SE394637B - Sett och anordning att endra riktningen pa verkningslinjen for en kraftvektor av fluidreaktionskrafter som utovas pa en i ett flygplanssystem ingaende beryta-struktur - Google Patents

Sett och anordning att endra riktningen pa verkningslinjen for en kraftvektor av fluidreaktionskrafter som utovas pa en i ett flygplanssystem ingaende beryta-struktur

Info

Publication number: SE394637B
Authority: SE; Sweden
Prior art keywords: bearta; change; power line; force vector; reaction forces
Prior art date: 1972-11-30

Application number

SE7316085A

Other languages

English (en)

Swedish (sv)

Inventor

L W Throndson

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.)

1972-11-30

Filing date

1973-11-28

Publication date

1977-07-04

1973-11-28 Application filed by Rockwell International Corp filed Critical Rockwell International Corp

1977-07-04 Publication of SE394637B publication Critical patent/SE394637B/xx

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)

SE7316085A 1972-11-30 1973-11-28 Sett och anordning att endra riktningen pa verkningslinjen for en kraftvektor av fluidreaktionskrafter som utovas pa en i ett flygplanssystem ingaende beryta-struktur SE394637B (sv)

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
SE394637B true SE394637B (sv)	1977-07-04

Family

ID=23204996

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
SE7316085A SE394637B (sv)	1972-11-30	1973-11-28	Sett och anordning att endra riktningen pa verkningslinjen for en kraftvektor av fluidreaktionskrafter som utovas pa en i ett flygplanssystem ingaende beryta-struktur

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)	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
US5016837A (en) *	1987-06-25	1991-05-21	Venturi Applications, Inc.	Venturi enhanced airfoil
EP0319574A4 (en) *	1987-06-25	1990-09-05	Mark T. Willis	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
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
CA2996285C (en)	2015-09-02	2023-10-31	Jetoptera, Inc.	Ejector and airfoil configurations
US11965456B2 (en) *	2015-09-02	2024-04-23	Jetoptera, Inc.	Fluidic turbo heater system
EP4563806A3 (de) *	2017-06-16	2025-07-30	Jetoptera, Inc.	Wingletejektorkonfigurationen
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
EP4025496A1 (de)	2019-09-03	2022-07-13	BAE SYSTEMS plc	Fluidische steuerung
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

1972
- 1972-11-30 US US00311011A patent/US3819134A/en not_active Expired - Lifetime
1973
- 1973-10-02 CA CA182,492A patent/CA967377A/en not_active Expired
- 1973-10-05 AU AU61062/73A patent/AU469746B2/en not_active Expired
- 1973-10-08 IL IL43401A patent/IL43401A/en unknown
- 1973-10-09 GB GB4701773A patent/GB1448017A/en not_active Expired
- 1973-10-09 GB GB1792576A patent/GB1448018A/en not_active Expired
- 1973-10-22 IT IT53277/73A patent/IT1000092B/it active
- 1973-11-28 SE SE7316085A patent/SE394637B/xx unknown
- 1973-11-29 DE DE2359518A patent/DE2359518C3/de not_active Expired
- 1973-11-29 BR BR9378/73A patent/BR7309378D0/pt unknown
- 1973-11-29 JP JP48133999A patent/JPS4983199A/ja active Pending
- 1973-11-29 DE DE19732366007 patent/DE2366007A1/de active Pending
- 1973-11-30 FR FR7342811A patent/FR2208814B1/fr not_active Expired
- 1973-11-30 ES ES421013A patent/ES421013A1/es not_active Expired

Also Published As

Publication number	Publication date
IL43401A0 (en)	1974-03-14
AU6106273A (en)	1975-05-15
US3819134A (en)	1974-06-25
GB1448018A (en)	1976-09-02
FR2208814A1 (de)	1974-06-28
GB1448017A (en)	1976-09-02
DE2359518B2 (de)	1977-12-08
CA967377A (en)	1975-05-13
DE2359518A1 (de)	1974-06-06
IT1000092B (it)	1976-03-30
ES421013A1 (es)	1976-05-01
BR7309378D0 (pt)	1974-08-29
IL43401A (en)	1976-04-30
DE2359518C3 (de)	1978-07-20
DE2366007A1 (de)	1977-08-25
FR2208814B1 (de)	1976-05-14
JPS4983199A (de)	1974-08-09
AU469746B2 (en)	1976-02-26

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