IT7923666A0 - Apparato deviatore di spinta per aereo a decollo ed atterraggio verticale. - Google Patents
Apparato deviatore di spinta per aereo a decollo ed atterraggio verticale.Info
- Publication number
- IT7923666A0 IT7923666A0 IT7923666A IT2366679A IT7923666A0 IT 7923666 A0 IT7923666 A0 IT 7923666A0 IT 7923666 A IT7923666 A IT 7923666A IT 2366679 A IT2366679 A IT 2366679A IT 7923666 A0 IT7923666 A0 IT 7923666A0
- Authority
- IT
- Italy
- Prior art keywords
- vertical take
- landing aircraft
- diverter apparatus
- thrust diverter
- thrust
- Prior art date
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
- B64C29/0066—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 with horizontal jet and jet deflector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/916,627 US4205813A (en) | 1978-06-19 | 1978-06-19 | Thrust vectoring apparatus for a VTOL aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
IT7923666A0 true IT7923666A0 (it) | 1979-06-18 |
IT1121812B IT1121812B (it) | 1986-04-23 |
Family
ID=25437586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT23666/79A IT1121812B (it) | 1978-06-19 | 1979-06-18 | Apparato deviatore di spinta per aereo a decollo ed atterraggio verticale |
Country Status (7)
Country | Link |
---|---|
US (1) | US4205813A (it) |
JP (1) | JPS557991A (it) |
AU (1) | AU4731979A (it) |
DE (1) | DE2924504A1 (it) |
FR (1) | FR2432093A1 (it) |
GB (1) | GB2023075A (it) |
IT (1) | IT1121812B (it) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4358074A (en) * | 1979-05-24 | 1982-11-09 | The Boeing Company | Propulsion system for V/STOL aircraft |
US4326686A (en) * | 1980-02-15 | 1982-04-27 | Runge Thomas M | Fan jet engine bypass air delivery system for blown wing aircraft lift augmentation device |
US4458863A (en) * | 1980-03-10 | 1984-07-10 | The Boeing Company | Strut supported inlet |
US4799633A (en) * | 1982-10-29 | 1989-01-24 | General Electric Company | Laminar flow necelle |
US4587803A (en) * | 1983-08-15 | 1986-05-13 | Rolls-Royce Inc. | Valve for diverting fluid flows in turbomachines |
US6182440B1 (en) * | 1986-01-14 | 2001-02-06 | Northrop Grumman Corporation | Infrared radiation coanda suppressor |
DE3735918A1 (de) * | 1987-10-23 | 1988-09-15 | Harry Sindermann | Klappen-system |
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 |
GB2231622B (en) * | 1989-03-16 | 1993-10-27 | Harold Birkett | Engine for V.T.O.L. Aircraft |
JPH0382699A (ja) * | 1989-08-28 | 1991-04-08 | Aretsukusu Denshi Kogyo Kk | 小形垂直離着陸航空機 |
US5098022A (en) * | 1991-01-07 | 1992-03-24 | United Technologies Corporation | Flow diverting nozzle for a gas turbine engine |
US6318668B1 (en) | 1996-08-02 | 2001-11-20 | Allison Advanced Development Company | Thrust vectoring techniques |
US6105901A (en) * | 1996-08-02 | 2000-08-22 | Allison Engine Co., Inc. | Thrust vectoring system |
US6382559B1 (en) | 1999-08-13 | 2002-05-07 | Rolls-Royce Corporation | Thrust vectoring mechanism |
US6918244B2 (en) * | 2001-08-17 | 2005-07-19 | John Eugene Dickau | Vertical takeoff and landing aircraft propulsion systems |
US6648268B2 (en) | 2002-02-13 | 2003-11-18 | Dupont Anthony A. | Control system for vertical take off and land (VTOL) aircraft |
GB2431626A (en) * | 2005-10-26 | 2007-05-02 | Avcen Ltd | Bypass turbofan engine |
US7721551B2 (en) * | 2006-06-29 | 2010-05-25 | United Technologies Corporation | Fan variable area nozzle for a gas turbine engine fan nacelle |
EP2074301B1 (en) * | 2006-10-12 | 2016-02-24 | United Technologies Corporation | Turbofan engine with thrust vectoring for starting and landing |
US7966827B2 (en) * | 2007-05-31 | 2011-06-28 | United Technologies Corporation | Gas turbine engine with fan variable area nozzle having a rotational valve system |
US8360356B2 (en) * | 2008-07-17 | 2013-01-29 | W. Eric Moore | Flying apparatus |
US20100170221A1 (en) * | 2009-01-08 | 2010-07-08 | Toyota Jidosha Kabushiki Kaisha | Turbo fan engine |
BRPI1001223A2 (pt) * | 2010-04-27 | 2014-03-25 | Marcio Carmo Lopes Pontes | Conjunto de aerofólio para turbo ventilador de avião |
US8549834B2 (en) | 2010-10-21 | 2013-10-08 | United Technologies Corporation | Gas turbine engine with variable area fan nozzle |
GB201508138D0 (en) | 2015-05-13 | 2015-06-24 | Rolls Royce Plc | Aircraft |
US10563613B2 (en) | 2015-08-31 | 2020-02-18 | Rolls-Royce North American Technologies Inc. | Coanda device for a round exhaust nozzle |
DE102020200741A1 (de) | 2020-01-22 | 2021-07-22 | Volkswagen Aktiengesellschaft | Tragflächen-Rotor-Anordnung, Luftfahrzeug und Verfahren zum Betreiben eines Luftfahrzeuges |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3126171A (en) * | 1964-03-24 | Integrated lift and propulsive system for aircraft | ||
FR1155971A (fr) * | 1956-07-11 | 1958-05-12 | Snecma | Perfectionnement aux propulseurs à réaction à plusieurs flux |
US3248878A (en) * | 1963-09-18 | 1966-05-03 | Gen Electric | Thrust deflector and reverser |
GB1103571A (en) * | 1963-10-28 | 1968-02-14 | Bristol Siddeley Engines Ltd | Aircraft jet propulsion engines |
US3262268A (en) * | 1965-06-07 | 1966-07-26 | Gen Electric | Thrust reverser |
US3769797A (en) * | 1971-10-28 | 1973-11-06 | Us Air Force | By-pass engine having a single, thrust diverter valve mechanism for a v/stol aircraft |
US3797785A (en) * | 1972-08-31 | 1974-03-19 | Rohr Industries Inc | Thrust modulating apparatus |
US4030291A (en) * | 1976-01-02 | 1977-06-21 | General Electric Company | Thrust reverser for a gas turbofan engine |
-
1978
- 1978-06-19 US US05/916,627 patent/US4205813A/en not_active Expired - Lifetime
-
1979
- 1979-05-14 GB GB7916721A patent/GB2023075A/en not_active Withdrawn
- 1979-05-23 AU AU47319/79A patent/AU4731979A/en not_active Abandoned
- 1979-06-15 JP JP7477079A patent/JPS557991A/ja active Pending
- 1979-06-18 IT IT23666/79A patent/IT1121812B/it active
- 1979-06-18 FR FR7915505A patent/FR2432093A1/fr not_active Withdrawn
- 1979-06-18 DE DE19792924504 patent/DE2924504A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
AU4731979A (en) | 1980-01-03 |
GB2023075A (en) | 1979-12-28 |
US4205813A (en) | 1980-06-03 |
FR2432093A1 (fr) | 1980-02-22 |
IT1121812B (it) | 1986-04-23 |
DE2924504A1 (de) | 1980-01-03 |
JPS557991A (en) | 1980-01-21 |
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