IT1000092B - Perfezionamento negli eiettori per incremento di potenza per sistemi aeromobili - Google Patents

Perfezionamento negli eiettori per incremento di potenza per sistemi aeromobili

Info

Publication number
IT1000092B
IT1000092B IT53277/73A IT5327773A IT1000092B IT 1000092 B IT1000092 B IT 1000092B IT 53277/73 A IT53277/73 A IT 53277/73A IT 5327773 A IT5327773 A IT 5327773A IT 1000092 B IT1000092 B IT 1000092B
Authority
IT
Italy
Prior art keywords
ejectors
improvement
power increase
aircraft systems
aircraft
Prior art date
Application number
IT53277/73A
Other languages
English (en)
Original Assignee
Rockwell International Co
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 Co filed Critical Rockwell International Co
Application granted granted Critical
Publication of IT1000092B publication Critical patent/IT1000092B/it

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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Control Of Turbines (AREA)
IT53277/73A 1972-11-30 1973-10-22 Perfezionamento negli eiettori per incremento di potenza per sistemi aeromobili IT1000092B (it)

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
IT1000092B true IT1000092B (it) 1976-03-30

Family

ID=23204996

Family Applications (1)

Application Number Title Priority Date Filing Date
IT53277/73A IT1000092B (it) 1972-11-30 1973-10-22 Perfezionamento negli eiettori per incremento di potenza per sistemi aeromobili

Country Status (12)

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

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
WO1988010210A1 (en) * 1987-06-25 1988-12-29 Willis Mark T Venturi enhanced airfoil
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
US20110215204A1 (en) * 2007-06-20 2011-09-08 General Electric Company System and method for generating thrust
US20100019079A1 (en) * 2007-06-20 2010-01-28 General Electric Company Thrust generator for a rotary wing aircraft
US11965456B2 (en) * 2015-09-02 2024-04-23 Jetoptera, Inc. Fluidic turbo heater system
JP6930743B2 (ja) 2015-09-02 2021-09-01 ジェトプテラ、インコーポレイテッド エジェクタ及びエアフォイル形状
JP7217272B2 (ja) * 2017-06-16 2023-02-02 ジェトップテラ，インコーポレイテッド ウィングレットエジェクタ構成
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 (en) * 2018-12-24 2021-06-02 LEONARDO S.p.A. Jet fan and vehicle comprising such a fan
EP4025496A1 (en) 2019-09-03 2022-07-13 BAE SYSTEMS plc Fluidic control
EP4025467A1 (en) 2019-09-03 2022-07-13 BAE SYSTEMS plc Vehicle 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 (it) * 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
US3819134A (en) 1974-06-25
JPS4983199A (it) 1974-08-09
FR2208814B1 (it) 1976-05-14
CA967377A (en) 1975-05-13
IL43401A (en) 1976-04-30
GB1448017A (en) 1976-09-02
AU6106273A (en) 1975-05-15
DE2359518B2 (de) 1977-12-08
SE394637B (sv) 1977-07-04
AU469746B2 (en) 1976-02-26
DE2359518C3 (de) 1978-07-20
IL43401A0 (en) 1974-03-14
ES421013A1 (es) 1976-05-01
FR2208814A1 (it) 1974-06-28
DE2366007A1 (de) 1977-08-25
GB1448018A (en) 1976-09-02
DE2359518A1 (de) 1974-06-06

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