DE69126132T2 - Antriebssystem für kurz- und senkrecht-start- und -landeflugzeug - Google Patents

Antriebssystem für kurz- und senkrecht-start- und -landeflugzeug

Info

Publication number
DE69126132T2
DE69126132T2 DE69126132T DE69126132T DE69126132T2 DE 69126132 T2 DE69126132 T2 DE 69126132T2 DE 69126132 T DE69126132 T DE 69126132T DE 69126132 T DE69126132 T DE 69126132T DE 69126132 T2 DE69126132 T2 DE 69126132T2
Authority
DE
Germany
Prior art keywords
short
drive system
vertical starting
landing planes
landing
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.)
Expired - Fee Related
Application number
DE69126132T
Other languages
English (en)
Other versions
DE69126132D1 (de
Inventor
Paul Bevilaqua
Paul Shumpert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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 Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of DE69126132D1 publication Critical patent/DE69126132D1/de
Application granted granted Critical
Publication of DE69126132T2 publication Critical patent/DE69126132T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B64C29/0025—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 fixed relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
DE69126132T 1990-05-07 1991-02-22 Antriebssystem für kurz- und senkrecht-start- und -landeflugzeug Expired - Fee Related DE69126132T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/521,211 US5209428A (en) 1990-05-07 1990-05-07 Propulsion system for a vertical and short takeoff and landing aircraft
PCT/US1991/001145 WO1991017083A1 (en) 1990-05-07 1991-02-22 Propulsion system for a vertical and short takeoff and landing aircraft

Publications (2)

Publication Number Publication Date
DE69126132D1 DE69126132D1 (de) 1997-06-19
DE69126132T2 true DE69126132T2 (de) 1997-08-28

Family

ID=24075841

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69126132T Expired - Fee Related DE69126132T2 (de) 1990-05-07 1991-02-22 Antriebssystem für kurz- und senkrecht-start- und -landeflugzeug

Country Status (7)

Country Link
US (1) US5209428A (de)
EP (1) EP0527956B1 (de)
JP (1) JP2647258B2 (de)
DE (1) DE69126132T2 (de)
IL (1) IL97434A (de)
RU (1) RU2108941C1 (de)
WO (1) WO1991017083A1 (de)

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US6918244B2 (en) * 2001-08-17 2005-07-19 John Eugene Dickau Vertical takeoff and landing aircraft propulsion systems
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US7925392B2 (en) 2002-04-23 2011-04-12 Lord Corporation Aircraft vehicular propulsion system monitoring device and method
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US6896221B1 (en) 2003-04-16 2005-05-24 Einar Einarsson Vertical takeoff and landing aircraft
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US8833692B2 (en) * 2006-11-27 2014-09-16 Urban Aeronautics Ltd. Wall effects on VTOL vehicles
US20100076625A1 (en) * 2006-11-30 2010-03-25 Raphael Yoeli Flight control cockpit modes in ducted fan vtol vehicles
EP2152576A2 (de) * 2007-05-02 2010-02-17 Urban Aeronautics Ltd. Steuerung von strömen und kräften in senkrechtstartfahrzeugen
WO2009077968A2 (en) * 2007-12-14 2009-06-25 Urban Aeronautics Ltd. Redundancies and flows in vehicles
WO2010026517A2 (en) * 2008-09-02 2010-03-11 Urban Aeronautics Ltd. Vtol vehicle with coaxially tilted or tiltable rotors
FR2935954B1 (fr) * 2008-09-18 2011-06-03 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs traversant le fuselage et reliee a celui-ci par au moins une bielle.
FR2935955B1 (fr) * 2008-09-18 2010-10-15 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression.
FR2938504B1 (fr) * 2008-11-14 2010-12-10 Snecma Entree d'air d'un moteur d'avion a helices propulsives non carenees
US20100193643A1 (en) * 2008-12-31 2010-08-05 Sidelkovskiy Dmitriy B Lift fan system
US20100170221A1 (en) * 2009-01-08 2010-07-08 Toyota Jidosha Kabushiki Kaisha Turbo fan engine
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US8572986B2 (en) * 2009-07-27 2013-11-05 United Technologies Corporation Retainer for suspended thermal protection elements in a gas turbine engine
US8876038B2 (en) 2010-10-05 2014-11-04 Urban Aeronautics Ltd. Ducted fan for VTOL vehicles with system and method to reduce roll moments
CN102336269B (zh) * 2011-08-10 2015-04-29 彭红云 全推力垂直起降矢量战斗机
US8708274B2 (en) 2011-09-09 2014-04-29 United Technologies Corporation Transverse mounted gas turbine engine
BR102012032396B1 (pt) * 2012-01-17 2021-01-05 United Technologies Corporation conjunto de mastro de motor, e, sistema de motor de turbina a gás
CN103318411B (zh) * 2012-03-19 2016-04-13 陈永春 固定翼垂直起降飞机
US8733800B1 (en) 2012-11-20 2014-05-27 United Technologies Corporation Tube having an integral, spring-loaded, spherical joint
US10518595B2 (en) 2013-03-15 2019-12-31 Terrafugia, Inc. Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities
RU2531792C1 (ru) * 2013-08-07 2014-10-27 Валерий Туркубеевич Пчентлешев Самолет короткого и/или вертикального взлета и посадки
EP3080425A4 (de) 2013-12-13 2017-09-20 United Technologies Corporation Quermontiertes nutzturbinenantriebssystem
CN103963959B (zh) * 2014-05-12 2015-12-30 北京理工大学 基于变质心技术的可悬停式折叠机翼升力体飞行器
US10766615B1 (en) * 2015-03-10 2020-09-08 Lindsay O'Brien Quarrie Hover airlift logistics operations guided expeditionary autonomous scalable and modular VTOL platform
CN108137149B (zh) 2015-09-02 2021-07-06 杰托普特拉股份有限公司 喷射器和翼型构型
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US10926874B2 (en) * 2016-01-15 2021-02-23 Aurora Flight Sciences Corporation Hybrid propulsion vertical take-off and landing aircraft
EP3442815A1 (de) 2016-04-15 2019-02-20 Terrafugia, Inc. Elektronische gangschaltanordnung für ein zweimodiges flug- und fahrzeug
CA2934346A1 (en) * 2016-06-29 2017-12-29 William C. Bailie Short take off and landing arial vehicle
JP7155174B2 (ja) 2017-06-27 2022-10-18 ジェトプテラ、インコーポレイテッド 航空機の垂直離着陸システムの構成
US10822101B2 (en) * 2017-07-21 2020-11-03 General Electric Company Vertical takeoff and landing aircraft having a forward thrust propulsor
FR3077804B1 (fr) * 2018-02-09 2022-03-18 Safran Propulsion hybride pour un aeronef
RU2682054C1 (ru) * 2018-02-26 2019-03-14 Дмитрий Сергеевич Дуров Сверхзвуковой малозаметный самолет вертикального взлета и посадки
RU2686561C1 (ru) * 2018-03-27 2019-04-29 Дмитрий Сергеевич Дуров Беспилотный малозаметный самолет вертикального взлета и посадки и способ его применения при воздушном базировании
CN112533826A (zh) * 2018-05-17 2021-03-19 杰托普特拉股份有限公司 组合式压缩流体喷射器和螺旋桨推进系统
RU2693427C1 (ru) * 2018-09-12 2019-07-02 Дмитрий Сергеевич Дуров Малозаметный беспилотный самолет вертикального взлета и посадки
RU2717606C1 (ru) * 2018-11-22 2020-03-24 Аслан Солтамбекович Тедтоев Силовая установка летательного аппарата вертикального взлета и посадки, а также летательный аппарат вертикального взлета и посадки, содержащий указанную силовую установку
RU2717409C1 (ru) * 2018-11-30 2020-03-23 Аслан Солтамбекович Тедтоев Вертикально ориентированный турбореактивный двигатель силовой установки летательного аппарата вертикального взлета и посадки, силовая установка летательного аппарата вертикального взлета и посадки, а также летательный аппарат вертикального взлета и посадки
RU2698497C1 (ru) * 2018-12-10 2019-08-28 Николай Борисович Болотин Летательный аппарат вертикального взлета и посадки
DE102019218100A1 (de) * 2019-11-22 2021-05-27 Rolls-Royce Deutschland Ltd & Co Kg Wellenmechanisches Antriebssytem und -verfahren für ein Luftfahrzeug
WO2021152482A1 (en) 2020-01-27 2021-08-05 Mts Sensor Technologie Gmbh & Co. Kg Magnetostrictive position measurement using frequency domain analysis
US11661183B2 (en) 2020-03-16 2023-05-30 D. Anthony Windisch Small light vertical take-off and landing capable delta wing aircraft
GB2599686A (en) 2020-10-09 2022-04-13 Rolls Royce Plc An improved turbofan gas turbine engine
US11859542B2 (en) * 2021-12-20 2024-01-02 Rolls-Royce North American Technologies, Inc. Dual power lift system
EP4282763A1 (de) 2022-05-26 2023-11-29 RTX Corporation Selektive leistungsverteilung für ein flugzeugantriebssystem
EP4283109A1 (de) * 2022-05-26 2023-11-29 RTX Corporation Schubvektorisierungsabgasdüse für ein flugzeugantriebssystem
US11939926B2 (en) 2022-08-16 2024-03-26 Rtx Corporation Selective power distribution for an aircraft propulsion system
US11952949B2 (en) 2022-09-06 2024-04-09 Rtx Corporation Selective power distribution for an aircraft propulsion system
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Also Published As

Publication number Publication date
EP0527956A1 (de) 1993-02-24
IL97434A (en) 1994-07-31
DE69126132D1 (de) 1997-06-19
US5209428A (en) 1993-05-11
IL97434A0 (en) 1992-06-21
JP2647258B2 (ja) 1997-08-27
EP0527956A4 (en) 1994-10-19
JPH05505992A (ja) 1993-09-02
WO1991017083A1 (en) 1991-11-14
RU2108941C1 (ru) 1998-04-20
EP0527956B1 (de) 1997-05-14

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee