IT1097982B - Sistema ausiliario di propulsione per sollevamento con ventilatore anteriore sovradimensionato - Google Patents
Sistema ausiliario di propulsione per sollevamento con ventilatore anteriore sovradimensionatoInfo
- Publication number
- IT1097982B IT1097982B IT26246/78A IT2624678A IT1097982B IT 1097982 B IT1097982 B IT 1097982B IT 26246/78 A IT26246/78 A IT 26246/78A IT 2624678 A IT2624678 A IT 2624678A IT 1097982 B IT1097982 B IT 1097982B
- Authority
- IT
- Italy
- Prior art keywords
- lifting
- auxiliary system
- front fan
- propulsion auxiliary
- oversized front
- Prior art date
Links
Classifications
-
- 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
-
- 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
- B64C29/005—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 the motors being fixed relative to the fuselage
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
-
- 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)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/820,657 US4222233A (en) | 1977-08-02 | 1977-08-02 | Auxiliary lift propulsion system with oversized front fan |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IT7826246A0 IT7826246A0 (it) | 1978-07-28 |
| IT1097982B true IT1097982B (it) | 1985-08-31 |
Family
ID=25231399
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT26246/78A IT1097982B (it) | 1977-08-02 | 1978-07-28 | Sistema ausiliario di propulsione per sollevamento con ventilatore anteriore sovradimensionato |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4222233A (it) |
| JP (1) | JPS5445099A (it) |
| DE (1) | DE2833678A1 (it) |
| FR (1) | FR2399548A1 (it) |
| IT (1) | IT1097982B (it) |
Families Citing this family (52)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2050260B (en) * | 1979-05-29 | 1983-06-22 | Rolls Royce | V/stol aircraft |
| US4506848A (en) * | 1980-12-22 | 1985-03-26 | British Aerospace Public Limited Company | Aircraft configuration and control arrangement therefor |
| US4478377A (en) * | 1980-12-22 | 1984-10-23 | British Aerospace Public Limited Company | Aircraft |
| DE3371893D1 (en) * | 1982-09-03 | 1987-07-09 | British Aerospace | Duct means for aircraft |
| US4833881A (en) * | 1984-12-17 | 1989-05-30 | General Electric Company | Gas turbine engine augmentor |
| US4813229A (en) * | 1985-03-04 | 1989-03-21 | General Electric Company | Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas |
| GB8812978D0 (en) * | 1988-06-01 | 1988-11-16 | British Aerospace | Nozzle assembly for aircraft |
| US4936748A (en) * | 1988-11-28 | 1990-06-26 | General Electric Company | Auxiliary power source in an unducted fan gas turbine engine |
| GB2469614B (en) | 1989-03-14 | 2011-03-23 | British Aerospace | Jet Propulsion Efflux Outlets |
| US5680754A (en) * | 1990-02-12 | 1997-10-28 | General Electric Company | Compressor splitter for use with a forward variable area bypass injector |
| US5307624A (en) * | 1990-04-04 | 1994-05-03 | General Electric Company | Variable area bypass valve assembly |
| US5155993A (en) * | 1990-04-09 | 1992-10-20 | General Electric Company | Apparatus for compressor air extraction |
| US5231825A (en) * | 1990-04-09 | 1993-08-03 | General Electric Company | Method for compressor air extraction |
| US5184461A (en) * | 1990-05-11 | 1993-02-09 | General Electric Company | Method and apparatus for automatic bypass operation |
| US5113649A (en) * | 1990-05-11 | 1992-05-19 | General Electric Company | Passive bypass valve assembly |
| US5054286A (en) * | 1990-06-29 | 1991-10-08 | General Electric Company | Bypass valve system |
| US5048286A (en) * | 1990-06-29 | 1991-09-17 | General Electric Company | Bypass valve door |
| US5160080A (en) * | 1990-10-01 | 1992-11-03 | General Electric Company | Gas turbine engine and method of operation for providing increased output shaft horsepower |
| GB2435637B (en) * | 1991-12-06 | 2008-02-06 | British Aerospace | Jet Propulsion Outlets |
| US5287697A (en) * | 1992-01-02 | 1994-02-22 | General Electric Company | Variable area bypass injector seal |
| CN1105827C (zh) * | 1995-12-20 | 2003-04-16 | 谢逢申 | 移出式超扇发动机 |
| GB2313580B (en) * | 1996-05-31 | 2000-02-23 | Astovl Limited | An aircraft power plant |
| GB2353983B (en) * | 2000-07-04 | 2003-10-15 | Adrian Alexander Hubbard | Variable mode jet engine-suitable for STOVL |
| FR2826055B1 (fr) * | 2001-06-14 | 2003-12-19 | Snecma Moteurs | Dispositif de propulsion a cycle variable par prelevement d'air comprime pour avion supersonique |
| US6918244B2 (en) * | 2001-08-17 | 2005-07-19 | John Eugene Dickau | Vertical takeoff and landing aircraft propulsion systems |
| US6694723B2 (en) | 2002-03-27 | 2004-02-24 | United Technologies Corporation | Valve assembly for gas turbine engine |
| US6729575B2 (en) * | 2002-04-01 | 2004-05-04 | Lockheed Martin Corporation | Propulsion system for a vertical and short takeoff and landing aircraft |
| WO2004002821A1 (en) * | 2002-06-28 | 2004-01-08 | Vtol Technologies Limited | Ducted air power plant |
| US7549291B2 (en) * | 2003-01-28 | 2009-06-23 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| US6968674B2 (en) | 2003-01-28 | 2005-11-29 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| US7121078B2 (en) * | 2003-01-28 | 2006-10-17 | General Electric Company | Methods and apparatus for operating gas turbine engines |
| GB2400411B (en) * | 2003-04-10 | 2006-09-06 | Rolls Royce Plc | Turbofan arrangement |
| US7510140B2 (en) * | 2005-09-12 | 2009-03-31 | The Boeing Company | Method and apparatus for generating lift |
| US7614210B2 (en) * | 2006-02-13 | 2009-11-10 | General Electric Company | Double bypass turbofan |
| US7784266B2 (en) * | 2006-12-18 | 2010-08-31 | General Electric Company | Methods and systems for supplying air to a vehicle |
| US20100170221A1 (en) * | 2009-01-08 | 2010-07-08 | Toyota Jidosha Kabushiki Kaisha | Turbo fan engine |
| US20110167831A1 (en) * | 2009-09-25 | 2011-07-14 | James Edward Johnson | Adaptive core engine |
| US8961114B2 (en) | 2010-11-22 | 2015-02-24 | General Electric Company | Integrated variable geometry flow restrictor and heat exchanger |
| US9279388B2 (en) * | 2011-11-01 | 2016-03-08 | United Technologies Corporation | Gas turbine engine with two-spool fan and variable vane turbine |
| WO2014074135A1 (en) * | 2012-11-12 | 2014-05-15 | United Technologies Corporation | Reverse core turbine engine mounted above aircraft wing |
| US20150225079A1 (en) * | 2013-10-15 | 2015-08-13 | Starck Engineering, LLC | Remotely or autonomously piloted reduced size aircraft with vertical take-off and landing capabilities |
| US10215070B2 (en) | 2015-06-29 | 2019-02-26 | General Electric Company | Power generation system exhaust cooling |
| US10087801B2 (en) | 2015-06-29 | 2018-10-02 | General Electric Company | Power generation system exhaust cooling |
| US10030558B2 (en) * | 2015-06-29 | 2018-07-24 | General Electric Company | Power generation system exhaust cooling |
| US9938874B2 (en) * | 2015-06-29 | 2018-04-10 | General Electric Company | Power generation system exhaust cooling |
| US10060316B2 (en) | 2015-06-29 | 2018-08-28 | General Electric Company | Power generation system exhaust cooling |
| US10316759B2 (en) | 2016-05-31 | 2019-06-11 | General Electric Company | Power generation system exhaust cooling |
| CN106438042A (zh) * | 2016-10-27 | 2017-02-22 | 成都翼高九天科技有限公司 | 一种基于无线通讯无人机的发动机装置 |
| US10737797B2 (en) * | 2017-07-21 | 2020-08-11 | General Electric Company | Vertical takeoff and landing aircraft |
| US11994089B2 (en) * | 2019-04-10 | 2024-05-28 | Rtx Corporation | After-fan system for a gas turbine engine |
| US11846196B2 (en) | 2020-02-21 | 2023-12-19 | Rtx Corporation | After-fan system with electrical motor for gas turbine engines |
| US11808216B1 (en) | 2022-06-10 | 2023-11-07 | Rolls-Royce North American Technologies Inc. | Air-provisioning system with ejectors |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2912188A (en) * | 1955-09-15 | 1959-11-10 | Bell Aircraft Corp | Jet propelled aircraft with tiltable combustion chambers |
| US3186165A (en) * | 1961-11-29 | 1965-06-01 | Gen Electric | Turbofan engine speed synchronizing arrangement |
| GB1003734A (en) * | 1963-08-22 | 1965-09-08 | Rolls Royce | Improvements in gas turbine engines of the by-pass type |
| DE1198131B (de) * | 1964-02-12 | 1965-08-05 | Daimler Benz Ag | Zweikreis-Gasturbinenstrahltriebwerk |
| GB1069033A (en) * | 1965-01-30 | 1967-05-17 | Rolls Royce | Improvements in or relating to gas turbine jet propulsion engines |
| DE2149619A1 (de) * | 1971-10-05 | 1973-04-19 | Motoren Turbinen Union | Turbinenstrahltriebwerk fuer senkrechtoder kurzstartende bzw. landende flugzeuge |
| CA1020365A (en) * | 1974-02-25 | 1977-11-08 | James E. Johnson | Modulating bypass variable cycle turbofan engine |
| US4010608A (en) * | 1975-06-16 | 1977-03-08 | General Electric Company | Split fan work gas turbine engine |
-
1977
- 1977-08-02 US US05/820,657 patent/US4222233A/en not_active Expired - Lifetime
-
1978
- 1978-07-26 FR FR7822091A patent/FR2399548A1/fr not_active Withdrawn
- 1978-07-28 IT IT26246/78A patent/IT1097982B/it active
- 1978-08-01 JP JP9321178A patent/JPS5445099A/ja active Pending
- 1978-08-01 DE DE19782833678 patent/DE2833678A1/de not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| FR2399548A1 (fr) | 1979-03-02 |
| IT7826246A0 (it) | 1978-07-28 |
| DE2833678A1 (de) | 1979-02-15 |
| US4222233A (en) | 1980-09-16 |
| JPS5445099A (en) | 1979-04-10 |
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