CN105947177A - Manned aircraft with variable sweep aerofoils - Google Patents
Manned aircraft with variable sweep aerofoils Download PDFInfo
- Publication number
- CN105947177A CN105947177A CN201610449673.4A CN201610449673A CN105947177A CN 105947177 A CN105947177 A CN 105947177A CN 201610449673 A CN201610449673 A CN 201610449673A CN 105947177 A CN105947177 A CN 105947177A
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- CN
- China
- Prior art keywords
- shape frame
- fixing
- movable
- electric pushrod
- supports
- 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.)
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Classifications
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- 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
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- 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 invention discloses a manned aircraft with variable sweep aerofoils. The manned aircraft comprises a fixed Y-shaped frame, a movable Y-shaped frame, two Y-shaped frame adjusting electric push rods and the like; the fixed Y-shaped frame and the movable Y-shaped frame are each provided with two supports, the movable Y-shaped frame is installed on the fixed Y-shaped frame in a sliding mode, and shells of the two Y-shaped frame adjusting electric push rods are installed at the two sides of the fixed Y-shaped frame respectively; the two sweep aerofoils are hinged to the two sides of the fixed Y-shaped frame respectively, shells of two sweep aerofoil adjusting electric push rods are hinged to the two sides of the fixed Y-shaped frame respectively, and the ends of piston rods of the two sweep aerofoil adjusting electric push rods are hinged to the two sides of the two sweep aerofoils; four telescopic rods are installed in sliding holes of the four supports in a sliding mode respectively. As a mousing bottle controlled by magnet attraction is arranged, power-free automatic mousing is achieved; the manned aircraft is simple in structure and low in cost.
Description
Technical field
The present invention relates to a kind of aircraft devices, be specifically related to a kind of variable sweep wing manned vehicle, belong to aircraft devices technical field.
Background technology
In actual life, the trip of people relies on the vehicles mostly, and in the case of for the trip especially pavement behavior difference of short distance, conventional vehicles volume is bigger, expense is more expensive, inconvenient through barrier, and the problem such as the time length brought of detouring, it is therefore desirable to the time saving and energy saving vehicles of a kind of short distance trip.Having many airhogs more and more higher for the pursuit degree of manned vehicle again, existing manned vehicle has much room for improvement on flight safety and controlling.
Summary of the invention
For the problems referred to above, the present invention provides a kind of variable sweep wing manned vehicle, and it is provided by two Y shape framves and two variable sweep wing, it is achieved that convenient adjustment and the purpose of flight flexibly.
The technical scheme that the present invention takes is: a kind of variable sweep wing manned vehicle, adjust electric pushrods, two swept-back wings and two swept-back wings including fixing Y shape frame and movable Y shape frame, two Y shape framves to adjust electric pushrods, two base supports, four expansion links and four expansion links and adjust electric pushrods, four swivel mounts and four electric rotating machines, driving cabin, power supply and controller, it is characterized in that: described fixing Y shape frame and movable Y shape frame are provided with two supports, and two described supports are mutually perpendicular to；On fixing Y shape frame, two support centre positions are provided with chute, and described movable Y shape frame is slidably mounted on fixing Y shape frame；Two described Y shape framves adjust the housing of electric pushrod and are separately mounted to fixing Y shape frame both sides, and the piston rod end of two Y shape frame adjustment electric pushrods is connected with movable Y shape frame both sides；Two described swept-back wings are respectively articulated with and are arranged on fixing Y shape frame both sides, the housing of two described swept-back wings adjustment electric pushrods is respectively articulated with and is arranged on fixing 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 respectively；Two described base supports are respectively and fixedly installed to fixing Y shape frame and the bottom of movable Y shape frame；Being provided with slide opening on support on described fixing Y shape frame and movable Y shape frame, four described expansion links are slidably mounted in the slide opening on four supports respectively；Four described expansion links adjust the housing of electric pushrod and are separately mounted on four supports, and the end of the piston rod of four expansion link adjustment electric pushrods is connected with four expansion links respectively；Four described electric rotating machines are separately mounted to the end of four expansion links, and four described swivel mounts are rotatably installed on the main shaft of four electric rotating machines respectively；Described driving cabin is fixedly mounted on fixing Y shape frame top；Described power supply and controller are separately mounted on two supports of movable Y shape frame.
Further, the two ends of four described swivel mounts are respectively arranged with angle adjustment motor, it is mounted on fan drum on the main shaft of described each angle adjustment motor, it is rotatablely equipped with fan on described each fan drum, described fan electromotor is arranged on fan drum, and the main shaft of fan electromotor is coaxially connected with fan.
Further, described driving cabin is provided with driver's seat and control knob.
Owing to present invention employs technique scheme, the invention have the advantages that the present invention is provided by the mouse-catching bottle that Magnet suction controls, it is achieved that unpowered, the purpose of automatic mouse-trapping；Present configuration is simple, and cost is relatively low.
Accompanying drawing explanation
Fig. 1 is the overall assembling perspective view of the present invention.
Fig. 2 is the overall assembling perspective view of another angle of the present invention.
Fig. 3 is the assembling perspective view fixing Y shape frame and base support in the present invention.
Fig. 4 is the assembling perspective view of fan drum, fan electromotor and fan in the present invention.
Drawing reference numeral: 1-fixes Y shape frame；2-swept-back wing adjusts electric pushrod；3-Y shape frame adjusts electric pushrod；4-swept-back wing；5-power supply；6-activity Y shape frame；7-controller；8-driving cabin；9-base support；10-swivel mount；11-expansion link；12-angle adjustment motor；13-expansion link adjusts electric pushrod；14-fan electromotor；15-fan drum；16-fan；17-electric rotating machine；101-slide opening.
Detailed description of the invention
Below in conjunction with specific embodiment, the invention will be further described, and the illustrative examples invented at this and explanation are for explaining the present invention, but not as a limitation of the invention.
As shown in Figure 1, Figure 2, Figure 3, Figure 4, a kind of variable sweep wing manned vehicle, adjusts 3, two swept-back wings 4 of electric pushrod including fixing Y shape frame 1 and movable 6, two Y shape framves of Y shape frame and two swept-back wings adjust electric pushrod 9, four expansion links 11 of 2, two base supports and four expansion link adjustment 13, four swivel mounts 10 of electric pushrod and four electric rotating machines 17, driving cabin 8, power supply 5 and controller 7.Fixing Y shape frame 1 and movable Y shape frame 6 are provided with two supports, and two described supports are mutually perpendicular to.On fixing Y shape frame 1, two support centre positions are provided with chute, and movable Y shape frame 6 is slidably mounted on fixing Y shape frame 1.The housing of two Y shape frame adjustment electric pushrods 3 is separately mounted to fixing Y shape frame 1 both sides, and the piston rod end of two Y shape frame adjustment electric pushrods 3 is connected with movable Y shape frame 6 both sides.Two swept-back wings 4 are respectively articulated with and are arranged on fixing Y shape frame 1 both sides, the housing of two swept-back wing adjustment electric pushrods 2 is respectively articulated with and is arranged on fixing Y shape frame 1 both sides, and the end of the piston rod of two swept-back wing adjustment electric pushrods 2 is hingedly mounted on two swept-back wings 4 respectively.Two base supports 9 are respectively and fixedly installed to fixing Y shape frame 1 and the bottom of movable Y shape frame 6.Being provided with slide opening 101 on support on fixing Y shape frame 1 and movable Y shape frame 6, four expansion links 11 are slidably mounted in the slide opening 101 on four supports respectively.The housing of four expansion link adjustment electric pushrods 13 is separately mounted on four supports, and the end of the piston rod of four expansion link adjustment electric pushrods 13 is connected with four expansion links 11 respectively.Four electric rotating machines 17 are separately mounted to the end of four expansion links 11, and four swivel mounts 10 are rotatably installed on the main shaft of four electric rotating machines 17 respectively；Described driving cabin 8 is fixedly mounted on fixing Y shape frame 1 top；Described power supply 5 and controller 7 are separately mounted on two supports of movable Y shape frame 6.
The two ends of four swivel mounts 10 are respectively arranged with angle adjustment motor 12, it is mounted on fan drum 15 on the main shaft of each angle adjustment motor 12, it is rotatablely equipped with fan 16 on each fan drum 15, fan electromotor 14 is arranged on fan drum 15, and the main shaft of fan electromotor 14 is coaxially connected with fan 16.Driving cabin 8 is provided with driver's seat and control knob.
The operation principle of the present invention is: the present invention in use, adjusts electric pushrod 2 by two swept-back wings and can adjust the angle of two swept-back wings 4；Can be adjusted by two Y shape framves adjustment electric pushrods 3 and beat distance between movable Y shape frame 6 and fixing Y shape frame 1, the length that i.e. present invention is overall；Adjust electric pushrod 13 by expansion link and can adjust the distance in the expansion link 11 slide opening 101 in fixing Y shape frame 1 and movable Y shape frame 6 upper bracket；The angle of swivel mount 10 can be adjusted by electric rotating machine 17；The angle in another direction of fan 16 can be adjusted by angle adjustment motor 12.
Claims (3)
1. a variable sweep wing manned vehicle, including fixing Y shape frame (1) and movable Y shape frame (6), two Y shape framves adjust electric pushrod (3), two swept-back wings (4) and two swept-back wings adjust electric pushrod (2), two base supports (9), four expansion links (11) and four expansion links adjust electric pushrod (13), four swivel mounts (10) and four electric rotating machines (17), driving cabin (8), power supply (5) and controller (7), it is characterized in that: described fixing Y shape frame (1) and movable Y shape frame (6) are provided with two supports, two described supports are mutually perpendicular to；Fixing upper two the support centre positions of Y shape frame (1) are provided with chute, and described movable Y shape frame (6) is slidably mounted on fixing Y shape frame (1)；Two described Y shape framves adjust the housing of electric pushrod (3) and are separately mounted to fixing Y shape frame (1) both sides, and the piston rod end of two Y shape framves adjustment electric pushrod (3) is connected with movable Y shape frame (6) both sides；Two described swept-back wings (4) are respectively articulated with and are arranged on fixing Y shape frame (1) both sides, the housing of two described swept-back wings adjustment electric pushrod (2) is respectively articulated with and is arranged on fixing Y shape frame (1) both sides, and the end of the piston rod of two swept-back wings adjustment electric pushrod (2) is hingedly mounted on two swept-back wings (4) respectively；Two described base supports (9) are respectively and fixedly installed to fixing Y shape frame (1) and the bottom of movable Y shape frame (6)；It is provided with slide opening (101), in the slide opening (101) that four described expansion links (11) are slidably mounted on four supports respectively on support on described fixing Y shape frame (1) and movable Y shape frame (6)；Four described expansion links adjust the housing of electric pushrod (13) and are separately mounted on four supports, and the end of the piston rod of four expansion links adjustment electric pushrod (13) is connected with four expansion links (11) respectively；Four described electric rotating machines (17) are separately mounted to the end of four expansion links (11), and four described swivel mounts (10) are rotatably installed on the main shaft of four electric rotating machines (17) respectively；Described driving cabin (8) is fixedly mounted on fixing Y shape frame (1) top；Described power supply (5) and controller (7) are separately mounted on two supports of movable Y shape frame (6).
2. a kind of variable sweep wing manned vehicle as claimed in claim 1, it is characterized in that: the two ends of four described swivel mounts (10) are respectively arranged with angle adjustment motor (12), it is mounted on fan drum (15) on the main shaft of described each angle adjustment motor (12), it is rotatablely equipped with fan (16) on described each fan drum (15), described fan electromotor (14) is arranged on fan drum (15), and the main shaft of fan electromotor (14) is coaxially connected with fan (16).
3. a kind of variable sweep wing manned vehicle as claimed in claim 1, it is characterised in that: described driving cabin (8) is provided with driver's seat and control knob.
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 true CN105947177A (en) | 2016-09-21 |
| CN105947177B 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) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110891859A (en) * | 2017-07-27 | 2020-03-17 | 株式会社辰巳菱机 | Suspension type mobile device |
| CN111697485A (en) * | 2020-06-11 | 2020-09-22 | 高强 | High-voltage line deicing aircraft |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1296361A (en) * | 1969-02-14 | 1972-11-15 | ||
| CN101028866A (en) * | 2007-03-30 | 2007-09-05 | 哈尔滨工业大学 | Aircraft with wing sweepback angle change |
| RU2316449C2 (en) * | 2005-11-03 | 2008-02-10 | Николай Михайлович Барабанщиков | Aircraft |
| CN103593524A (en) * | 2013-11-13 | 2014-02-19 | 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 |
| CN205076045U (en) * | 2015-10-29 | 2016-03-09 | 安徽理工大学 | Combined type aircraft of varistructure |
| 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 |
| 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
Patent Citations (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 |
| CN101028866A (en) * | 2007-03-30 | 2007-09-05 | 哈尔滨工业大学 | Aircraft with wing sweepback angle change |
| CN103593524A (en) * | 2013-11-13 | 2014-02-19 | 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 |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110891859A (en) * | 2017-07-27 | 2020-03-17 | 株式会社辰巳菱机 | Suspension type mobile device |
| EP3659915A4 (en) * | 2017-07-27 | 2021-04-28 | Tatsumi Ryoki Co., Ltd | Hovering vehicle |
| CN111697485A (en) * | 2020-06-11 | 2020-09-22 | 高强 | High-voltage line deicing aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105947177B (en) | 2018-07-10 |
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| Date | Code | Title | Description |
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| 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 |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |