CN213800213U - Four rotors pass through quick-witted frame - Google Patents
Four rotors pass through quick-witted frame Download PDFInfo
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- CN213800213U CN213800213U CN202022289470.8U CN202022289470U CN213800213U CN 213800213 U CN213800213 U CN 213800213U CN 202022289470 U CN202022289470 U CN 202022289470U CN 213800213 U CN213800213 U CN 213800213U
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Abstract
The utility model provides a four-rotor crossing machine frame, which comprises a bottom plate, a top plate, a camera fixing plate, a machine arm and a machine arm clamping plate; the top plate is fixed on the bottom plate through 8 aluminum columns, and the camera fixing plate is embedded at the front ends of the bottom plate and the top plate; the machine arm is fixed between the bottom plate and the machine arm clamping plate; four machine arms are uniformly shaped and symmetrically distributed on two sides of the bottom plate; the included angle formed by the front two machine arms and the included angle formed by the rear two machine arms are both 108 degrees; the wheelbase of the rack is 175 mm; bottom plate, roof, camera fixed plate, horn and horn splint adopt the fine material of 3K carbon, the utility model discloses four rotors pass through whole fuselage of frame small, light in weight, compatible height.
Description
Technical Field
The utility model belongs to the unmanned aerial vehicle field, concretely relates to four rotors pass through quick-witted frame.
Background
With the rise of the unmanned industry, various small traversing machines appear in the visual field of people and are deeply favored, but the problems follow in the using process, the small traversing machines are insufficient in compatibility, and the mounting space and hole positions of one machine frame are limited.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a four rotors pass through quick-witted frame to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a rack suitable for a four-rotor penetrating machine comprises a bottom plate, a top plate, a camera fixing plate, a machine arm and a machine arm clamping plate, wherein the top plate is fixed on the bottom plate through 8 aluminum columns, and the camera fixing plate is embedded at the front ends of the bottom plate and the top plate; the machine arm is fixed between the bottom plate and the machine arm clamping plate; four machine arms are uniformly shaped and symmetrically distributed on two sides of the bottom plate; the contained angle that two front horn formed and the contained angle that two back horns formed are 108, the horn is equipped with the motor mounting hole, the camera fixed plate is equipped with the camera mounting hole, the bottom plate is equipped with flight control installation hole site and picture and passes the installation hole site.
Preferably, the motor mounting hole of the horn is compatible with a motor with the size of 12mm to 16 mm.
Preferably, the camera fixing plate can be provided with a 19mm camera, the angle of the camera can be adjusted, and the position of the camera can be moved within a range of 4mm forwards or backwards.
Preferably, the base plate can be compatible with 20 mm-size flight controls and 25.5 mm-size diamond-type flight controls, and the map transmission mounting holes can be used for mounting map transmissions with 20 mm-size mounting sizes.
Drawings
FIG. 1 is an overall view of a gantry;
FIG. 2 is a side view of the gantry;
FIG. 3 is a top view of the frame;
FIG. 4 is a top view of the base plate;
in the figure: 1-top plate, 2-bottom plate, 3-horn, 4-horn clamping plate, 5-camera fixing plate, 6-aluminum column, 7-camera mounting hole, 8-bayonet, 9-aluminum column screw hole, 10-motor mounting hole, 11-flight control mounting hole, 12-diamond flight control mounting hole and 13-picture transmission mounting hole.
Detailed Description
The invention is further explained with reference to the drawings, without limiting the scope of protection of the invention.
Referring to fig. 1-4, a four-rotor pass-through airframe includes a top plate, a bottom plate, an airframe, a camera fixing plate, and an airframe clamp plate; roof 1 and bottom plate 2 all be equipped with bayonet socket 8, be used for blocking camera fixed plate 5, horn 3 is equipped with motor mounting hole 10, motor mounting hole 10 is used for the motor of fixed mounting 12mm to 16mm size, camera fixed plate 5 is equipped with camera screw hole 7, camera screw hole 7 is used for installing the camera, and the camera can move forward or backward, and angle modulation, bottom plate 2 is equipped with flight control mounting hole 11, rhombus flight control mounting hole 12 and picture and passes mounting hole 13, places horn 3 in the middle of horn splint 4 and bottom plate 2, and camera fixed plate 5 is fixed with bayonet socket 8, and the length of aluminium post 6 is 22mm and is connected roof 1 and bottom plate 2 and become a whole frame.
Has the advantages that: two types of flight control mounting hole sites are arranged on the bottom plate, flight control with the size of 20mm multiplied by 20mm and diamond-shaped flight control with the hole sites of 25.5mm multiplied by 25.5mm can be mounted, flight control of 3 layers of towers can be placed in 2 layers of towers, and 2-3 layers of towers can be placed in the map transmission mounting hole sites with the size of 20mm multiplied by 20mm arranged on the tail part of the tower, so that the requirement of placing more layers of tower-type flight control is met.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented 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, and any reference signs in the claims are not intended to 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 (4)
1. The utility model provides a four rotors pass through quick-witted frame, the frame includes bottom plate, roof, camera fixed plate, horn and horn splint, its characterized in that: the top plate is fixed on the bottom plate through 8 aluminum columns, and the camera fixing plate is embedded at the front ends of the bottom plate and the top plate; the machine arm is fixed between the bottom plate and the machine arm clamping plate; four machine arms are uniformly shaped and symmetrically distributed on two sides of the bottom plate; the contained angle that two front horn formed and the contained angle that two back horns formed are 108, the horn is equipped with the motor mounting hole, the camera fixed plate is equipped with the camera mounting hole, the bottom plate is equipped with flight control installation hole site and picture and passes the installation hole site.
2. A quad-rotor cross-over airframe as recited in claim 1, further comprising: the motor mounting hole of the machine arm is compatible with a motor with the mounting size of 12 mm-16 mm.
3. A quad-rotor cross-over airframe as recited in claim 1, further comprising: the camera fixing plate can be used for installing a camera with the size of 19mm, the angle of the camera can be adjusted, and the position of the camera can move within the range of 4mm forwards or backwards.
4. A quad-rotor cross-over airframe as recited in claim 1, further comprising: the bottom plate is used for installing 20mm flight controls and 25.5mm diamond flight controls, 25.5mm diamond flight controls and 20mm figure transmission devices.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202022289470.8U CN213800213U (en) | 2020-10-09 | 2020-10-09 | Four rotors pass through quick-witted frame |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202022289470.8U CN213800213U (en) | 2020-10-09 | 2020-10-09 | Four rotors pass through quick-witted frame |
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CN213800213U true CN213800213U (en) | 2021-07-27 |
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CN202022289470.8U Active CN213800213U (en) | 2020-10-09 | 2020-10-09 | Four rotors pass through quick-witted frame |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116812184A (en) * | 2023-07-04 | 2023-09-29 | 深圳技术大学 | Six-axis unmanned aerial vehicle for radar mapping |
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2020
- 2020-10-09 CN CN202022289470.8U patent/CN213800213U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116812184A (en) * | 2023-07-04 | 2023-09-29 | 深圳技术大学 | Six-axis unmanned aerial vehicle for radar mapping |
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