed conduction axle 7, frame 2 installation is located frame 4 structure recess department between two parties, guiding gutter 34 is linked together with oiling pipe 31 inner lane, constant current piece 35 overflows the accessory for the liquid filling formula.

The constant flow piece 35 is a part for passing oil, lubricating oil is stored in the oil filling pipe 31 and slightly overflows through the constant flow piece 35 before flowing out of the oil outlet 36, and the oil flow limiting function is achieved.

For example: when carrying out the use, unmanned aerial vehicle flies through many rotors 9 of the combination of

conduction axle

7, 7 surperficial recesses of conduction axle are equipped with embedded lubricating structure 5, the combination of supporter 32 of rigid coupling installed part 37 is equipped with oiling pipe 31, the outer end opening passes through the involution of closed cover 30, lubricating oil is stored in oiling pipe 31 inside, when exporting by the integrative guiding gutter 34 of constituting of the wide structure between the spacing piece 33 on both sides, overflow through the constant current piece 35 trace before 36 flows out from the oil-out, fluid current limiting effect has, can effectively improve the lubricating property of rotatable part operation, and then improve the performance of aerial photography unmanned aerial vehicle part.

The utility model provides a problem be that current floated device of taking photo by plane utilizes the rotor flight aloft, and fast-speed turning force increases the part friction, accelerates blade rotation loss easily, and then influences unmanned aerial vehicle's that takes photo by plane suspension performance, the utility model discloses a combination of each other of above-mentioned parts can effectively improve the lubricating property of turning part operation through lubricating structure, and then improves the performance of unmanned aerial vehicle part that takes photo by plane.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. The utility model provides a floated device of taking photo by plane, its structure includes automatically controlled box (1), frame (2), organism (3), frame (4), lubricating structure (5), pivot (6), conduction axle (7), frame (8), many rotors (9), its characterized in that fall to the ground:

be equipped with on organism (3) and be located embedded frame (2) of structure groove between two parties, automatically controlled box (1) sets in the cross middle part position department that corresponds frame (4), transmission axle (7) surface groove looks joint pivot (6), pivot (6) are corresponding to set in many rotors (9) surface groove, frame (4) both sides diapire position has been installed and has been fallen ground frame (8), transmission axle (7) surface groove is equipped with embedded lubricating structure (5).

2. A suspended aerial device according to claim 1, wherein: lubricating structure (5) are including closed lid (30), notes oil pipe (31), supporter (32), spacing piece (33), guiding gutter (34), decide and flow piece (35), oil-out (36), installed part (37), closed lid (30) are established soon on notes oil pipe (31) surface outer groove, notes oil pipe (31) opening looks rigid coupling supporter (32) local recess on, supporter (32) are through installed part (37) combination wall and are connect conduction axle (7), spacing piece (33) surface local position is equipped with continuous and decide and flow piece (35), decide and flow piece (35) combination oil-out (36) looks rigid coupling, guiding gutter (34) constitute by the wide structure an organic whole between spacing piece (33) on both sides, oil-out (36) are linked together conduction axle (7) inner wall.

3. A suspended aerial device according to claim 1, wherein: the multiple rotors (9) are arranged on the surfaces of the grooves at the corresponding outer ends of the structure of the rack (4).

4. A suspended aerial device according to claim 1, wherein: the frame (2) is assembled and connected with the electric control box (1) into a whole.

5. A suspended aerial device according to claim 1, wherein: and the position of the frame (4) corresponding to the groove at the outer end is provided with a conduction shaft (7).

6. A suspended aerial device according to claim 1, wherein: the frame (2) is arranged at a groove in the middle of the structure of the frame (4).