CN105947177B - A kind of swing-wing manned vehicle - Google Patents
A kind of swing-wing manned vehicle Download PDFInfo
- Publication number
- CN105947177B CN105947177B CN201610449673.4A CN201610449673A CN105947177B CN 105947177 B CN105947177 B CN 105947177B CN 201610449673 A CN201610449673 A CN 201610449673A CN 105947177 B CN105947177 B CN 105947177B
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- China
- Prior art keywords
- shape frame
- fixed
- swept
- movable
- shape
- Prior art date
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
-
- 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
- B64U30/10—Wings
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The present invention disclose a kind of swing-wing manned vehicle, including fixed Y shape frame and movable Y shape frame, two Y shape framves adjustment electric pushrods etc., fixed Y shape frame and movable Y shape frame be respectively provided with there are two stent；Movable Y shape frame is slidably mounted on fixed Y shape frame；The housing of two Y shape frame adjustment electric pushrods is separately mounted to fixed Y shape frame both sides；Two swept-back wings are respectively articulated with mounted on fixed Y shape frame both sides, and the housing of two swept-back wing adjustment electric pushrods is respectively articulated with mounted on fixed Y shape frame both sides, and the end of the piston rod of two swept-back wing adjustment electric pushrods is hingedly mounted on two swept-back wings；Four telescopic rods are slidably mounted on respectively in the slide opening on four stents.The mouse-catching bottle that the present invention is controlled by being provided with magnet suction, realizes unpowered, automatic mouse-trapping purpose；The configuration of the present invention is simple, cost are relatively low.
Description
Technical field
The present invention relates to a kind of aircraft devices, and in particular to a kind of swing-wing manned vehicle belongs to aircraft
Equipment technical field.
Background technology
In actual life, the trip of people relies on the vehicles mostly, and for the trip especially pavement behavior of short distance
In the case of difference, conventional vehicles volume is larger, and expense is more expensive, across barrier it is inconvenient and detour bring when
Between it is long the problems such as, it is therefore desirable to a kind of time saving and energy saving vehicles of short distance trip.Again there are many airhog for carrying
The pursuit degree of people's aircraft is also higher and higher, and existing manned vehicle is to be improved on flight safety and controlling.
Invention content
In view of the above-mentioned problems, the present invention provides a kind of swing-wing manned vehicle, by setting, there are two Y shape framves
And two swing-wing, realize convenient adjustment and the purpose flexibly flown.
The technical solution that the present invention takes is：A kind of swing-wing manned vehicle, including fixed Y shape frame and activity Y
Shape frame, two Y shape frame adjustment electric pushrods, two swept-back wings and two swept-back wing adjustment electric pushrods, two base supports, four
A telescopic rod and four telescopic rod adjustment electric pushrods, four swivel mounts and four electric rotating machines, cockpit, power supply and control
Device, it is characterised in that：The fixation Y shape frame and movable Y shape frame are respectively provided with there are two stent, and described two stents mutually hang down
Directly；Two stent centre positions are provided with sliding slot on fixed Y shape frame, and the movable Y shape frame is slidably mounted on fixed Y shape frame
On；The housing of two Y shape framves adjustment electric pushrod is separately mounted to fixed Y shape frame both sides, and two Y shape frame adjustment are electronic
The piston rod end of push rod is connected with movable Y shape frame both sides；Two swept-back wings are respectively articulated with mounted on fixed Y shape frame
Both sides, the housing of described two swept-back wing adjustment electric pushrods are respectively articulated with mounted on fixed Y shape frame both sides, two swept-back wings
The end for adjusting the piston rod of electric pushrod is respectively articulated on two swept-back wings；Two base supports are solid respectively
Dingan County is mounted in the lower part of fixed Y shape frame and movable Y shape frame；It is respectively provided on stent on the fixation Y shape frame and movable Y shape frame
There is slide opening, described four telescopic rods are slidably mounted on respectively in the slide opening on four stents；Four telescopic rods adjustment
The housing of electric pushrod is separately mounted on four stents, the end of the piston rod of four telescopic rods adjustment electric pushrod respectively with
Four telescopic rods are connected；Four electric rotating machines are separately mounted to the end of four telescopic rods, described four rotations
Frame is rotatably installed in respectively on the main shaft of four electric rotating machines；The cockpit is fixedly mounted on fixed Y shape frame top；It is described
Power supply and controller be separately mounted on two stents of movable Y shape frame.
Further, the both ends of four swivel mounts are respectively arranged with angle adjustment motor, each angle
It adjusts and is mounted on fan drum on the main shaft of motor, fan, the wind are rotatablely equipped on each fan drum
It fans motor to be mounted on fan drum, the main shaft and fan of fan electromotor are coaxially connected.
Further, driver's seat and control button are provided in the cockpit.
Since present invention employs above-mentioned technical proposal, the present invention has the following advantages：There are two Y by setting by the present invention
Shape frame and two swing-wing realize convenient adjustment and the purpose flexibly flown；The configuration of the present invention is simple, cost compared with
It is low.
Description of the drawings
Fig. 1 is the whole assembling dimensional structure diagram of the present invention.
Fig. 2 is the whole assembling dimensional structure diagram of another angle of the present invention.
Fig. 3 is the assembling dimensional structure diagram that Y shape frame and base support are fixed in the present invention.
Fig. 4 is the assembling dimensional structure diagram of fan drum, fan electromotor and fan in the present invention.
Drawing reference numeral：1- fixes Y shape frame；2- swept-back wings adjust electric pushrod；3-Y shapes frame adjusts electric pushrod；4- sweepback
The wing；5- power supplys；6- activity Y shape framves；7- controllers；8- cockpits；9- base supports；10- swivel mounts；11- telescopic rods；12- angles
Degree adjustment motor；13- telescopic rods adjust electric pushrod；14- fan electromotors；15- fan drums；16- fans；17- electric rotating machines；
101- slide openings.
Specific embodiment
With reference to specific embodiment, the invention will be further described, in the illustrative examples and explanation of the invention
For explaining the present invention, but it is not as a limitation of the invention.
As shown in Figure 1, Figure 2, Figure 3, Figure 4, a kind of swing-wing manned vehicle, including fixed Y shape frame 1 and activity Y
6, two Y shape frame adjustment 3, two swept-back wings 4 of electric pushrod of shape frame and two swept-back wing adjustment 2, two pedestal branch of electric pushrod
9, four telescopic rods 11 of frame and four telescopic rod adjustment 13, four swivel mounts 10 of electric pushrod and four electric rotating machines 17 drive
Cabin 8, power supply 5 and controller 7.Fixed Y shape frame 1 and movable Y shape frame 6 are respectively provided with there are two stent, and described two stents are mutual
Vertically.Two stent centre positions are provided with sliding slot on fixed Y shape frame 1, and movable Y shape frame 6 is slidably mounted on fixed Y shape frame 1.
The housing of two Y shape frame adjustment electric pushrods 3 is separately mounted to fixed 1 both sides of Y shape frame, and two Y shape framves adjust electric pushrod 3
Piston rod end is connected with movable 6 both sides of Y shape frame.Two swept-back wings 4, which are respectively articulated with, is mounted on fixed 1 both sides of Y shape frame, two
The housing of swept-back wing adjustment electric pushrod 2 is respectively articulated with mounted on fixed 1 both sides of Y shape frame, and two swept-back wings adjust electric pushrod 2
The end of piston rod be respectively articulated on two swept-back wings 4.Two base supports 9 are respectively and fixedly installed to fixed Y shape
The lower part of frame 1 and movable Y shape frame 6.Slide opening 101 is both provided on stent on fixed Y shape frame 1 and movable Y shape frame 6, four are stretched
Contracting bar 11 is slidably mounted on respectively in the slide opening 101 on four stents.The housing difference of four telescopic rod adjustment electric pushrods 13
On four stents, the end of the piston rod of four telescopic rod adjustment electric pushrods 13 is connected respectively with four telescopic rods 11
It connects.Four electric rotating machines 17 are separately mounted to the end of four telescopic rods 11, and four swivel mounts 10 are rotatably installed in four respectively
On the main shaft of electric rotating machine 17；The cockpit 8 is fixedly mounted on fixed 1 top of Y shape frame；The power supply 5 and controller 7
It is separately mounted on two stents of movable Y shape frame 6.
The both ends of four swivel mounts 10 are respectively arranged with angle adjustment motor 12, and each angle is adjusted on the main shaft of motor 12
Fan drum 15 is mounted on, fan 16 is rotatablely equipped on each fan drum 15, fan electromotor 14 is mounted on fan drum
On 15, the main shaft and fan 16 of fan electromotor 14 are coaxially connected.Driver's seat and control button are provided in cockpit 8.
The present invention operation principle be：In the use of the present invention, adjusting electric pushrod 2 by two swept-back wings can adjust
The angle of two swept-back wings 4；By two Y shape framves adjust electric pushrods 3 can adjust movable Y shape frame 6 and fixed Y shape frame 1 it
Between beat distance, i.e. the whole length of the present invention；Telescopic rod 11 can be adjusted in fixed Y shape by adjusting electric pushrod 13 by telescopic rod
The distance in slide opening 101 in frame 1 and movable 6 upper bracket of Y shape frame；The angle of swivel mount 10 can be adjusted by electric rotating machine 17
Degree；The angle in 16 another direction of fan can be adjusted by adjusting motor 12 by angle.
Claims (3)
1. a kind of swing-wing manned vehicle, including fixed Y shape frame（1）With movable Y shape frame（6）, two Y shape frame adjustment electricity
Dynamic push rod（3）, two swept-back wings（4）Electric pushrod is adjusted with two swept-back wings（2）, two base supports（9）, four telescopic rods
（11）Electric pushrod is adjusted with four telescopic rods（13）, four swivel mounts（10）With four electric rotating machines（17）, cockpit（8）、
Power supply（5）And controller（7）, it is characterised in that：The fixation Y shape frame（1）With movable Y shape frame（6）It is propped up there are two being respectively provided with
Frame, described two stents are mutually perpendicular to；Fixed Y shape frame（1）Upper two stent centre positions are provided with sliding slot, the activity
Y shape frame（6）It is slidably mounted on fixed Y shape frame（1）On；Two Y shape framves adjustment electric pushrod（3）Housing install respectively
In fixed Y shape frame（1）Both sides, two Y shape framves adjust electric pushrod（3）Piston rod end and movable Y shape frame（6）Both sides are connected
It connects；Two swept-back wings（4）It is respectively articulated with mounted on fixed Y shape frame（1）Both sides, described two swept-back wing adjustment are electronic
Push rod（2）Housing be respectively articulated with mounted on fixed Y shape frame（1）Both sides, two swept-back wings adjust electric pushrod（2）Piston rod
End be respectively articulated with mounted on two swept-back wings（4）On；Two base supports（9）It is respectively and fixedly installed to fixed Y
Shape frame（1）With movable Y shape frame（6）Lower part；The fixation Y shape frame（1）With movable Y shape frame（6）On stent on be respectively provided with
There is slide opening（101）, four telescopic rods（11）The slide opening being slidably mounted on respectively on four stents（101）In；Described
Four telescopic rods adjust electric pushrod（13）Housing be separately mounted on four stents, four telescopic rods adjust electric pushrods
（13）Piston rod end respectively with four telescopic rods（11）It is connected；Four electric rotating machines（17）It is separately mounted to
Four telescopic rods（11）End, described four swivel mounts（10）It is rotatably installed in four electric rotating machines respectively（17）Main shaft
On；The cockpit（8）It is fixedly mounted on fixed Y shape frame（1）Top；The power supply（5）And controller（7）It installs respectively
In movable Y shape frame（6）Two stents on.
2. a kind of swing-wing manned vehicle as described in claim 1, it is characterised in that：Four swivel mounts
（10）Both ends be respectively arranged with angle adjustment motor（12）, each angle adjustment motor（12）Main shaft on be respectively mounted
There is fan drum（15）, each fan drum（15）On be rotatablely equipped with fan（16）, fan electromotor（14）It is mounted on
Fan drum（15）On, fan electromotor（14）Main shaft and fan（16）It is coaxially connected.
3. a kind of swing-wing manned vehicle as described in claim 1, it is characterised in that：The cockpit（8）In
It is provided with driver's seat and control button.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610449673.4A CN105947177B (en) | 2016-06-21 | 2016-06-21 | A kind of swing-wing manned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610449673.4A CN105947177B (en) | 2016-06-21 | 2016-06-21 | A kind of swing-wing manned vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105947177A CN105947177A (en) | 2016-09-21 |
| CN105947177B true CN105947177B (en) | 2018-07-10 |
Family
ID=56906271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610449673.4A Active CN105947177B (en) | 2016-06-21 | 2016-06-21 | A kind of swing-wing manned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105947177B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019021521A1 (en) * | 2017-07-27 | 2019-01-31 | 株式会社辰巳菱機 | Hovering vehicle |
| CN111697485B (en) * | 2020-06-11 | 2021-07-23 | 高强 | High-voltage line deicing aircraft |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1296361A (en) * | 1969-02-14 | 1972-11-15 | ||
| RU2316449C2 (en) * | 2005-11-03 | 2008-02-10 | Николай Михайлович Барабанщиков | Aircraft |
| CN100429119C (en) * | 2007-03-30 | 2008-10-29 | 哈尔滨工业大学 | Aircraft with wing sweepback angle change |
| CN103593524B (en) * | 2013-11-13 | 2014-10-01 | 北京航空航天大学 | Dynamics modeling and analyzing method for aerospace vehicle |
| CN105083532A (en) * | 2015-08-14 | 2015-11-25 | 中国航空工业集团公司西安飞机设计研究所 | Variable unmanned aerial vehicle |
| CN205203378U (en) * | 2015-08-24 | 2016-05-04 | 深圳市诺亚星辰科技开发有限公司 | Improved multi -rotor unmanned aerial vehicle |
| CN205076045U (en) * | 2015-10-29 | 2016-03-09 | 安徽理工大学 | Combined type aircraft of varistructure |
| CN205221092U (en) * | 2015-11-06 | 2016-05-11 | 珠海华迈航空科技有限公司 | Four -rotor aircraft |
-
2016
- 2016-06-21 CN CN201610449673.4A patent/CN105947177B/en active Active
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| Publication number | Publication date |
|---|---|
| CN105947177A (en) | 2016-09-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Zheng Zhenyang Inventor after: Xu Rongting Inventor before: The inventor has waived the right to be mentioned |
|
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20180523 Address after: 362100 West Pavilion No. 11, Lian Yan village, Feng Mei Town, Quangang District, Quanzhou, Fujian. Applicant after: Zheng Zhenyang Address before: 054999 107 Yao Lou village, Luzhai Township, Linxi County, Xingtai, Hebei Applicant before: Xu Rongting |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |