CN108482637A - A kind of unmanned plane is electronic to receive cantilever design - Google Patents
A kind of unmanned plane is electronic to receive cantilever design Download PDFInfo
- Publication number
- CN108482637A CN108482637A CN201810195296.5A CN201810195296A CN108482637A CN 108482637 A CN108482637 A CN 108482637A CN 201810195296 A CN201810195296 A CN 201810195296A CN 108482637 A CN108482637 A CN 108482637A
- Authority
- CN
- China
- Prior art keywords
- cantilever
- unmanned plane
- electric pushrod
- cantilevers
- plummer
- 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.)
- Pending
Links
Classifications
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
-
- 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
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Abstract
Cantilever design is received the invention discloses a kind of unmanned plane is electronic, it is related to unmanned plane field, including cantilever plummer, slider assembly and electric machine assembly, the slider assembly includes four electric pushrod cantilevers and four stabiliser bars, four electric pushrod cantilevers are screwed mounted on the center of cantilever plummer, and four electric pushrod cantilevers are circumferentially uniformly distributed, four stabiliser bars are fixedly mounted on by screw successively between two adjacent electric pushrod cantilevers, there are four the electric machine assembly is set, it is respectively and fixedly installed to the end of an electric pushrod cantilever；The structure makes unmanned plane self structure compacter, has the function of cantilever retracting, on the one hand more motor can be protected without damage, on the other hand reduce the overall dimensions of unmanned plane when not used.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of unmanned plane is electronic to receive cantilever design.
Background technology
Unmanned plane can be divided into two major classes substantially, and one kind is fixed-wing formula, and one kind is rotary wind type, with unmanned plane skill
The unmanned plane of the development of art, consumer level more and more occurs on the market, and the unmanned plane of consumer level is rotary wind type mostly,
The unmanned plane of rotary wind type can all have cantilever substantially, and motor is mounted on cantilever, when storing unmanned plane, if cannot incite somebody to action
If motor and rotor retracting are hidden, the risk of damage is had, unnecessary loss can be caused if damage.
Invention content
A kind of unmanned plane of present invention offer is electronic to receive cantilever design, which makes unmanned plane self structure more step up
It gathers, has the function of cantilever retracting, on the one hand more motor can be protected without damage, on the other hand reduce unmanned plane when not used whole
Body size.
To achieve the above object, the present invention provides technical solution below：A kind of unmanned plane is electronic to receive cantilever design, packet
Cantilever plummer, slider assembly and electric machine assembly are included, the slider assembly includes four electric pushrod cantilevers and four stabiliser bars,
Four electric pushrod cantilevers are screwed mounted on the center of cantilever plummer, and four electric pushrods are outstanding
Arm is circumferentially uniformly distributed, and four stabiliser bars are fixedly mounted on by screw successively between two adjacent electric pushrod cantilevers,
There are four the electric machine assembly is set, it is respectively and fixedly installed to the end of an electric pushrod cantilever.
Preferably, the center of the cantilever plummer is equipped with push rod fixed station, and four electric pushrod cantilevers pass through
Screw is fixedly mounted on push rod fixed station.
Preferably, it is uniformly provided with four motors on the cantilever plummer and retracts disk.
Preferably, the electric machine assembly includes motor, rotor and rotor protective cover, and the motor is solid with electric pushrod cantilever
Fixed connection, the rotor are fixedly connected with the output end of motor, and the rotor protective cover is threadedly coupled with motor.
It is using the advantageous effect of above technical scheme：Structure of the invention, which is that a kind of unmanned plane is electronic, receives cantilever design,
The cantilever of the unmanned plane is directly by electric pushrod cantilever instead of actually electric pushrod cantilever essence is exactly electric pushrod, electricity
For dynamic push rod cantilever by the power supply power supply of unmanned plane itself, it is outstanding that four stabiliser bars are respectively and fixedly installed to two adjacent electric pushrods
Between arm, structural strength is enhanced, improves the stability of structure, when using unmanned plane, four electricity can be started
Dynamic push rod cantilever, electric machine assembly is released, and after use, is retractd electric machine assembly by electric pushrod cantilever, is hidden into motor
(there are one the shells covered for cantilever plummer upper end) is retractd in disk, in conclusion the structure makes unmanned plane self structure
It is compacter, have the function of cantilever retracting, on the one hand more motor can be protected without damage, on the other hand reduce unmanned plane and do not have to
When overall dimensions.
Description of the drawings
Fig. 1 is the electronic vertical view for receiving cantilever design of the unmanned plane.
Wherein, 1, cantilever plummer；11, push rod fixed station；12, motor retracts disk；2, slider assembly；21. electric pushrod
Cantilever；22, stabiliser bar；3, electric machine assembly；31, motor；32. rotor；33, rotor protective cover.
Specific implementation mode
Below against attached drawing, by the description of the embodiment, making to the specific implementation mode of the present invention further details of
Explanation, it is therefore an objective to those skilled in the art be helped to have more complete, accurate and deep reason to the design of the present invention, technical solution
Solution, and contribute to its implementation.
Fig. 1 shows the specific implementation mode of the present invention：A kind of unmanned plane is electronic to receive cantilever design, including cantilever plummer
1, slider assembly 2 and electric machine assembly 3, the slider assembly 2 includes four electric pushrod cantilevers 21 and four stabiliser bars 22, described
Four electric pushrod cantilevers 21 are screwed mounted on the center of cantilever plummer 11, and four electric pushrods are outstanding
Arm 21 is circumferentially uniformly distributed, and four stabiliser bars 22 are fixedly mounted on two adjacent electric pushrod cantilevers 21 by screw successively
Between, there are four the electric machine assembly 3 is set, it is respectively and fixedly installed to the end of an electric pushrod cantilever 21.
The center of the cantilever plummer 1 is equipped with push rod fixed station 11, and four electric pushrod cantilevers 21 pass through spiral shell
Silk is fixedly mounted on push rod fixed station 11；It is uniformly provided with four motors on the cantilever plummer 1 and retracts disk 12；The motor
Component 3 includes motor 31, rotor 32 and rotor protective cover 33, and the motor 31 is fixedly connected with electric pushrod cantilever 21, described
Rotor 32 is fixedly connected with the output end of motor 31, and the rotor protective cover 33 is threadedly coupled with motor 31.
The principle of the present invention：
Based on above-mentioned, structure of the invention, which is that a kind of unmanned plane is electronic, receives cantilever design, the cantilever directly quilt of the unmanned plane
Electric pushrod cantilever 21 is instead of actually 21 essence of electric pushrod cantilever is exactly electric pushrod, and electric pushrod cantilever 21 is by nothing
The man-machine power supply power supply of itself, four stabiliser bars 22 are respectively and fixedly installed between two adjacent electric pushrod cantilevers 21, are increased
Strong structural strength, improves the stability of structure, when using unmanned plane, can start four electric pushrod cantilevers
21, electric machine assembly 3 is released, after use, electric machine assembly 3 is retractd by electric pushrod cantilever 21, is hidden into motor retracting
In disk 12 (there are one the shells covered for 1 upper end of cantilever plummer), in conclusion the structure makes unmanned plane self structure more
Step up to gather, has the function of cantilever retracting, on the one hand more motor can be protected without damage, on the other hand reduce unmanned plane when not used
Overall dimensions.
The present invention is exemplarily described above in association with attached drawing, it is clear that the present invention implements not by above-mentioned side
The limitation of formula, as long as using the improvement of the various unsubstantialities of inventive concept and technical scheme of the present invention progress；Or not
It is improved, the above-mentioned design of the present invention and technical solution are directly applied into other occasions, in protection scope of the present invention
Within.
Claims (4)
1. a kind of unmanned plane is electronic to receive cantilever design, it is characterised in that：Including cantilever plummer (1), slider assembly (2) and electricity
Thermomechanical components (3), the slider assembly (2) include four electric pushrod cantilevers (21) and four stabiliser bars (22), four electricity
Dynamic push rod cantilever (21) is screwed the center mounted on cantilever plummer (11), and four electric pushrod cantilevers
(21) it is circumferentially uniformly distributed, four stabiliser bars (22) are fixedly mounted on two adjacent electric pushrod cantilevers by screw successively
(21) between, the electric machine assembly (3) is respectively and fixedly installed to the end of an electric pushrod cantilever (21) there are four setting.
2. a kind of unmanned plane according to claim 1 is electronic to receive cantilever design, it is characterised in that：The cantilever plummer
(1) center is equipped with push rod fixed station (11), and four electric pushrod cantilevers (21) are screwed mounted on push rod
On fixed station (11).
3. a kind of unmanned plane according to claim 1 is electronic to receive cantilever design, it is characterised in that：The cantilever plummer
(1) it is uniformly provided with four motors on and retracts disk (12).
4. a kind of unmanned plane according to claim 1 is electronic to receive cantilever design, it is characterised in that：The electric machine assembly
(3) include motor (31), rotor (32) and rotor protective cover (33), the motor (31) is fixed with electric pushrod cantilever (21) to be connected
It connects, the rotor (32) is fixedly connected with the output end of motor (31), and the rotor protective cover (33) connects with motor (31) screw thread
It connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810195296.5A CN108482637A (en) | 2018-03-09 | 2018-03-09 | A kind of unmanned plane is electronic to receive cantilever design |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810195296.5A CN108482637A (en) | 2018-03-09 | 2018-03-09 | A kind of unmanned plane is electronic to receive cantilever design |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108482637A true CN108482637A (en) | 2018-09-04 |
Family
ID=63338548
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810195296.5A Pending CN108482637A (en) | 2018-03-09 | 2018-03-09 | A kind of unmanned plane is electronic to receive cantilever design |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108482637A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250118A (en) * | 2018-10-18 | 2019-01-22 | 沈阳大学 | A kind of controllable bird claw mechanical gripper device of small drone |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110226892A1 (en) * | 2008-08-08 | 2011-09-22 | William Crowther | Rotary wing vehicle |
| CN204701765U (en) * | 2015-06-03 | 2015-10-14 | 江苏数字鹰科技发展有限公司 | With the multi-rotor aerocraft of rotor and cantilever folding and unfolding |
| CN106005387A (en) * | 2016-07-20 | 2016-10-12 | 张学衡 | Vertical take-off and landing type dehazing aircraft |
| CN205819555U (en) * | 2016-06-27 | 2016-12-21 | 哈尔滨理工大学 | A kind of quadrotor |
| CN107628243A (en) * | 2017-10-21 | 2018-01-26 | 庞海涛 | A kind of garden shaping tree-pruning aircraft |
-
2018
- 2018-03-09 CN CN201810195296.5A patent/CN108482637A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110226892A1 (en) * | 2008-08-08 | 2011-09-22 | William Crowther | Rotary wing vehicle |
| CN204701765U (en) * | 2015-06-03 | 2015-10-14 | 江苏数字鹰科技发展有限公司 | With the multi-rotor aerocraft of rotor and cantilever folding and unfolding |
| CN205819555U (en) * | 2016-06-27 | 2016-12-21 | 哈尔滨理工大学 | A kind of quadrotor |
| CN106005387A (en) * | 2016-07-20 | 2016-10-12 | 张学衡 | Vertical take-off and landing type dehazing aircraft |
| CN107628243A (en) * | 2017-10-21 | 2018-01-26 | 庞海涛 | A kind of garden shaping tree-pruning aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109250118A (en) * | 2018-10-18 | 2019-01-22 | 沈阳大学 | A kind of controllable bird claw mechanical gripper device of small drone |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205396561U (en) | Aircraft that has crashproof gasbag | |
| CN108482637A (en) | A kind of unmanned plane is electronic to receive cantilever design | |
| CN210686198U (en) | Wind power generation device | |
| CN201798778U (en) | Skull dissection drill | |
| CN207828949U (en) | A kind of shockproof easily rammer compacter | |
| CN206164248U (en) | Structure is put to winding | |
| CN101202493B (en) | Integrated set with electromotion and power generation | |
| CN104333190A (en) | Dual counter-rotating generator | |
| CN101504881B (en) | Combined capacitor capable of effectively absorbing harmonic voltage | |
| CN204068588U (en) | A kind of few groove number high voltage direct current micromachine | |
| CN203352402U (en) | Squirrel cage-type motor rotor and plastic-package motor adopting same | |
| CN208508685U (en) | A kind of explosion-proof type is taken photo by plane motor | |
| CN207368072U (en) | A kind of Copper-Aluminum compound pole | |
| CN205161486U (en) | Portable funny cat ware | |
| CN207504694U (en) | A kind of motor and its wind turbine of application | |
| CN208459968U (en) | A kind of novel computer cooling device | |
| CN207004731U (en) | A kind of dot matrix breeze wind unit | |
| CN207000107U (en) | A kind of vehicle-mounted air purification power supply | |
| CN207382082U (en) | A kind of flat wire generator unit stator assembly | |
| CN211266745U (en) | Power adapter safe in utilization | |
| CN205647073U (en) | Electric motor rotor reaches motor that contains this electric motor rotor | |
| CN210776454U (en) | Rotating seat of electronic contest case | |
| CN209994190U (en) | Iron-clad motor with protective housing | |
| CN104595102A (en) | Field wind power electricity supply device | |
| CN101309032B (en) | Wind-driven generator |
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 | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180904 |