CN208559775U - One kind is verted vector type unmanned plane motor fixing seat - Google Patents
One kind is verted vector type unmanned plane motor fixing seat Download PDFInfo
- Publication number
- CN208559775U CN208559775U CN201821154768.4U CN201821154768U CN208559775U CN 208559775 U CN208559775 U CN 208559775U CN 201821154768 U CN201821154768 U CN 201821154768U CN 208559775 U CN208559775 U CN 208559775U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- servo
- controller
- fixing seat
- steering engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
It verts vector type unmanned plane motor fixing seat the utility model discloses one kind, it including driving motor, Servo-controller and is fixed in Servo-controller its steering engine and turns shaft support, the driving motor is located above Servo-controller and is pivotally connected by the steering engine shaft of bracket (3) and Servo-controller;Servo-controller bottom is connected with mount holder, mount holder is fixed on unmanned plane horn by a clamping device, driving motor makees fore-and-aft tilt, rotation along steering engine shaft by Servo-controller, and screw blade is driven to rotate, form the lift for not having to angle, it constitutes vector and adjusts power, can avoid common multiaxis unmanned plane by this changes unmanned plane during flying direction and turned to, translated etc. by more motor differential modes and act.
Description
Technical field
The utility model belongs to air vehicle technique field, and it is solid to concretely relate to one kind vector type unmanned plane motor that verts
Reservation.
Background technique
Multi-rotor unmanned aerial vehicle is easy to operate because structure is simple, and application surface is also increasingly wider in life, traditional more rotors
Unmanned plane motor is directly connected with fixed bracket, and the movements such as steering, pitching, roll carry out real by the revolving speed of each motor
Existing, this just just has certain limitation to the mobility of unmanned plane.
Summary of the invention
It verts vector type unmanned plane motor fixing seat the purpose of the utility model is to provide one kind, is intended to overcome background skill
The problem of art.
In order to solve the above technical problems, purpose of the utility model is realized as follows:
One kind is verted vector type unmanned plane motor fixing seat, including driving motor, Servo-controller and is fixed in servorudder
Its steering engine of machine turns shaft support, and the driving motor is located at the steering engine shaft for above Servo-controller and passing through bracket and Servo-controller
Pivot joint;
Servo-controller bottom is connected with mount holder, and mount holder is fixed on unmanned plane horn by a clamping device, drives
Dynamic motor makees fore-and-aft tilt, rotation along steering engine shaft by Servo-controller, and screw blade is driven to rotate, and forms one and does not have to
The lift of angle constitutes vector and adjusts power.
Preferred embodiment on the basis of above scheme and as above scheme: the clamping device is by obvolvent on horn
Upper pipe clamp, lower tube clip composition, the clamping device structure is simple, and assembly is quick.
Preferred embodiment on the basis of above scheme and as above scheme: mount holder and the clamping company of the upper tube,
Mount holder is fixed on horn.
Preferred embodiment on the basis of above scheme and as above scheme: the bracket is U-bracket, the U-shaped
Two free end of bracket and the both ends of steering engine shaft are connected, and it is more solid and reliable that U-bracket is attached rear structure.
Preferred embodiment on the basis of above scheme and as above scheme: the horn uses carbon fiber pipe, carbon fiber
Dimension pipe is light, intensity is big, reduces fuselage weight while providing fuselage sufficient intensity.
Preferred embodiment on the basis of above scheme and as above scheme: offering location hole on the horn, on
The obvolvent face of pipe clamp and horn is provided with a positioning convex platform, and the positioning convex platform is corresponding with location hole.
Compared with the prior art, the utility model has prominent and beneficial technical effects that: 1, the rotation of certain angle can be passed through
The torque of structure at an angle offsets the influence of external environment (wind) to unmanned plane;2, can be flown by this change unmanned plane
Line direction avoids common multiaxis unmanned plane by more motor differential modes and the movement such as is turned to, translated;3, it can use this
Vector type unmanned plane motor fixing seat of verting constitutes VTOL fixed-wing unmanned plane, convenient so that fixed-wing unmanned plane is put
De- launching cradle and recorery parachute.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model;
Fig. 2 is upper pipe clamp structure schematic diagram;
Fig. 3 is horn structural schematic diagram.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application clearer, below in conjunction with the attached drawing 1-3 in embodiment,
Technical solution in embodiment is clearly and completely described,
One kind is verted vector type unmanned plane motor fixing seat, including driving motor 2, Servo-controller 9 and is fixed in servo
The both ends of the U-bracket 3 of its steering engine shaft 4 of steering engine 9,3 liang of free ends of U-bracket and steering engine shaft 4 are connected, and driving motor 2
It is pivotally connected above Servo-controller 9 and through the steering engine shaft 4 of U-bracket 3 and Servo-controller 9;
9 bottom of Servo-controller is connected with mount holder 8, and mount holder 8 is fixed on unmanned plane horn 7 by a clamping device
On.
In the present embodiment, clamping device is made of upper pipe clamp 5, lower tube clip 6 of the obvolvent on horn 7, mount holder 8 with it is upper
Pipe clamp 5 is connected the bracket 3 as U-bracket.
Preferably, the horn 7 uses carbon fiber pipe.
Preferably, location hole 71 is offered on horn 7, upper pipe clamp 5 is corresponding with location hole 71 with the obvolvent face of horn 7
Be provided with a positioning convex platform 51, positioning convex platform 51, which is embedded into location hole 71, carries out anti-rotation positioning for upper pipe clamp 5;
Similarly, lower tube clip 6 is identical as upper 5 structure of pipe clamp, it may have positioning convex platform;
The purpose being arranged in this way is to prevent from leading to its rotation due to upper and lower pipe clamp insufficient clamping force, influences normal flight.
Specific working principle:
By remote control or long-range control, steering engine shaft 4 is driven by the electric control system controls Servo-controller 9 on unmanned plane
Rotation, steering engine shaft 4 will synchronous drive U-bracket 3 rotate, to make driving motor 2 with 4 center of circle of steering engine shaft with U-shaped
Bracket 3 is radius rotation, realizes fore-and-aft tilt, rotation, rotates in driving motor 2 and screw blade 1 is driven to rotate, just formed not
With the lift of angle, constitutes vector and adjust power.
Above-described embodiment is only the preferred embodiment of the utility model, not limits the protection model of the utility model according to this
It encloses, therefore: the equivalence changes that all structures, shape, principle according to the utility model are done should all be covered by the protection of the utility model
Within the scope of.
Claims (6)
- The vector type unmanned plane motor fixing seat 1. one kind is verted, including driving motor (2), Servo-controller (9) and being fixed in are watched The bracket (3) of its steering engine shaft (4) of steering engine (9) is taken, the driving motor (2) is located above Servo-controller (9) and passes through bracket (3) it is pivotally connected with the steering engine shaft (4) of Servo-controller (9);Servo-controller (9) bottom is connected with mount holder (8), and mount holder (8) is fixed on unmanned plane horn by a clamping device (7) on.
- The vector type unmanned plane motor fixing seat 2. one kind according to claim 1 is verted, it is characterised in that: the clamping machine Structure is made of upper pipe clamp (5), lower tube clip (6) of the obvolvent on horn (7).
- The vector type unmanned plane motor fixing seat 3. one kind according to claim 2 is verted, it is characterised in that: mount holder (8) it is connected with the upper pipe clamp (5).
- The vector type unmanned plane motor fixing seat 4. one kind according to claim 1 is verted, it is characterised in that: the bracket It (3) is U-bracket, the both ends of two free end of U-bracket and steering engine shaft (4) are connected.
- The vector type unmanned plane motor fixing seat 5. one kind according to claim 1 is verted, it is characterised in that: the horn (7) carbon fiber pipe is used.
- The vector type unmanned plane motor fixing seat 6. one kind according to claim 1 is verted, it is characterised in that: the horn (7) it is offered on location hole (71), the obvolvent face of upper pipe clamp (5) and horn (7) is provided with a positioning convex platform (51), the positioning Boss (51) is corresponding with location hole (71).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821154768.4U CN208559775U (en) | 2018-07-20 | 2018-07-20 | One kind is verted vector type unmanned plane motor fixing seat |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821154768.4U CN208559775U (en) | 2018-07-20 | 2018-07-20 | One kind is verted vector type unmanned plane motor fixing seat |
Publications (1)
Publication Number | Publication Date |
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CN208559775U true CN208559775U (en) | 2019-03-01 |
Family
ID=65446848
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201821154768.4U Expired - Fee Related CN208559775U (en) | 2018-07-20 | 2018-07-20 | One kind is verted vector type unmanned plane motor fixing seat |
Country Status (1)
Country | Link |
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CN (1) | CN208559775U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112357047A (en) * | 2020-11-19 | 2021-02-12 | 南京信息工程大学 | Unmanned aerial vehicle with telescopic arm variable rotor wing |
-
2018
- 2018-07-20 CN CN201821154768.4U patent/CN208559775U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112357047A (en) * | 2020-11-19 | 2021-02-12 | 南京信息工程大学 | Unmanned aerial vehicle with telescopic arm variable rotor wing |
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190301 Termination date: 20200720 |
|
CF01 | Termination of patent right due to non-payment of annual fee |