CN101987565A - Vertical takeoff and landing flying car - Google Patents
Vertical takeoff and landing flying car Download PDFInfo
- Publication number
- CN101987565A CN101987565A CN2009100947941A CN200910094794A CN101987565A CN 101987565 A CN101987565 A CN 101987565A CN 2009100947941 A CN2009100947941 A CN 2009100947941A CN 200910094794 A CN200910094794 A CN 200910094794A CN 101987565 A CN101987565 A CN 101987565A
- Authority
- CN
- China
- Prior art keywords
- rotor
- rotor wing
- shaft
- conical insert
- rotor shaft
- 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
- 239000003381 stabilizer Substances 0.000 claims abstract description 9
- 230000005540 biological transmission Effects 0.000 claims description 28
- 230000006835 compression Effects 0.000 claims description 8
- 238000007906 compression Methods 0.000 claims description 8
- 230000008878 coupling Effects 0.000 abstract description 3
- 238000010168 coupling process Methods 0.000 abstract description 3
- 238000005859 coupling reaction Methods 0.000 abstract description 3
- 230000000737 periodic effect Effects 0.000 abstract 2
- 238000006243 chemical reaction Methods 0.000 abstract 1
- 239000003638 chemical reducing agent Substances 0.000 abstract 1
- 230000000712 assembly Effects 0.000 description 4
- 238000000429 assembly Methods 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 2
- 230000008602 contraction Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000005520 electrodynamics Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- 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
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Arrangement And Driving Of Transmission Devices (AREA)
- Gear Transmission (AREA)
Abstract
The invention discloses a vertical takeoff and landing flying car, wherein, the upper part of a car body is equipped with an upper rotor wing and a lower rotor wing which coaxially rotate reversely; the upper rotor wing and the lower rotor wing are provided with automatic rotor wing positioning and folding devices for automatically folding backwards the rotor wings; a telescopic device for an internal rotor wing shaft is arranged at the lower part of a cone gear main speed reducer; an external rotor wing shaft is equipped with an automatic rotor wing shaft positioning device for automatically positioning backwards the folded upper rotor wing and the folded lower rotor wing; the lower rotor wing is provided with a periodic moment and total moment control device; power conversion between the rotor wings and wheels can be conveniently controlled, and a controllable coupling controls disconnection and connection; the rear part of the car body is equipped with a controllable rotor wing support doubling as a stabilizer fin; when the vertical takeoff and landing flying car runs on a road, the controllable rotor wing support doubling as the stabilizer fin rotates to rise for supporting and fixing the rear parts of the upper rotor wing and the lower rotor wing, and rotates to fall down when the car vertically takes off and lands as well as flies; and the upper rotor wing extends to depart from the lower rotor wing and coaxially rotate reversely with the lower rotor wing to generate a lifting force for controlling the periodic moment and total moment control device and an accelerator so that the vertical takeoff and landing flying car can vertically take off and land as well as fly. The vertical takeoff and landing flying car provided by the invention can run normally on the road and vertically take off and land.
Description
Technical field
The invention belongs to a kind of hovercar, more particularly, it relates to a kind of vertical take-off and landing flying car.
Background technology
Up to the present, hovercar was developed many types, but really the hovercar of energy vertical takeoff and landing does not still enter the practical stage, Chinese patent publication number CN1718458A, open day is on January 11st, 2006, and name is called and discloses a kind of Heliflying automobile with telescopic propeller blade and overlapping telescopic propeller blade in " vertical flight automobile ", because its propeller blade is still bigger after shrinking, some other defective is very limited the practicality of this vertical flight automobile in addition.
Summary of the invention
The present invention has overcome the deficiencies in the prior art, provide a kind of simple in structure, be easy to manufacture, can be as automobile cruising on highway, in particular cases again can be as the autogyro vertical takeoff and landing, the vertical take-off and landing flying car of flight, in order to solve above technical matters, the present invention is achieved by the following technical solutions, vertical take-off and landing flying car of the present invention comprises driving engine, change-speed box, wheel, vehicle body, operator's compartment, described vertical take-off and landing flying car body top section is equipped with the last rotor and the following rotor of contrarotation, the rotor self-orientation collecting device that rotor is drawn in automatically backward is housed on last rotor and the following rotor, last rotor is connected with interior rotor shaft, following rotor is connected with outer rotor shaft, be equipped with on the outer rotor shaft and can make rotor and following rotor draw the rotor shaft automatic positioning equipment that locate automatically backward the back in, interior rotor shaft is connected with the conical insert main reduction gear with outer rotor shaft, conical insert main reduction gear below is equipped with axially following contraction of interior rotor rotor is contracted downwards to folding the interior rotor shaft extension compression apparatus of position with backspin wingheaviness, following rotor is equipped with cycle square and total square control setup, power-transfer clutch is housed on the driving engine, by the control connection or the disconnection of controlled coupler separately, engine output can be through transmission shaft, the conical insert driving device, controlled coupler, transmission shaft is connected with the conical insert main reduction gear, engine output also can be through transmission shaft, the conical insert driving device, controlled coupler, transmission shaft is connected with change-speed box, body tail is equipped with the controlled rotor support stabilizer of holding concurrently, need at hovercar under the situation of vertical takeoff and landing and flight, put down the controlled rotor support stabilizer of holding concurrently, disconnect the controlled coupler between conical insert driving device and the change-speed box, be communicated with the controlled coupler between conical insert driving device and the conical insert main reduction gear, engine power is through power-transfer clutch, the conical insert driving device, controlled coupler, the conical insert main reduction gear, rotor shaft drives the rotation of the contrarotation bispin wing, manipulation cycle square and total square control setup, the throttle equal controller can make vertical take-off and landing flying car as efficient vertical takeoff and landing of helicopter and flight, has increased the manoevreability of automobile greatly.
Description of drawings
Accompanying drawing is an embodiments of the invention theory structure scheme drawing.
Among the figure: rotor is located on the collecting device 1 interior rotor shaft 2 rotor 3 power transmission shafts 4 controllable couplings 5 conical tooth transmission devices 6 power transmission shafts 7 controlled rotor supports stabilizer 8 rear wheels 9 power transmission shafts 10 engines 11 clutches 12 universal joints 13 conical tooth transmission devices 14 speed changers 15 power transmission shafts 16 controllable couplings 17 interior rotor shaft extension compression apparatus 18 front vehicle wheels 19 vehicle bodies, 20 driver's cabins, 21 conical tooth main reducing gears, 22 rotor shaft automatic positioning equipments, 23 cycle square and 25 times rotors of total square control device 24 outer rotor shaft, 26 differential mechanisms 27 of holding concurrently automatically
The specific embodiment
The invention will be further described below in conjunction with accompanying drawing.
In the accompanying drawings, vertical take-off and landing flying car, comprise driving engine 11, change-speed box 15, front vehicle wheel 19, rear wheel 9, vehicle body 20, operator's compartment 21, the last rotor 3 and the following rotor 26 of contrarotation is equipped with on vehicle body 20 tops, the rotor self-orientation collecting device 1 that rotor is drawn in automatically backward is housed on last rotor 3 and the following rotor 26, last rotor 3 is connected with interior rotor shaft 2, following rotor 26 is connected with outer rotor shaft 25, be equipped with on the outer rotor shaft 25 and can make rotor 3 and following rotor 26 draw the rotor shaft automatic positioning equipment 23 that locate automatically backward the back in, interior rotor shaft 2 is connected with conical insert main reduction gear 22 with outer rotor shaft 25, conical insert main reduction gear 22 belows be equipped with interior rotor shaft 2 shrink downwards make rotor 3 contract downwards to the interior rotor shaft extension compression apparatus 18 of following rotor 26 lap positions, following rotor 26 is equipped with cycle square and total square control setup 24, power-transfer clutch 12 is housed on the driving engine 11, disconnect controlled coupler 17, be communicated with controlled coupler 5, driving engine 11 horsepower outputs are through transmission shaft 7, conical insert driving device 6, controlled coupler 5, transmission shaft 4 is connected with conical insert main reduction gear 22, disconnect controlled coupler 5, be communicated with controlled coupler 17, driving engine 11 horsepower outputs are through transmission shaft 7, conical insert driving device 6, controlled coupler 17, transmission shaft 16 is connected with change-speed box 15, the controlled rotor support stabilizer 8 of holding concurrently is equipped with at vehicle body 20 rear portions, the configuration design of vertical take-off and landing flying car is similar to the general-utility car design substantially, be provided with rotor 3 and following rotor 26 on the top of vertical take-off and landing flying car, when vertical take-off and landing flying car travels on highway, the rotor self-orientation collecting device 1 of last rotor 3 and following rotor 26 and rotor shaft automatic positioning equipment 23 will be gone up rotor 3 and locate gathering backward with following rotor 26, interior rotor shaft extension compression apparatus 18 will go up rotor 3 contract downwards to following rotor 26 lap positions in, rotor shaft retractor device 18 is made of fluid pressure type telescoping mechanism or electrodynamic type retractor device, the expansion link of interior rotor shaft extension compression apparatus 18 upper end is connected with interior rotor shaft 2 lower ends, interior rotor shaft extension compression apparatus 18 with interior rotor shaft 2 shrink downwards make rotor 3 contract downwards to following rotor 26 lap positions, counter-clockwise rotate controlled rotor support hold concurrently stabilizer 8 to vehicle body 20 upright positions, the following rotor 26 and last rotor 3 rear portions of drawing the overlapping placement in back backward in are fixedly held, conical insert driving device 6 is that the vertical mutually conical insert of placing constitutes, and as transmission power output being divided into level and vertical direction output, controlled coupler is the controlled coupler of spline, stir disconnection that splined sleeve on the castellated shaft can realize transmission shaft and be communicated with, controlled coupler between conical insert driving device 6 and the conical insert main reduction gear 22 5 is disconnected, conical insert driving device 6 is communicated with controlled coupler 17 between the change-speed box 15, the horsepower output of driving engine 11 will be through power-transfer clutch 12, transmission shaft 7, conical insert driving device 6, controlled coupler 17, transmission shaft 16, change-speed box 15, conical insert driving device 14, universal-joint 13, transmission shaft 10 sends to rear wheel 9 bonded assembly difies 27 drive rear wheels 9 and rotates, change-speed box 15 is a vehicular transmission, neutral gear can be arranged, several D Drives and reverse gear, at this moment vertical take-off and landing flying car can be used as general-utility car and equally handles on highway and travel, as runs into extraordinary circumstances, disconnected as traffic congestion and road, at the end of one's rope when needing vertical takeoff and landing and flight, the stabilizer 8 of earlier controlled rotor support being held concurrently goes to and vehicle body 20 level attitudes in the direction of the clock, above rotor shaft extension compression apparatus 18 stretches to interior rotor shaft 2 and the last rotor 3 that is attached thereto in handling, controlled coupler between conical insert driving device 6 and the change-speed box 15 17 is disconnected, again conical insert driving device 6 is communicated with controlled coupler 5 between the conical insert main reduction gear 22, conical insert main reduction gear 22 for two big conical inserts of boring flank of tooth symmetry up and down and placing and with transmission shaft 4 bonded assemblys be positioned over two in the middle of the big conical insert the fine taper teeth and be configured to, transmission shaft 4 drives the fine taper teeth and rotates, moving two the big conical inserts of fine taper cingulum are done hand of rotation rotation in opposite directions, big conical insert above in the conical insert main reduction gear 22 is connected with outer rotor shaft 25, and following big conical insert is connected with interior rotor shaft 2, and interior rotor shaft 2 and outer rotor shaft 25 are made coaxial reverse, interior rotor shaft 2 is interior outer double-layer structure, internal layer is a spline shaft structure, and outer upper end flushes with outer rotor shaft 25 upper ends substantially, and outer upper part is the splined sleeve structure, the lower end is connected with following big conical insert in the conical insert main reduction gear 22, internal layer castellated shaft upper end is connected with last rotor 3, is that spline is connected with outer splined sleeve below, gets final product transferring power like this, can stretch up and down again, the power of driving engine 11 outputs is through power-transfer clutch 12, transmission shaft 7, conical insert driving device 6, controlled coupler 5, transmission shaft 4, conical insert main reduction gear 22, drive with conical insert main reduction gear 22 bonded assemblys in rotor shaft 2 and outer rotor shaft 25 make contrarotation, make with interior rotor shaft 2 bonded assemblys on rotor 3 and with outer rotor shaft 25 bonded assemblys under rotor 26 make contrarotation, generation lift, following rotor 26 is equipped with cycle square and total square control setup 24, be the described device that is used for the cross plate of phase control and is used for the control of rotor angle of general helicopter, the vertical takeoff and landing of vertical take-off and landing flying car, before fly, turn to and hover all by handling control cycle square and total square control setup, spring and fixed support after controls such as throttle, rotor self-orientation collecting device 1 are drawn in by last rotor 3 and following rotor 26 between forward two rotors constitute, because the gathering of vertical take-off and landing flying car rotor when vertical takeoff and landing and open all and finish on ground, therefore after even rotor self-orientation collecting device is out of order and lost efficacy, still availablely manually realize the gathering of rotor and open, therefore use very safety and conveniently, rotor shaft automatic positioning equipment 23 is by constituting with outer rotor shaft 25 or the disk and the lock spare of captiveing joint with interior rotor shaft 2, among the embodiment, rotor is arranged as equilateral triangle, when two rotors that rotor self-orientation collecting device 1 is installed during in the position, dead ahead, the position of control robot control system(RCS) locking rotor shaft automatic positioning equipment 23 disks, can be on disk perforating locking or put breach pin locking at the disk edge.
Claims (3)
1. vertical take-off and landing flying car, comprise driving engine (11), change-speed box (15), front vehicle wheel (19), rear wheel (9), vehicle body (20), operator's compartment (21), it is characterized in that vehicle body (20) top is equipped with the last rotor (3) and the following rotor (26) of contrarotation, the rotor self-orientation collecting device (1) that rotor is drawn in automatically backward is housed on last rotor (3) and the following rotor (26), last rotor (3) is connected with interior rotor shaft (2), following rotor (26) is connected with outer rotor shaft (25), be equipped with on the outer rotor shaft (25) and can make rotor (3) and following rotor (26) draw the rotor shaft automatic positioning equipment (23) that locate automatically backward the back in, interior rotor shaft (2) is connected with conical insert main reduction gear (22) with outer rotor shaft (25), conical insert main reduction gear (22) below be equipped with interior rotor shaft (2) shrink downwards make rotor (3) contract downwards to the interior rotor shaft extension compression apparatus (18) of following rotor (26) lap position, following rotor (26) is equipped with cycle square and total square control setup (24).
2. vertical take-off and landing flying car according to claim 1, it is characterized in that, power-transfer clutch (12) is housed on the described driving engine (11), disconnect controlled coupler (17), be communicated with controlled coupler (5), driving engine (11) horsepower output is through transmission shaft (7), conical insert driving device (6), controlled coupler (5), transmission shaft (4) is connected with conical insert main reduction gear (22), disconnect controlled coupler (5), be communicated with controlled coupler (17), driving engine (11) horsepower output is through transmission shaft (7), conical insert driving device (6), controlled coupler (17), transmission shaft (16) is connected with change-speed box (15).
3. vertical take-off and landing flying car according to claim 1 is characterized in that, the controlled rotor support stabilizer (8) of holding concurrently is equipped with at described vehicle body (20) rear portion.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100947941A CN101987565A (en) | 2009-08-04 | 2009-08-04 | Vertical takeoff and landing flying car |
| PCT/CN2010/001190 WO2011015038A1 (en) | 2009-08-04 | 2010-08-04 | Flying car with vertical takeoff and landing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100947941A CN101987565A (en) | 2009-08-04 | 2009-08-04 | Vertical takeoff and landing flying car |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101987565A true CN101987565A (en) | 2011-03-23 |
Family
ID=43543888
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009100947941A Pending CN101987565A (en) | 2009-08-04 | 2009-08-04 | Vertical takeoff and landing flying car |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN101987565A (en) |
| WO (1) | WO2011015038A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103770589A (en) * | 2014-02-28 | 2014-05-07 | 武汉蓝天翔航空科技有限公司 | Flying car |
| CN105196815A (en) * | 2015-10-27 | 2015-12-30 | 陈晓春 | Synchronous turnover mechanism applied to aerocar |
| CN108032692A (en) * | 2017-11-30 | 2018-05-15 | 吉林大学 | Novel screw type offroad vehicle |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102490559A (en) * | 2011-11-23 | 2012-06-13 | 许明坚 | Airphibious vehicle |
| CN107791763B (en) * | 2017-09-27 | 2020-06-23 | 北京航空航天大学 | Telescopic tail stay bar for flying car |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3625631A (en) * | 1969-11-03 | 1971-12-07 | Bell Aerospace Corp | Rotor hub and blade folding system |
| JPH08150818A (en) * | 1994-11-29 | 1996-06-11 | Rokuro Hosoda | Multifuctional helicopter |
| CN1067636C (en) * | 1996-12-11 | 2001-06-27 | 石家智 | Vehicle convertible into aircraft |
| CN1699085A (en) * | 2004-05-18 | 2005-11-23 | 曾稳清 | Vehicle capable of flying |
| US7530790B2 (en) * | 2006-09-20 | 2009-05-12 | Sikorsky Aircraft Corporation | Rotor blade folding system |
| CN201158285Y (en) * | 2008-01-11 | 2008-12-03 | 王学威 | Dual-purpose automobile for open area |
| CN201220750Y (en) * | 2008-06-12 | 2009-04-15 | 张庆柳 | Vertically taking off and landing airplane |
| CN101612870B (en) * | 2008-06-26 | 2013-09-11 | 张庆柳 | Vertical take-off and landing flying car |
| CN201395024Y (en) * | 2008-06-26 | 2010-02-03 | 张庆柳 | Vertically-takeoff and landing hovercar |
| CN201506223U (en) * | 2009-08-04 | 2010-06-16 | 张庆柳 | Vertical takeoff and landing aerocar |
-
2009
- 2009-08-04 CN CN2009100947941A patent/CN101987565A/en active Pending
-
2010
- 2010-08-04 WO PCT/CN2010/001190 patent/WO2011015038A1/en active Application Filing
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103770589A (en) * | 2014-02-28 | 2014-05-07 | 武汉蓝天翔航空科技有限公司 | Flying car |
| CN105196815A (en) * | 2015-10-27 | 2015-12-30 | 陈晓春 | Synchronous turnover mechanism applied to aerocar |
| CN108032692A (en) * | 2017-11-30 | 2018-05-15 | 吉林大学 | Novel screw type offroad vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2011015038A1 (en) | 2011-02-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101612870B (en) | Vertical take-off and landing flying car | |
| CN103596842B (en) | The driver element of aircraft running gear wheel | |
| RU2686803C2 (en) | Dirension control system and method for hybrid vehicle of air and ground transport | |
| CN102363445B (en) | Tilting dynamic vertical take-off and landing land-air amphibious aircraft | |
| CN106976552A (en) | Tilting rotor wing unmanned aerial vehicle | |
| CN204660020U (en) | One is distributed independently controls multi-rotor aerocraft | |
| CN107107690B (en) | Central wing plate and its control method for flight formula delivery vehicle | |
| CN101987565A (en) | Vertical takeoff and landing flying car | |
| CN109017182A (en) | A kind of folding hovercar of VTOL wing | |
| CN106427438B (en) | A kind of retractable land and air double-used driving of rotor and its control method | |
| WO2009149592A1 (en) | Vertical takeoff and landing airplane | |
| CN209257804U (en) | A kind of folding hovercar of VTOL wing | |
| CN211195749U (en) | Tilt shaftless duct rotor aerocar | |
| CN112238719A (en) | Driving device of aerocar | |
| CN201506223U (en) | Vertical takeoff and landing aerocar | |
| CN110654190A (en) | Tilting shaftless ducted rotor aerocar and working method thereof | |
| CN105966633A (en) | Transmission system for combined aircraft | |
| CN110167770A (en) | Acceleration control for convertible empty use-terrestrial vehicle | |
| US10239608B2 (en) | Aircraft landing gear | |
| CN201395024Y (en) | Vertically-takeoff and landing hovercar | |
| CN107139667A (en) | Convertible propeller set | |
| CN207826543U (en) | Tilting rotor wing unmanned aerial vehicle | |
| CN204452933U (en) | The many rotor wing unmanned aerial vehicles of belt-driving | |
| CN102632993B (en) | Series-parallel tilting drive mechanism of tilt rotor aircraft | |
| CN210942237U (en) | Control system and three rotor unmanned aerial vehicle of oil-drive that ball cage universal joint constitutes |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20110323 |