CN108974346A - A kind of unmanned plane wing fixed structure - Google Patents
A kind of unmanned plane wing fixed structure Download PDFInfo
- Publication number
- CN108974346A CN108974346A CN201810867964.4A CN201810867964A CN108974346A CN 108974346 A CN108974346 A CN 108974346A CN 201810867964 A CN201810867964 A CN 201810867964A CN 108974346 A CN108974346 A CN 108974346A
- Authority
- CN
- China
- Prior art keywords
- ball
- unmanned plane
- hole
- installation set
- wing
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Abstract
The present invention relates to unmanned plane equipment technical field, in particular to a kind of unmanned plane wing fixed structure, unmanned plane is installed and is provided with support plate on total box；Guide sleeve is fixed in support plate；Circular mounting axis is inserted into installation set after passing through guide sleeve；Wing connecting rod is inserted into guide sleeve；Sliding sleeve one end is inserted on the lateral wall of the inside installation set of installation set and is provided with annular mounting groove；The bottom of spin mounting hole is provided with hemispherical slot；The bottom end of hemispherical slot is provided with circular through hole；The diameter of ball is equal to the diameter of hemispherical slot；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 the surface of ball；Ball one end is inserted into annular groove after passing through circular through hole.In using the present invention, the connection structure without using additional tool, dismount more convenient, and unmanned plane wing dismounting step is simple, and disassembly efficiency is high.
Description
Technical field
The present invention 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.
Summary of the invention
In view of the defects and deficiencies of the prior art, the present invention intends to provide a kind of unmanned planes convenient to disassembly
Wing fixed structure.
To achieve the above object, the technical solution adopted by the present invention is that:
A kind of unmanned plane wing fixed structure of the present invention, it includes that unmanned plane installs total box and wing connecting rod；Institute
It states wing connecting rod one end and is provided with propeller；The propeller other end is provided with circular mounting axis；The unmanned plane installation
Support plate is provided on total box；Guide sleeve is fixed in the support plate；The inner hole of the guide sleeve and the bar of wing connecting rod
Body matches；The unmanned plane is installed and is fixed with installation set on total box；The circular mounting axis is inserted into peace after passing through guide sleeve
In encapsulation；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；It is 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 annular is recessed
The inner bottom wall of slot 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 rollings
Ball mounting hole；The spin mounting hole is circumferentially distributed in installation set；The bottom of the spin mounting hole is provided with hemispherical
Slot；The bottom end of the hemispherical slot is provided with circular through hole；Ball is provided in the hemispherical slot；The ball
Diameter 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 inner sleeve
There is rubber ring；The inner ring surface of the rubber ring is pressed on the surface of ball；Described ball one end is inserted into after passing through circular through hole
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 invention has the following beneficial effects: a kind of unmanned plane wing fixed structure of the present invention, machine
Wing connecting rod one end is provided with propeller；The propeller other end is provided with circular mounting axis；Unmanned plane is installed to be provided on total box
Support plate；Guide sleeve is fixed in support plate；The inner hole of guide sleeve and the shaft of wing connecting rod match；Unmanned plane installation is total
Installation set is fixed on box；Circular mounting axis is inserted into installation set after passing through guide sleeve；Wing connecting rod is inserted into guide sleeve
It is interior；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；Sliding sleeve one end
It 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 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 spin mounting holes；
Spin mounting hole is circumferentially distributed in installation set；The bottom of spin mounting hole is provided with hemispherical slot；Hemispherical slot
Bottom end is provided with circular through hole；Ball is provided in hemispherical slot；The diameter of ball is equal to the diameter of hemispherical slot；It is round
The diameter of 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 the table of ball
On face；Ball one end is inserted into annular groove after passing through circular through hole.In using the present invention, wing connecting rod, which is inserted into, leads
It is only capable of being unable to rotate along the axial direction sliding to guide sleeve after to set；Under the action of rubber ring, use ball
It is pressed on the hole wall of hemispherical slot；Annular groove is inserted by ball；Position circular mounting axis in installation set；It is real
Existing wing connecting rod is installed fixed on total box in unmanned plane；When needing to split out wing connecting rod, sliding sleeve is toward the direction of ball
Push-in, and each ball is pushed to move along the direction of rubber ring, so that ball is pushed away annular groove, until sliding sleeve is inserted into installation
Between set and circular mounting axis, wing connecting rod can be pulled out；The connection structure without using additional tool, dismounting is more
Add conveniently, and unmanned plane wing dismounting step is simple, disassembly efficiency is high, and complete machine is easy to carry.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention；
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 present invention will be further described below with reference to the drawings.
As shown in Figures 1 to 3, a kind of unmanned plane wing fixed structure of the present invention, it includes that unmanned plane installation is 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 circle
Installation axle 6；The unmanned plane is installed and is provided with support plate 101 on total box 1；Guide sleeve 7 is fixed in the support plate 101；Institute
The shaft of the inner hole and wing connecting rod 8 of stating guide sleeve 7 matches；The unmanned plane is installed and is fixed with installation set 2 on total box 1；
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；Machine
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 invention, several bulge loops 501 are provided with the set of the sliding sleeve 5；It is described
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, prevents
It skids when hand pushes sliding sleeve 5.
As a kind of preferred embodiment of the invention, the cross section of the wing connecting rod 8 is square shape.
In using the present invention, wing connecting rod be inserted into be only capable of after guide sleeve along the axial direction sliding to guide sleeve and
It can not rotate；Under the action of rubber ring, uses ball and be pressed on the hole wall of hemispherical slot；It is inserted by ball
To annular groove；Position circular mounting axis in installation set；It is fixed on total box to realize that wing connecting rod is installed in unmanned plane；When
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 is moved along the direction of rubber ring, and ball is made to push away annular groove, until sliding sleeve is inserted into installation set and round peace
It fills between axis, wing connecting rod can be pulled out；The connection structure without using additional tool, dismount it is more convenient, and
And unmanned plane wing dismounting step is simple, disassembly efficiency is high.
The above description is only a preferred embodiment of the present invention, thus it is all according to the configuration described in the scope of the patent application of the present invention,
The equivalent change or modification that feature and principle are done, is included in the scope of the patent application of the present invention.
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 |
|---|---|---|---|
| CN201810867964.4A CN108974346A (en) | 2018-08-02 | 2018-08-02 | A kind of unmanned plane wing fixed structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810867964.4A CN108974346A (en) | 2018-08-02 | 2018-08-02 | A kind of unmanned plane wing fixed structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108974346A true CN108974346A (en) | 2018-12-11 |
Family
ID=64554285
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810867964.4A Withdrawn CN108974346A (en) | 2018-08-02 | 2018-08-02 | A kind of unmanned plane wing fixed structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108974346A (en) |
-
2018
- 2018-08-02 CN CN201810867964.4A patent/CN108974346A/en not_active Withdrawn
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3127809B1 (en) | Release and capture of a fixed-wing aircraft | |
| US10988257B2 (en) | Aircraft-retrieval system | |
| US11608191B2 (en) | Rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight | |
| EP3543111B1 (en) | Self-tightening rotor | |
| US11524797B2 (en) | Aircraft-retrieval system | |
| EP2714512B1 (en) | Rocket or ballistic launched rotary wing unmanned air vehicle | |
| CN205293068U (en) | Undercarriage device that can receive and release automatically | |
| CN102774492A (en) | Small unmanned helicopter fuselage | |
| CN205168905U (en) | Stationary vane aerial survey unmanned aerial vehicle | |
| CN102910288A (en) | Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil | |
| CN104354858B (en) | A kind of agricultural many rotor wing unmanned aerial vehicles | |
| CN105952842A (en) | Damping device for charging base station of power line patrol unmanned aerial vehicle | |
| CN202879795U (en) | Multipurpose unmanned plane with flexible ram-type parawings | |
| CN105083521A (en) | Airship | |
| CN216185992U (en) | Modularized fixed wing unmanned aerial vehicle | |
| EP4098567A1 (en) | External power assist systems for evtol aircraft | |
| CN208715471U (en) | Unmanned aerial vehicle wing fixed knot constructs | |
| TWM524313U (en) | Unmanned aerial vehicle | |
| CN111152919B (en) | Control method of unmanned aerial vehicle capable of taking off and landing vertically | |
| CN108974346A (en) | A kind of unmanned plane wing fixed structure | |
| CN205293058U (en) | Conveniently carry on fixed wing uavs of jumbo size loading device | |
| CN209192224U (en) | A kind of easy-to-dismount propeller of unmanned plane | |
| CN205293069U (en) | Full topography undercarriage device of unmanned vehicles | |
| CN211618110U (en) | Diaxon VTOL unmanned aerial vehicle | |
| CN106965934A (en) | The landing modes and device of a kind of aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181211 |
|
| WW01 | Invention patent application withdrawn after publication |