CN208715471U - Unmanned aerial vehicle wing fixed knot constructs - Google Patents
Unmanned aerial vehicle wing fixed knot constructs Download PDFInfo
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- CN208715471U CN208715471U CN201821234236.1U CN201821234236U CN208715471U CN 208715471 U CN208715471 U CN 208715471U CN 201821234236 U CN201821234236 U CN 201821234236U CN 208715471 U CN208715471 U CN 208715471U
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- 238000005096 rolling process Methods 0.000 claims abstract description 4
- 238000009434 installation Methods 0.000 claims description 31
- 239000007787 solid Substances 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000036544 posture Effects 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle wing fixing structure.A supporting plate is arranged on an unmanned aerial vehicle mounting general box; a guide sleeve is fixed on the support plate; the circular mounting shaft penetrates through the guide sleeve and then is inserted into the mounting sleeve; the wing connecting rod is inserted into the guide sleeve; one end of the sliding sleeve is inserted into the outer side wall of the inner mounting sleeve of the mounting sleeve and is provided with an annular mounting groove; the bottom of the rolling ball mounting hole is provided with a hemispherical groove hole; the bottom end of the hemispherical groove hole is provided with a circular through hole; the diameter of the ball is equal to that of the hemispherical slotted hole; the diameter of the circular through hole is smaller than that of the ball; a rubber ring is sleeved in the annular mounting groove; the inner ring surface of the rubber ring is pressed on the surface of the ball; one end of the ball passes through the circular through hole and then is inserted into the annular groove. Use the utility model discloses the time, this connection structure need not to use extra instrument, and the dismouting is more convenient, and unmanned aerial vehicle wing dismouting step is simple moreover, and the dismouting is efficient.
Description
Technical field
The utility model relates to unmanned plane equipment technical field, in particular to a kind of unmanned plane wing fixed structure.
Background technique
Unmanned plane is the not manned vehicle using radio robot and the presetting apparatus provided for oneself manipulation.Nobody
Machine is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition: unmanned helicopter, unmanned fixed-wing
This several major class of machine, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol.Compared with manned aircraft, it have it is small in size,
Low cost, it is easy to use, low, survival ability is stronger to environmental requirement the advantages that.Unmanned plane of taking photo by plane is to be integrated with high definition to take the photograph
As the remotely-piloted vehicle of device, system specifically includes that carrier aircraft, flies control, gyro holder, transmission of video, earth station and call system
System etc., drone flying height of taking photo by plane are suitble to video display propaganda film and the shooting of birds-eye view etc. generally at 500 meters or more.It is this
Aircraft is flexible and convenient, can quickly finish the shooting of camera lens.
Multi-rotor unmanned aerial vehicle can VTOL, it is using multiple rotors as power device, and multi-rotor unmanned aerial vehicle is using empty
Aerodynamic force overcomes own wt, can autonomous or remote control distributor, can disposably or repeatedly recycle use, various load can be carried.
Multi-rotor unmanned aerial vehicle topology layout is novel, flying method is unique, has autonomous take-off and landing ability, adapts to complicated ring
Border, to take off land place requirement it is low, height is intelligent.Multi-rotor unmanned aerial vehicle can be flown with various postures, such as hover, is preceding
Fly, side flies and inverted flight etc..It is generally believed that propeller quantity is more, fly more steady, it is easier to operate, traditional unmanned plane
Wing is all to be fixed with carbon fiber board to do complete machine, dismantles assembly difficulty, and intensity is low, and detachable unmanned plane wing is in dismounting
It needs using tools such as screwdrivers, in field work, extracting tool need to be carried, easily tool is caused to lose, and is inconvenient to carry.
Utility model content
The purpose of this utility model is that it is in view of the drawbacks of the prior art and insufficient, a kind of nothing convenient to disassembly is provided
Man-machine wing fixed structure.
In order to achieve the above purposes, the technical solution adopted by the utility model is:
A kind of unmanned plane wing fixed structure described in the utility model, it includes that unmanned plane installs total box and wing company
Extension bar；Wing connecting rod one end is provided with propeller；The propeller other end is provided with circular mounting axis；It is described nobody
Machine is installed and is provided with support plate on total box；Guide sleeve is fixed in the support plate；The inner hole of the guide sleeve is connect with wing
The shaft of bar matches；The unmanned plane is installed and is fixed with installation set on total box；The circular mounting axis is inserted after passing through guide sleeve
Enter into installation set；The wing connecting rod is inserted into guide sleeve；
The outside of the circular mounting axis is cased with sliding sleeve；The set body of the sliding sleeve and the inner hole of installation set match；
Described sliding sleeve one end is inserted into the inside of installation set；Annular groove is provided on the axle body of the circular mounting axis；The ring
The inner bottom wall of connected in star is arc-shaped shape；
Annular mounting groove is provided on the lateral wall of the installation set；The inner bottom wall of the annular mounting groove is evenly equipped with several
A spin mounting hole；The spin mounting hole is circumferentially distributed in installation set；The bottom of the spin mounting hole is provided with half
Spherical slot；The bottom end of the hemispherical slot is provided with circular through hole；Ball is provided in the hemispherical slot；The rolling
The diameter of pearl is equal to the diameter of hemispherical slot；The diameter of the circular through hole is less than the diameter of ball；The annular mounting groove
Inside it is cased with rubber ring；The inner ring surface of the rubber ring is pressed on the surface of ball；After described ball one end passes through circular through hole
It is inserted into annular groove.
Further, several bulge loops are provided with the set of the sliding sleeve；The bulge loop is along the axial direction side of sliding sleeve
To being arranged successively.
Further, the cross section of the wing connecting rod is square shape.
After adopting the above structure, the utility model has the beneficial effect that a kind of unmanned plane wing described in the utility model is solid
Determine structure, wing connecting rod one end is provided with propeller；The propeller other end is provided with circular mounting axis；Unmanned plane installs total box
On be provided with support plate；Guide sleeve is fixed in support plate；The inner hole of guide sleeve and the shaft of wing connecting rod match；Nobody
Machine is installed and is fixed with installation set on total box；Circular mounting axis is inserted into installation set after passing through guide sleeve；The insertion of wing connecting rod
Into guide sleeve；The outside of circular mounting axis is cased with sliding sleeve；The set body of the sliding sleeve and the inner hole of installation set match；It is sliding
Dynamic set one end is inserted into the inside of installation set；Annular groove is provided on the axle body of circular mounting axis；The inner bottom wall of annular groove
It is arc-shaped shape；Annular mounting groove is provided on the lateral wall of installation set；The inner bottom wall of annular mounting groove is evenly equipped with several rollings
Ball mounting hole；Spin mounting hole is circumferentially distributed in installation set；The bottom of spin mounting hole is provided with hemispherical slot；Hemisphere
The bottom end of shape slot is provided with circular through hole；Ball is provided in hemispherical slot；The diameter of ball is equal to hemispherical slot
Diameter；The diameter of circular through hole is less than the diameter of ball；Rubber ring is cased in annular mounting groove；The inner ring surface of rubber ring is pressed on
On the surface of ball；Ball one end is inserted into annular groove after passing through circular through hole.When the utility model is used, wing connects
Extension bar is only capable of being unable to rotate along the axial direction sliding to guide sleeve after being inserted into guide sleeve；Due to the effect of rubber ring
Under, it uses ball and is pressed on the hole wall of hemispherical slot；Annular groove is inserted by ball；Pacifying circular mounting axis
It is positioned on encapsulation；It is fixed on total box to realize that wing connecting rod is installed in unmanned plane；When needing to split out wing connecting rod, sliding sleeve
It is pushed into toward the direction of ball, and each ball is pushed to move along the direction of rubber ring, ball is made to push away annular groove, until sliding
Set is inserted between installation set and circular mounting axis, and wing connecting rod can be pulled out；The connection structure without using additional
Tool, dismount more convenient, and unmanned plane wing dismounting step is simple, and disassembly efficiency is high, and complete machine is easy to carry.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of wing；
Fig. 3 is the structural schematic diagram of installation set；
Description of symbols:
1, unmanned plane installs total box；101, support plate；2, installation set；201, annular mounting ring；
202, spin mounting hole；203, hemispherical slot；204, circular through hole；3, ball；
4, rubber ring；5, sliding sleeve；501, bulge loop；6, circular mounting axis；601, annular groove；
7, guide sleeve；8, wing connecting rod；9, propeller.
Specific embodiment
The utility model will be further described below with reference to the accompanying drawings.
As shown in Figures 1 to 3, a kind of unmanned plane wing fixed structure described in the utility model, it includes unmanned plane peace
Fill total box 1 and wing connecting rod 8；Described 8 one end of wing connecting rod is provided with propeller 9；9 other end of propeller is provided with
Circular mounting axis 6；The unmanned plane is installed and is provided with support plate 101 on total box 1；Guide sleeve is fixed in the support plate 101
7；The inner hole of the guide sleeve 7 and the shaft of wing connecting rod 8 match；The unmanned plane is installed and is fixed with installation on total box 1
Set 2；The circular mounting axis 6 is inserted into installation set 2 after passing through guide sleeve 7；The wing connecting rod 8 is inserted into guide sleeve 7
It is interior；Wing connecting rod 8 is only capable of being unable to rotate along the axial direction sliding to guide sleeve 7 after being inserted into guide sleeve 7.
The outside of the circular mounting axis 6 is cased with sliding sleeve 5；The inner hole phase of the set body and installation set 2 of the sliding sleeve 5
Match；Described 5 one end of sliding sleeve is inserted into the inside of installation set 2；Annular groove is provided on the axle body of the circular mounting axis 6
601；The inner bottom wall of the annular groove 601 is arc-shaped shape.
Annular mounting groove 201 is provided on the lateral wall of the installation set 2；The inner bottom wall of the annular mounting groove 201 is equal
It is furnished with several spin mounting holes 202；The spin mounting hole 202 is circumferentially distributed in installation set 2；The spin mounting hole
202 bottom is provided with hemispherical slot 203；The bottom end of the hemispherical slot 203 is provided with circular through hole 204；Described half
Ball 3 is provided in spherical slot 203；The diameter of the ball 3 is equal to the diameter of hemispherical slot 203；The circular through hole
204 diameter is less than the diameter of ball 3；Rubber ring 4 is cased in the annular mounting groove 201；The inner ring face pressure of the rubber ring 4
Tightly on the surface of ball 3；Described 3 one end of ball is inserted into annular groove 601 after passing through circular through hole 204；Due to rubber
Under the action of ring 4, uses ball 3 and be pressed on the hole wall of hemispherical slot 203；Annular groove is inserted by ball 3
601；Position circular mounting axis 6 in installation set 2；It is fixed on total box 1 to realize that wing connecting rod 8 is installed in unmanned plane；When need
When splitting out wing connecting rod 8, sliding sleeve 5 is pushed into toward the direction of ball 3, and each ball 3 is pushed to transport along the direction of rubber ring 4
It is dynamic, so that ball 3 is pushed away annular groove 601, until sliding sleeve 5 is inserted between installation set 2 and circular mounting axis 6, wing is connected
Bar 8 can be pulled out；The connection structure without using additional tool, dismount more convenient, and unmanned plane wing dismounts
Step is simple, and disassembly efficiency is high.
As a kind of preferred embodiment of the utility model, several bulge loops 501 are provided with the set of the sliding sleeve 5；
The bulge loop 501 is arranged successively along the axial direction of sliding sleeve 5；The effect of bulge loop 501 makes the sliding feel for increasing sliding sleeve 5,
Prevent the skidding when hand pushes sliding sleeve 5.
As a kind of preferred embodiment of the utility model, the cross section of the wing connecting rod 8 is square shape.
When the utility model is used, wing connecting rod is only capable of sliding along the axial direction to guide sleeve after being inserted into guide sleeve
It is dynamic to be unable to rotate；Under the action of rubber ring, uses ball and be pressed on the hole wall of hemispherical slot；Pass through ball
It is inserted into annular groove；Position circular mounting axis in installation set；It is solid on total box to realize that wing connecting rod is installed in unmanned plane
It is fixed；When needing to split out wing connecting rod, finger is acted on the bulge loop of sliding sleeve, is pushed into sliding sleeve toward the direction of ball,
And push each ball to move along the direction of rubber ring, so that ball is pushed away annular groove, until sliding sleeve be inserted into installation set with
Between circular mounting axis, wing connecting rod can be pulled out；The connection structure without using additional tool, dismount more square
Just, and unmanned plane wing dismounting step is simple, and disassembly efficiency is high.
The above description is only a preferred embodiment of the present invention, therefore all according to described in the utility model patent application range
The equivalent change or modification done of structure, feature and principle, be included in the scope of the utility model patent application.
Claims (3)
1. a kind of unmanned plane wing fixed structure, it is characterised in that: it includes that unmanned plane installs total box (1) and wing connecting rod
(8)；Described wing connecting rod (8) one end is provided with propeller (9)；Propeller (9) other end is provided with circular mounting axis
(6)；The unmanned plane is installed and is provided with support plate (101) on total box (1)；Guide sleeve is fixed on the support plate (101)
(7)；The inner hole of the guide sleeve (7) and the shaft of wing connecting rod (8) match；The unmanned plane is installed solid on total box (1)
Surely there are installation set (2)；The circular mounting axis (6) is inserted into installation set (2) after passing through guide sleeve (7)；The wing connection
Bar (8) is inserted into guide sleeve (7)；
The outside of the circular mounting axis (6) is cased with sliding sleeve (5)；The set body of the sliding sleeve (5) and the inner hole of installation set (2)
Match；Described sliding sleeve (5) one end is inserted into the inside of installation set (2)；It is provided on the axle body of the circular mounting axis (6)
Annular groove (601)；The inner bottom wall of the annular groove (601) is arc-shaped shape；
Annular mounting groove (201) are provided on the lateral wall of the installation set (2)；The inner bottom wall of the annular mounting groove (201)
It is evenly equipped with several spin mounting holes (202)；The spin mounting hole (202) is circumferentially distributed on installation set (2)；The rolling
The bottom of ball mounting hole (202) is provided with hemispherical slot (203)；The bottom end of the hemispherical slot (203) is provided with circle
Through-hole (204)；Ball (3) are provided in the hemispherical slot (203)；The diameter of the ball (3) is equal to hemispherical slot
(203) diameter；The diameter of the circular through hole (204) is less than the diameter of ball (3)；Annular mounting groove (201) inner sleeve
There are rubber ring (4)；The inner ring surface of the rubber ring (4) is pressed on the surface of ball (3)；Described ball (3) one end passes through circle
It is inserted into after shape through-hole (204) in annular groove (601).
2. a kind of unmanned plane wing fixed structure according to claim 1, it is characterised in that: the set of the sliding sleeve (5)
It is provided with several bulge loops (501) with it；The bulge loop (501) is arranged successively along the axial direction of sliding sleeve (5).
3. a kind of unmanned plane wing fixed structure according to claim 1, it is characterised in that: the wing connecting rod (8)
Cross section be square shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821234236.1U CN208715471U (en) | 2018-08-02 | 2018-08-02 | Unmanned aerial vehicle wing fixed knot constructs |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821234236.1U CN208715471U (en) | 2018-08-02 | 2018-08-02 | Unmanned aerial vehicle wing fixed knot constructs |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208715471U true CN208715471U (en) | 2019-04-09 |
Family
ID=65975864
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821234236.1U Expired - Fee Related CN208715471U (en) | 2018-08-02 | 2018-08-02 | Unmanned aerial vehicle wing fixed knot constructs |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208715471U (en) |
-
2018
- 2018-08-02 CN CN201821234236.1U patent/CN208715471U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190409 Termination date: 20210802 |