IL43401A - Aircraft system lift ejector - Google Patents

Aircraft system lift ejector

Info

Publication number
IL43401A
IL43401A IL43401A IL4340173A IL43401A IL 43401 A IL43401 A IL 43401A IL 43401 A IL43401 A IL 43401A IL 4340173 A IL4340173 A IL 4340173A IL 43401 A IL43401 A IL 43401A
Authority
IL
Israel
Prior art keywords
flow fluid
ejector
fluid
section
inlet
Prior art date
Application number
IL43401A
Other languages
English (en)
Other versions
IL43401A0 (en
Original Assignee
Rockwell International 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 Rockwell International Corp filed Critical Rockwell International Corp
Publication of IL43401A0 publication Critical patent/IL43401A0/xx
Publication of IL43401A publication Critical patent/IL43401A/en

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
    • B64C29/0041—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 jet motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Control Of Turbines (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
IL43401A 1972-11-30 1973-10-08 Aircraft system lift ejector IL43401A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00311011A US3819134A (en) 1972-11-30 1972-11-30 Aircraft system lift ejector

Publications (2)

Publication Number Publication Date
IL43401A0 IL43401A0 (en) 1974-03-14
IL43401A true IL43401A (en) 1976-04-30

Family

ID=23204996

Family Applications (1)

Application Number Title Priority Date Filing Date
IL43401A IL43401A (en) 1972-11-30 1973-10-08 Aircraft system lift ejector

Country Status (12)

Country Link
US (1) US3819134A (de)
JP (1) JPS4983199A (de)
AU (1) AU469746B2 (de)
BR (1) BR7309378D0 (de)
CA (1) CA967377A (de)
DE (2) DE2366007A1 (de)
ES (1) ES421013A1 (de)
FR (1) FR2208814B1 (de)
GB (2) GB1448017A (de)
IL (1) IL43401A (de)
IT (1) IT1000092B (de)
SE (1) SE394637B (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3941335A (en) * 1975-06-19 1976-03-02 The United States Of America As Represented By The Secretary Of The Air Force Automatic boundary layer control in an ejector wing aircraft
US4274812A (en) 1978-12-01 1981-06-23 Elvidge John H K Jet pump
BR8807113A (pt) * 1987-06-25 1989-10-17 Mark T Willis Aerofolio intensificado por difusor
US5016837A (en) * 1987-06-25 1991-05-21 Venturi Applications, Inc. Venturi enhanced airfoil
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
WO1991009776A1 (en) * 1989-12-29 1991-07-11 Venturi Applications, Inc. Venturi-enhanced airfoil
US20060225404A1 (en) * 2001-09-05 2006-10-12 Dev Sudarshan P Vertical or short take off and landing vehicle
DE10313729B4 (de) * 2003-03-27 2007-11-29 Airbus Deutschland Gmbh Luftauslaßventil für ein Flugzeug
US20060102801A1 (en) * 2004-11-01 2006-05-18 The Boeing Company High-lift distributed active flow control system and method
US7685804B2 (en) * 2006-09-08 2010-03-30 General Electric Company Device for enhancing efficiency of an energy extraction system
US20100019079A1 (en) * 2007-06-20 2010-01-28 General Electric Company Thrust generator for a rotary wing aircraft
US20110215204A1 (en) * 2007-06-20 2011-09-08 General Electric Company System and method for generating thrust
IL257811B (en) 2015-09-02 2022-08-01 Jetoptera Inc Pleoidal propulsion system
US11965456B2 (en) * 2015-09-02 2024-04-23 Jetoptera, Inc. Fluidic turbo heater system
CN111655580B (zh) * 2017-06-16 2024-01-16 杰拓普特拉股份有限公司 小翼喷射器构造
US10822101B2 (en) * 2017-07-21 2020-11-03 General Electric Company Vertical takeoff and landing aircraft having a forward thrust propulsor
US11352132B2 (en) 2018-07-23 2022-06-07 General Electric Company Lift fan with diffuser duct
EP3674559B1 (de) * 2018-12-24 2021-06-02 LEONARDO S.p.A. Strahllüfter und fahrzeug mit einem solchen lüfter
US12024280B2 (en) 2019-09-03 2024-07-02 Bae Systems Plc Vehicle control
WO2021044141A1 (en) 2019-09-03 2021-03-11 Bae Systems Plc Fluidic control
GB2586807B (en) * 2019-09-03 2023-07-19 Bae Systems Plc Vehicle control
CN113998106B (zh) * 2021-10-27 2023-12-08 南京壮大智能科技研究院有限公司 无人机水上迫降方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL110393C (de) * 1955-11-29 1965-01-15 Bertin & Cie
GB871470A (en) * 1956-09-20 1961-06-28 Fairey Co Ltd Improvements relating to aircraft incorporating vertical thrust generators
US3045947A (en) * 1959-04-24 1962-07-24 Bertin & Cie Ejectors, particularly for producing lift in aircraft
FR1267920A (fr) * 1960-06-15 1961-07-28 Snecma Dispositif de sustentation pour aérodynes, et plus particulièrement pour aérodynes à décollage vertical sans changement d'assiette
US3664611A (en) * 1969-12-17 1972-05-23 Flight Dynamics Res Aerodynamic vehicle

Also Published As

Publication number Publication date
BR7309378D0 (pt) 1974-08-29
IT1000092B (it) 1976-03-30
AU6106273A (en) 1975-05-15
DE2359518A1 (de) 1974-06-06
CA967377A (en) 1975-05-13
US3819134A (en) 1974-06-25
DE2359518B2 (de) 1977-12-08
IL43401A0 (en) 1974-03-14
FR2208814B1 (de) 1976-05-14
FR2208814A1 (de) 1974-06-28
GB1448017A (en) 1976-09-02
GB1448018A (en) 1976-09-02
AU469746B2 (en) 1976-02-26
SE394637B (sv) 1977-07-04
DE2359518C3 (de) 1978-07-20
JPS4983199A (de) 1974-08-09
ES421013A1 (es) 1976-05-01
DE2366007A1 (de) 1977-08-25

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