CN206068152U - The hanger and unmanned plane of VUAV - Google Patents
The hanger and unmanned plane of VUAV Download PDFInfo
- Publication number
- CN206068152U CN206068152U CN201621101698.7U CN201621101698U CN206068152U CN 206068152 U CN206068152 U CN 206068152U CN 201621101698 U CN201621101698 U CN 201621101698U CN 206068152 U CN206068152 U CN 206068152U
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- Prior art keywords
- hanger
- unmanned plane
- plane
- vuav
- motor
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Abstract
This application discloses the hanger and unmanned plane of a kind of VUAV, a kind of hanger of VUAV of the hanger, including body, also include connector, for triangular prism shaped, the section of the body is rounded triangle to the body, and the connector is arranged on an incline of the body.This utility model also provides a kind of unmanned plane, including above-mentioned hanger, and motor is installed at the body two ends, the mounting plane of the motor horizontal by 2 ° of 6 ° of angles so that propeller Plane of rotation is horizontal by 2 ° of 6 ° of angles.Hanger monnolithic case of the present utility model is the triangular prism shaped design with fillet, reduces hanger resistance in flight course.Hanger of the present utility model passes through the mounting plane for arranging the motor horizontal by certain angle, so that propeller Plane of rotation is at an angle, so unmanned plane is at a static-stability state, strengthens the stability of unmanned plane so that unmanned plane possesses stronger wind resistance.
Description
Technical field
The disclosure relates generally to unmanned plane field, and in particular to a kind of hanger and unmanned plane of VUAV.
Background technology
VUAV motor hanger design at present is generally arranged on horizontal motor cabinet using cylindrical electrical machine
And connect and be installed on fuselage by pipe beam.The Plane of rotation and plane-parallel of propeller, this mode are running into side
When wind or other external disturbances, body underdamping easily causes certain and manipulates direction generation concussion, so not only expends the energy
Shorten cruising time or even flight safety can be affected in some cases.In addition resistance of the hanger of this form in flight course
Power is larger, affects flight efficiency.
Utility model content
In view of drawbacks described above of the prior art or deficiency, expect to provide a kind of reduce resistance in flight course vertical
The hanger and unmanned plane of drop unmanned plane.
In a first aspect, a kind of hanger of VUAV, including body, also including connector, the body is three
Prismatic, the section of the body is rounded triangle, and the connector is arranged on an incline of the body.
The section of the body is fillet equilateral triangle.
The arc length of the fillet is 20-30mm.
The arc length of the fillet is 25mm.
Described is provided with the space for accommodating motor in vivo, a diameter of motor diameter of the inscribed circle of the rounded triangle
1-1.8 again.
1.4 times of a diameter of motor diameter of the inscribed circle of the rounded triangle.
Second aspect, a kind of unmanned plane, including above-mentioned hanger, the body two ends install motor, the peace of the motor
Plane is filled horizontal by 2 ° of -6 ° of angles, so that propeller Plane of rotation is horizontal by 2 ° of -6 ° of angles.
The symmetrical plane of the hanger and the angle of perpendicular are 2 ° -6 °.
The symmetrical plane of the hanger and the angle of perpendicular are 4 °, and/or the mounting plane and level of the motor
Face is in 4 ° of angles.
The hanger beam is fixedly connected connecting rod one end, and the connecting rod other end is connected with wing after stretching out the connector
Connect.
The connecting rod other end is provided with screw hole, and the screw hole is equipped with the screw being connected with wing.
This utility model has the advantages that：
1st, hanger monnolithic case of the present utility model is the triangular prism shaped design with fillet, reduces hanger in flight course
Resistance.
2nd, hanger of the present utility model passes through the mounting plane for arranging the motor horizontal by certain angle so that spiral
At an angle, such unmanned plane is at a static-stability state to oar Plane of rotation, strengthens the stability of unmanned plane so that nothing
It is man-machine to possess stronger wind resistance.
Description of the drawings
By reading the detailed description made to non-limiting example made with reference to the following drawings, the application other
Feature, objects and advantages will become more apparent upon：
The dimensional structure diagram of the hanger of the VUAV that Fig. 1 is provided for this utility model embodiment；
The top view of the hanger of the VUAV that Fig. 2 is provided for this utility model embodiment；
Fig. 3 is the Section A-A schematic diagram in Fig. 2；
Fig. 4 is the section B-B schematic diagram in Fig. 2；
The hanging rack structure schematic diagram for being provided with propeller that Fig. 5 is provided for this utility model embodiment；
Front views of the Fig. 6 for Fig. 5；
Side views of the Fig. 7 for Fig. 6；
The principle explanation schematic diagram of the stability that Fig. 8 is provided for this utility model embodiment.
In figure：
1 body, 2 connectors, 3 fillet equilateral triangles, 4 fillets, 5 motors, the mounting plane of 6 motors, 7 horizontal planes, 8 spiral shells
Rotation oar, the symmetrical plane of 9 hangers, 10 perpendiculars, 11 hanger beams, 12 connecting rods.
Specific embodiment
With reference to the accompanying drawings and examples the application is described in further detail.It is understood that this place is retouched
The specific embodiment stated is used only for explaining relevant utility model, rather than the restriction to the utility model.Further need exist for explanation
, for the ease of description, in accompanying drawing, illustrate only the part related to utility model.
It should be noted that in the case where not conflicting, the feature in embodiment and embodiment in the application can phase
Mutually combine.Below with reference to the accompanying drawings and in conjunction with the embodiments describing the application in detail.
Fig. 1, Fig. 2, Fig. 3 and Fig. 4, a kind of hanger of VUAV, including body 1 are refer to, also including connection
Part 2, for triangular prism shaped, the section of body 1 is rounded triangle to body 1, and connector 2 is arranged on an incline of body 1.This reality
Apply in example, the section of body 1 is fillet equilateral triangle 3.
The monnolithic case of this utility model hanger is the triangular prism shaped design with fillet, reduces hanger resistance in flight course
Power size.
Referring to Fig. 3 and Fig. 4, on the basis of above-described embodiment, the arc length of fillet 4 is 20-30mm to the present embodiment.
Preferably, the arc length of fillet 4 is 25mm.
Referring to Fig. 1, further, the space for accommodating motor in body 1, is provided with, the inscribed circle of fillet equilateral triangle 3
1-1.8 times of a diameter of motor diameter.
Preferably, 1.4 times of a diameter of motor diameter of the inscribed circle of fillet equilateral triangle 3.
Referring to Fig. 5 and Fig. 6, this utility model also provides a kind of unmanned plane, including above-mentioned hanger, and 1 two ends of body are installed
Motor 5, the mounting plane 6 of motor are in 2 ° -6 ° with the angle a of horizontal plane 7 so that 8 Plane of rotation of propeller horizontal by 2 ° -
6 ° of angles.
Preferably, the mounting plane 6 of motor and horizontal plane 7 are in 4 ° of angles.
Referring to Fig. 7, it is preferred that the symmetrical plane 9 of hanger and the angle of perpendicular 10 are 2-6 °, preferably 4 °.
Referring to Fig. 5 and Fig. 6, the present embodiment on the basis of above-described embodiment, for convenience of the connection of hanger and wing, body
Be provided with hanger beam 11 in 1, hanger beam 11 is fixedly connected 12 one end of connecting rod, 12 other end of connecting rod stretch out after connector 2 with machine
The wing connects.
Preferably, for convenience of connecting, 12 other end of connecting rod is provided with screw hole, and the screw hole is equipped with and is connected with wing
Screw.I.e. wing is connected with connecting rod by screw.
Using hanger of the present utility model and the mounting means of horizontal plane, it is possible to increase unmanned plane static stability, unmanned plane
Wind resistance strengthens.
Referring to Fig. 8, show possess certain inwardly tilt angle, the aircraft energy when outside interference is run into by experimentation
The attitude for enough producing extra additional moment to make its reply original.In figure, T represents the pulling force of propeller.This utility model itself
Possesses horizontal and vertical inclination angle therefore, it is possible to tackle the external disturbance from all directions.
Above description is only the preferred embodiment and the explanation to institute's application technology principle of the application.People in the art
Member is it should be appreciated that utility model scope involved in the application, however it is not limited to the particular combination of above-mentioned technical characteristic
Technical scheme, while should also cover in the case where conceiving without departing from the utility model, by above-mentioned technical characteristic or its equivalent
Other technical schemes that feature carries out combination in any and formed.Such as features described above is had with (but not limited to) disclosed herein
The technical scheme that the technical characteristic for having similar functions is replaced mutually and formed.
Claims (10)
1. a kind of hanger of VUAV, including body, it is characterised in that also including connector, the body are three
Prismatic, the section of the body is rounded triangle, and the connector is arranged on an incline of the body.
2. the hanger of VUAV according to claim 1, it is characterised in that the section of the body is fillet
Equilateral triangle.
3. the hanger of VUAV according to claim 1, it is characterised in that the arc length of the fillet is 20-
30mm。
4. the hanger of VUAV according to claim 3, it is characterised in that the arc length of the fillet is
25mm。
5. the hanger of the VUAV according to any one of claim 1-4, it is characterised in that described sets in vivo
Have accommodate motor space, 1-1.8 times of a diameter of motor diameter of the inscribed circle of the rounded triangle.
6. the hanger of VUAV according to claim 5, it is characterised in that the inscribe of the rounded triangle
1.4 times for motor diameter of diameter of a circle.
7. a kind of unmanned plane, it is characterised in that including the hanger described in any one of claim 1-6, the body two ends are installed
Motor, the mounting plane of the motor horizontal by 2 ° of -6 ° of angles so that propeller Plane of rotation is horizontal by 2 ° -6 °
Angle.
8. unmanned plane according to claim 7, it is characterised in that the symmetrical plane of the hanger and the angle of perpendicular
For 2 ° -6 °.
9. unmanned plane according to claim 8, it is characterised in that also including hanger beam and connecting rod, described sets in vivo
Have a hanger beam, the hanger beam is fixedly connected connecting rod one end, the connecting rod other end stretch out after the connector with
Wing connects.
10. unmanned plane according to claim 9, it is characterised in that the connecting rod other end is provided with screw hole, the spiral shell
Silk hole is equipped with the screw being connected with wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621101698.7U CN206068152U (en) | 2016-09-30 | 2016-09-30 | The hanger and unmanned plane of VUAV |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621101698.7U CN206068152U (en) | 2016-09-30 | 2016-09-30 | The hanger and unmanned plane of VUAV |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206068152U true CN206068152U (en) | 2017-04-05 |
Family
ID=58440100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621101698.7U Active CN206068152U (en) | 2016-09-30 | 2016-09-30 | The hanger and unmanned plane of VUAV |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206068152U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275419A (en) * | 2016-09-30 | 2017-01-04 | 顺丰科技有限公司 | The hanger of VUAV and unmanned plane |
-
2016
- 2016-09-30 CN CN201621101698.7U patent/CN206068152U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275419A (en) * | 2016-09-30 | 2017-01-04 | 顺丰科技有限公司 | The hanger of VUAV and unmanned plane |
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210723 Address after: 518063 5th floor, block B, building 1, software industry base, Yuehai street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Fengyi Technology (Shenzhen) Co.,Ltd. Address before: 518061 Intersection of Xuefu Road (south) and Baishi Road (east) in Nanshan District, Shenzhen City, Guangdong Province, 6-13 floors, Block B, Shenzhen Software Industry Base Patentee before: SF TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right |