DE2366007A1 - Ausbildung und anordnung der coanda-ejektoren - Google Patents

Ausbildung und anordnung der coanda-ejektoren

Info

Publication number
DE2366007A1
DE2366007A1 DE19732366007 DE2366007A DE2366007A1 DE 2366007 A1 DE2366007 A1 DE 2366007A1 DE 19732366007 DE19732366007 DE 19732366007 DE 2366007 A DE2366007 A DE 2366007A DE 2366007 A1 DE2366007 A1 DE 2366007A1
Authority
DE
Germany
Prior art keywords
training
arrangement
coanda
ejectors
coanda ejectors
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
Application number
DE19732366007
Other languages
English (en)
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.)
Boeing North American Inc
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 DE2366007A1 publication Critical patent/DE2366007A1/de
Pending 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
    • B64C29/0041—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)
DE19732366007 1972-11-30 1973-11-29 Ausbildung und anordnung der coanda-ejektoren Pending DE2366007A1 (de)

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 (1)

Publication Number Publication Date
DE2366007A1 true DE2366007A1 (de) 1977-08-25

Family

ID=23204996

Family Applications (2)

Application Number Title Priority Date Filing Date
DE2359518A Expired DE2359518C3 (de) 1972-11-30 1973-11-29 Hubdüseneinrichtung für ein Flugzeug
DE19732366007 Pending DE2366007A1 (de) 1972-11-30 1973-11-29 Ausbildung und anordnung der coanda-ejektoren

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE2359518A Expired DE2359518C3 (de) 1972-11-30 1973-11-29 Hubdüseneinrichtung für ein Flugzeug

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) DE2359518C3 (de)
ES (1) ES421013A1 (de)
FR (1) FR2208814B1 (de)
GB (2) GB1448018A (de)
IL (1) IL43401A (de)
IT (1) IT1000092B (de)
SE (1) SE394637B (de)

Families Citing this family (20)

* 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
JPH02501213A (ja) * 1987-06-25 1990-04-26 ウィリス・マーク・テー ベンチュリ強化エーロフォイル
US5016837A (en) * 1987-06-25 1991-05-21 Venturi Applications, Inc. Venturi enhanced airfoil
US5076512A (en) * 1989-02-08 1991-12-31 Boeing Canada Ltd. Ventral segmented nozzles for promoting rapid temperature and pressure decay
US5062588A (en) * 1989-02-08 1991-11-05 Boeing Of Canada Ltd. Segmented rotatable nozzles
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
AU2016338383A1 (en) 2015-09-02 2018-03-22 Jetoptera, Inc. Fluidic propulsive system
CA3067346A1 (en) * 2017-06-16 2018-12-20 Jetoptera, Inc. Winglet ejector configurations
US10737797B2 (en) * 2017-07-21 2020-08-11 General Electric Company Vertical takeoff and landing aircraft
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
GB2586807B (en) * 2019-09-03 2023-07-19 Bae Systems Plc Vehicle control
US12024280B2 (en) 2019-09-03 2024-07-02 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
DE2359518A1 (de) 1974-06-06
GB1448018A (en) 1976-09-02
DE2359518B2 (de) 1977-12-08
DE2359518C3 (de) 1978-07-20
AU469746B2 (en) 1976-02-26
US3819134A (en) 1974-06-25
IL43401A (en) 1976-04-30
SE394637B (sv) 1977-07-04
FR2208814B1 (de) 1976-05-14
GB1448017A (en) 1976-09-02
ES421013A1 (es) 1976-05-01
BR7309378D0 (pt) 1974-08-29
JPS4983199A (de) 1974-08-09
FR2208814A1 (de) 1974-06-28
IL43401A0 (en) 1974-03-14
AU6106273A (en) 1975-05-15
CA967377A (en) 1975-05-13
IT1000092B (it) 1976-03-30

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