WO2016066848A1 - Module d'entraînement destiné à un véhicule automobile et véhicule automobile comprenant un module d'entraînement de ce type - Google Patents

Module d'entraînement destiné à un véhicule automobile et véhicule automobile comprenant un module d'entraînement de ce type Download PDF

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Publication number
WO2016066848A1
WO2016066848A1 PCT/EP2015/075359 EP2015075359W WO2016066848A1 WO 2016066848 A1 WO2016066848 A1 WO 2016066848A1 EP 2015075359 W EP2015075359 W EP 2015075359W WO 2016066848 A1 WO2016066848 A1 WO 2016066848A1
Authority
WO
WIPO (PCT)
Prior art keywords
impellers
impeller
vehicle
drive
rotor blades
Prior art date
Application number
PCT/EP2015/075359
Other languages
German (de)
English (en)
Inventor
Johann SCHWÖLLER
Original Assignee
Schwöller Johann
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Schwöller Johann filed Critical Schwöller Johann
Publication of WO2016066848A1 publication Critical patent/WO2016066848A1/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • 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

Definitions

  • the impellers may have stator arms, which are arranged underneath the rotor blades and profiled.
  • the number of stator rows preferably exceeds the number of rotor blades. However, fewer stator arms may be provided as rotor blades.
  • the number of stator arms thus preferably differs from the number of rotor blades of the impeller to prevent swinging.
  • the stator arms may be profiled so as to substantially completely balance the swirl generated by the rotor blades
  • the impeller may have a rotor with a plurality of rotor blades, wherein the arrival angle of the rotor blades during operation may be variable. In this way it is possible to arbitrarily control the buoyancy and / or propulsion of a single impeller.
  • the vehicle may comprise an internal combustion engine, a generator and a buffer battery or a supercapacitor, wherein in the hubs of the impeller electric motors are arranged, which are supplied via the Pufferakku or the supercapacitor with power.
  • the electric motors can deliver much more power for a short time than can be generated permanently by the generator or the generators or even provide the necessary energy for a safe landing in case of failure of the internal combustion engine.
  • It may be provided a control device by means of which the impeller can be operated with different rotational speeds and / or different inclination angles and / or different angles of attack of the rotor blades.
  • Figure 2 shows the vehicle of Figure 1 in a perspective view, with two
  • Figure 5 shows the vehicle of Figure 1 in a perspective view, wherein four
  • FIG. 7 shows a further embodiment of the vehicle according to the invention
  • the pivotable impellers 8, 9 are pivotable outwardly to the left and right with respect to the vehicle longitudinal axis 10 laterally next to the chassis 2 by means of the pivoting device 11, that the pivotable impeller 8, 9 adjacent or spaced from the stationary Impeller 7 are arranged ( Figure 6).
  • the fixed impeller 7 are in flight by means of a hydraulic lifting device (not shown) or with spindle devices or the like. a piece raised. The method for transferring the impellers 7, 8 and 9 from a driving operation to a flying operation will be described later in detail.
  • the pivoting device 1 1 may be an electrically, hydraulically, mechanically or pneumatically actuated lever arm.
  • hub motors For driving the wheels hub motors are provided, either two wheel hub motors are provided on the rear wheels and / or the front wheels or, alternatively, four wheel hub motors on all four wheels.
  • stator arms which are already arranged concentrically circumferentially.
  • the stator arms could also be designed such that they completely cover and protect the impellers when driving.
  • the vehicle may have lowerable doors. This allows easy entry and exit while maintaining a higher and larger lateral chassis area. As a result, the vehicle can be easily and stably built at the same time, since the outer contour does not have to be interrupted by large doors.
  • the doors can be locked by means of a locking device (not shown). By means of the locking device, a rigid composite between the doors and the body is formed.
  • the vehicle doors can also be designed as so-called gullwing doors. Due to the special movement upwards or diagonally upwards a collision of the doors with the impellers is avoided, if they are currently in the extended position.
  • the vehicle may have unilateral control (steering wheel, pedal train, etc.).
  • the vehicle has a two-sided control. This has the advantage if the pilot becomes ill, that a second person can take over the control. Even for a training operation such an arrangement makes sense.
  • Such a rotational movement about the vertical axis can also be achieved if the left-handed rotors turn faster and the right-handed rotors slower. Due to the larger counter torque of the left-handed rotors, the vehicle turns to the right.
  • Such a transmission has a multiple gear output and the individual outputs are preferably individually steplessly adjustable.
  • toothed belt or cardan shafts are provided for transmitting the force. These are less lossy than. the power transmission via generators, motor controllers and motors. However, this requires a much higher mechanical complexity.
  • the pivoting means may according to these two embodiments have a corresponding mechanism of shaft and bevel gears for transmitting the force.
  • the redundancy is favored by the provision of an electric motor per drive.
  • the buffer battery or the supercapacitor can be chosen so large that even if the internal combustion engine still enough energy is available to land the vehicle safely.
  • the embodiments explained above have an internal combustion engine.
  • the vehicle exclusively with electric motors, i. without forming an internal combustion engine.
  • the weight saved by eliminating the internal combustion engine and the fuel is preferably used for a large battery and / or a large supercapacitor.
  • the internal combustion engine may be directly connected to the impellers via a mechanical drive train comprising a propeller shaft and / or a toothed belt with or without gears.
  • one of the two drive devices comprises only one impeller and the other drive device comprises two impellers pivotable by means of a pivoting device.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)

Abstract

L'invention concerne un module d'entraînement destiné à un véhicule automobile. Le module d'entraînement comprend deux dispositifs d'entraînement présentant au total au moins trois rotors pourvus de pales, au moins deux des rotors étant accouplés à un dispositif de pivotement, de telle manière qu'au moins deux des rotors, dans une position de départ, peuvent se chevaucher au moins en partie et, dans une position de fonctionnement, un de ces rotors peut être agencé sensiblement à côté d'un autre rotor, les dispositifs de pivotement comprenant deux axes de pivotement différents.
PCT/EP2015/075359 2014-10-31 2015-10-30 Module d'entraînement destiné à un véhicule automobile et véhicule automobile comprenant un module d'entraînement de ce type WO2016066848A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102014115926.8 2014-10-31
DE102014115926.8A DE102014115926A1 (de) 2014-10-31 2014-10-31 Antriebsmodul für ein Kraftfahrzeug und Kraftfahrzeug mit einem solchen Antriebsmodul

Publications (1)

Publication Number Publication Date
WO2016066848A1 true WO2016066848A1 (fr) 2016-05-06

Family

ID=54366225

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2015/075359 WO2016066848A1 (fr) 2014-10-31 2015-10-30 Module d'entraînement destiné à un véhicule automobile et véhicule automobile comprenant un module d'entraînement de ce type

Country Status (2)

Country Link
DE (1) DE102014115926A1 (fr)
WO (1) WO2016066848A1 (fr)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107053983A (zh) * 2017-05-11 2017-08-18 湖南顶立科技有限公司 一种飞行汽车
CN107116981A (zh) * 2017-05-11 2017-09-01 湖南顶立科技有限公司 一种四翼飞行汽车
WO2018000096A1 (fr) * 2016-06-29 2018-01-04 William Bailie Véhicule aérien à décollage et atterrissage courts
CN108357313A (zh) * 2017-01-26 2018-08-03 汪俊霞 新型飞行汽车
CN108528161A (zh) * 2018-06-15 2018-09-14 中宇航通（北京）科技有限公司 飞行汽车重心自动调节系统及方法和飞行汽车
US20180362160A1 (en) * 2017-06-14 2018-12-20 Bell Helicopter Textron Inc. Personal air vehicle with ducted fans
DE202019000841U1 (de) 2019-02-20 2019-04-05 Rainer Epperlein Flugauto
US20190263206A1 (en) * 2018-02-28 2019-08-29 Stmicroelectronics S.R.L. Multi-environment flexible vehicle
DE102019118023B3 (de) 2019-07-04 2020-07-23 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102019112132A1 (de) * 2019-05-09 2020-11-12 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
CN112622547A (zh) * 2020-12-24 2021-04-09 中国直升机设计研究所 一种旋翼车轮及飞行汽车
WO2021233573A1 (fr) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aéronef ayant une hélice carénée dans la surface portante
DE102020113491A1 (de) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
WO2021233572A1 (fr) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aéronef
DE102020113488A1 (de) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
JP7004369B1 (ja) 2021-11-08 2022-01-21 株式会社石川エナジーリサーチ 飛行装置
US11634233B2 (en) * 2020-06-22 2023-04-25 Textron Innovations Inc. Distributed battery bank for ducted-rotor aircraft

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Publication number Priority date Publication date Assignee Title
CN110662662A (zh) 2017-04-27 2020-01-07 弗莱昂空中系统有限公司 整合式陆空运输系统
AT520145A1 (de) * 2017-06-22 2019-01-15 Werner Dipl Ing Holzer Ausfahrbarer propellerschutzrahmen mit integrierten angetriebenen probellern
AT520144A1 (de) * 2017-06-22 2019-01-15 Werner Dipl Ing Holzer Schwenkbarer propellerschutzrahmen mit integrierten elektrisch angetriebenen propellern
CN107984992A (zh) * 2017-11-28 2018-05-04 北京航空航天大学 一种可垂直起降的陆空两用运载器
CN108146169B (zh) * 2017-11-28 2021-06-29 北京航空航天大学 一种机翼后折式陆空两用运载器
DE102019101361A1 (de) * 2019-01-21 2020-07-23 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Mantelpropeller und Luftfahrzeug
CN110282117A (zh) * 2019-07-10 2019-09-27 黄山鲸鲨飞行器科技有限公司 一种具备机翼折叠收纳功能的城市垂直起降飞机

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DE1020855B (de) * 1954-11-25 1957-12-12 Keskusosuusliike Hankkija R L Zur Herstellung von Emmentaler Kaese bestimmte Ablaufwanne
DE2845260A1 (de) * 1978-10-18 1980-05-14 Sach Lothar Bodenluftfahrzeug, ein fahrzeug zum betrieb auf dem boden und in der luft
DE4203286A1 (de) * 1992-02-03 1993-08-05 Hektor Steinhilber Flugauto
US6138943A (en) * 1998-12-11 2000-10-31 Huang; Yung-Chi Foldable ascending/descending wing stand for flying apparatus
DE10214535A1 (de) * 2001-12-07 2003-06-26 Oleg Tchebunin Antriebsanlage für Mini-Flugapparat mit Senkrecht-Start-Landung und entsprechende Zusammenstellung verschiedener Arten des Personal-Flugautos
US6745977B1 (en) * 2003-08-21 2004-06-08 Larry D. Long Flying car
WO2008147484A2 (fr) * 2007-02-16 2008-12-04 Donald Orval Shaw Véhicule volant modulaire
GB2483165A (en) * 2010-08-27 2012-02-29 Rolls Royce Corp Roadable aircraft with extendable wings and thrust vectoring
DE202012009714U1 (de) * 2012-10-09 2013-01-14 Wolff Wolfsthal Rando "Flugauto"
DE102012010937A1 (de) * 2012-06-01 2013-12-05 Emt Ingenieurgesellschaft Dipl.-Ing. Hartmut Euer Mbh Fluggerät
CA2840823A1 (fr) * 2014-01-28 2015-07-28 Rajesh Gaonjur Aeronef a decollage et atterrissage verticaux pouvant circuler sur la route

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US7032861B2 (en) * 2002-01-07 2006-04-25 Sanders Jr John K Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors
US8646720B2 (en) * 2010-05-10 2014-02-11 Donald Orval Shaw Modular flight vehicle with wings
BR112013007255B1 (pt) * 2010-11-12 2021-01-19 Sky Sapience sistema

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DE1020855B (de) * 1954-11-25 1957-12-12 Keskusosuusliike Hankkija R L Zur Herstellung von Emmentaler Kaese bestimmte Ablaufwanne
DE2845260A1 (de) * 1978-10-18 1980-05-14 Sach Lothar Bodenluftfahrzeug, ein fahrzeug zum betrieb auf dem boden und in der luft
DE4203286A1 (de) * 1992-02-03 1993-08-05 Hektor Steinhilber Flugauto
US6138943A (en) * 1998-12-11 2000-10-31 Huang; Yung-Chi Foldable ascending/descending wing stand for flying apparatus
DE10214535A1 (de) * 2001-12-07 2003-06-26 Oleg Tchebunin Antriebsanlage für Mini-Flugapparat mit Senkrecht-Start-Landung und entsprechende Zusammenstellung verschiedener Arten des Personal-Flugautos
US6745977B1 (en) * 2003-08-21 2004-06-08 Larry D. Long Flying car
WO2008147484A2 (fr) * 2007-02-16 2008-12-04 Donald Orval Shaw Véhicule volant modulaire
GB2483165A (en) * 2010-08-27 2012-02-29 Rolls Royce Corp Roadable aircraft with extendable wings and thrust vectoring
DE102012010937A1 (de) * 2012-06-01 2013-12-05 Emt Ingenieurgesellschaft Dipl.-Ing. Hartmut Euer Mbh Fluggerät
DE202012009714U1 (de) * 2012-10-09 2013-01-14 Wolff Wolfsthal Rando "Flugauto"
CA2840823A1 (fr) * 2014-01-28 2015-07-28 Rajesh Gaonjur Aeronef a decollage et atterrissage verticaux pouvant circuler sur la route

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018000096A1 (fr) * 2016-06-29 2018-01-04 William Bailie Véhicule aérien à décollage et atterrissage courts
CN108357313A (zh) * 2017-01-26 2018-08-03 汪俊霞 新型飞行汽车
CN108357313B (zh) * 2017-01-26 2022-06-07 汪俊霞 飞行汽车
CN107053983A (zh) * 2017-05-11 2017-08-18 湖南顶立科技有限公司 一种飞行汽车
CN107116981A (zh) * 2017-05-11 2017-09-01 湖南顶立科技有限公司 一种四翼飞行汽车
US10730622B2 (en) * 2017-06-14 2020-08-04 Bell Helicopter Textron Inc. Personal air vehicle with ducted fans
US20180362160A1 (en) * 2017-06-14 2018-12-20 Bell Helicopter Textron Inc. Personal air vehicle with ducted fans
US20190263206A1 (en) * 2018-02-28 2019-08-29 Stmicroelectronics S.R.L. Multi-environment flexible vehicle
US11660920B2 (en) * 2018-02-28 2023-05-30 Stmicroelectronics S.R.L. Multi-environment flexible vehicle
CN108528161A (zh) * 2018-06-15 2018-09-14 中宇航通（北京）科技有限公司 飞行汽车重心自动调节系统及方法和飞行汽车
DE202019000841U1 (de) 2019-02-20 2019-04-05 Rainer Epperlein Flugauto
DE102020001048B4 (de) 2019-02-20 2022-06-23 Rainer Epperlein Die Erfindung ist ein straßenfahrtaugliches sowie autonom voll flugfähiges, vorwiegend - senkrechtstartendes und -landendes, brennstoffzellen- und batteriebetriebenes, zwei- bis viersitziges Flugauto, gekennzeichnet durch aus- und einschwenkbare Propeller mit e-Motoren an zwei bis vier Auslegem oder an den zwei schenkbaren Tragflächenhälften, die im Straßenfahrmodus in Aufnahmeschächte eingefahren werden.
DE102020001048A1 (de) * 2019-02-20 2020-09-03 Rainer Epperlein Die Erfindung ist ein straßenfahrtaugliches sowie autonom voll flugfähiges, vorwiegend - senkrechtstartendes und -landendes, brennstoffzellen- und batteriebetriebenes, zwei- bis viersitziges Flugauto, gekennzeichnet durch aus- und einschwenkbare Propeller mit e-Motoren an zwei bis vier Auslegem oder an den zwei schenkbaren Tragflächenhälften, die im Straßenfahrmodus in Aufnahmeschächte eingefahren werden.
DE102020001048B8 (de) 2019-02-20 2022-09-15 Rainer Epperlein Straßenfahrtaugliches sowie autonom voll flugfähiges Flugauto
DE102019112132B4 (de) 2019-05-09 2024-05-23 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
US11873084B2 (en) 2019-05-09 2024-01-16 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aircraft with ducted fan and movable louvers over the ducted fan
DE102019112132A1 (de) * 2019-05-09 2020-11-12 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102019118023B3 (de) 2019-07-04 2020-07-23 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102020113488A1 (de) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102020113490B4 (de) 2020-05-19 2022-08-11 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
WO2021233573A1 (fr) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aéronef ayant une hélice carénée dans la surface portante
DE102020113488B4 (de) 2020-05-19 2022-03-31 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
WO2021233574A1 (fr) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aéronef
DE102020113489A1 (de) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102020113489B4 (de) 2020-05-19 2022-08-11 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
DE102020113490A1 (de) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
WO2021233572A1 (fr) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aéronef
DE102020113491A1 (de) 2020-05-19 2021-11-25 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Luftfahrzeug
US11634233B2 (en) * 2020-06-22 2023-04-25 Textron Innovations Inc. Distributed battery bank for ducted-rotor aircraft
CN112622547A (zh) * 2020-12-24 2021-04-09 中国直升机设计研究所 一种旋翼车轮及飞行汽车
JP2023069872A (ja) * 2021-11-08 2023-05-18 株式会社石川エナジーリサーチ 飛行装置
JP7004369B1 (ja) 2021-11-08 2022-01-21 株式会社石川エナジーリサーチ 飛行装置

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