GB2469769B - Aft propeller vane system - Google Patents
Aft propeller vane systemInfo
- Publication number
- GB2469769B GB2469769B GB1013244A GB201013244A GB2469769B GB 2469769 B GB2469769 B GB 2469769B GB 1013244 A GB1013244 A GB 1013244A GB 201013244 A GB201013244 A GB 201013244A GB 2469769 B GB2469769 B GB 2469769B
- Authority
- GB
- United Kingdom
- Prior art keywords
- vane system
- aft propeller
- propeller vane
- aft
- vane
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13491308P | 2008-07-15 | 2008-07-15 | |
GB0912343A GB2461811B (en) | 2008-07-15 | 2009-07-15 | Variable pitch aft propeller vanes |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201013244D0 GB201013244D0 (en) | 2010-09-22 |
GB2469769A GB2469769A (en) | 2010-10-27 |
GB2469769B true GB2469769B (en) | 2011-02-23 |
Family
ID=41058034
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0912343A Active GB2461811B (en) | 2008-07-15 | 2009-07-15 | Variable pitch aft propeller vanes |
GB1013244A Active GB2469769B (en) | 2008-07-15 | 2009-07-15 | Aft propeller vane system |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0912343A Active GB2461811B (en) | 2008-07-15 | 2009-07-15 | Variable pitch aft propeller vanes |
Country Status (2)
Country | Link |
---|---|
US (1) | US20100014977A1 (en) |
GB (2) | GB2461811B (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11300003B2 (en) | 2012-10-23 | 2022-04-12 | General Electric Company | Unducted thrust producing system |
US10202865B2 (en) * | 2012-10-23 | 2019-02-12 | General Electric Company | Unducted thrust producing system |
US20160333729A1 (en) * | 2015-05-11 | 2016-11-17 | General Electric Company | Turbine engine having variable pitch outlet guide vanes |
US11391298B2 (en) * | 2015-10-07 | 2022-07-19 | General Electric Company | Engine having variable pitch outlet guide vanes |
US9771878B2 (en) * | 2015-10-19 | 2017-09-26 | General Electric Company | Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines |
GB2593417A (en) * | 2019-10-02 | 2021-09-29 | Advanced Mobility Res And Development Ltd | Systems and methods for aircraft |
FR3109140B1 (en) * | 2020-04-10 | 2022-04-29 | Safran | System for determining the angular setting of an annular row of stator vanes |
FR3112809B1 (en) * | 2020-07-23 | 2022-07-29 | Safran Aircraft Engines | TURBOMACHINE MODULE EQUIPPED WITH A PROPELLER AND STATOR VANE SUPPORTED BY HOLDING MEANS AND CORRESPONDING TURBOMACHINE |
EP4155506A1 (en) * | 2021-09-26 | 2023-03-29 | Malte Schwarze | Efficient thrust generation |
WO2022228734A2 (en) * | 2021-04-26 | 2022-11-03 | Malte Schwarze | Efficiently generating thrust |
US11802490B2 (en) | 2021-08-25 | 2023-10-31 | Rolls-Royce Corporation | Controllable variable fan outlet guide vanes |
US11788429B2 (en) | 2021-08-25 | 2023-10-17 | Rolls-Royce Corporation | Variable tandem fan outlet guide vanes |
US11686211B2 (en) | 2021-08-25 | 2023-06-27 | Rolls-Royce Corporation | Variable outlet guide vanes |
US11879343B2 (en) | 2021-08-25 | 2024-01-23 | Rolls-Royce Corporation | Systems for controlling variable outlet guide vanes |
US11492918B1 (en) | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
US11802525B2 (en) * | 2022-01-07 | 2023-10-31 | General Electric Company | Outlet guide vane |
US11834995B2 (en) | 2022-03-29 | 2023-12-05 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
US11834954B2 (en) * | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
US11680530B1 (en) | 2022-04-27 | 2023-06-20 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
US11834992B2 (en) | 2022-04-27 | 2023-12-05 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5445105A (en) * | 1994-09-30 | 1995-08-29 | The United States Of America As Represented By The Secretary Of The Navy | Torque balanced postswirl propulsor unit and method for eliminating torque on a submerged body |
WO2004033295A1 (en) * | 2002-10-11 | 2004-04-22 | Stefan Unzicker | Vertical take-off and landing aircraft |
EP1955944A1 (en) * | 2007-02-06 | 2008-08-13 | Daewoo Shipbuilding & Marine Engineering Co., Ltd | Asymmetric preswirl stator of ship |
Family Cites Families (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3047251A (en) * | 1960-07-14 | 1962-07-31 | William L Lewis | Aerodynamic propulsion unit |
US3976265A (en) * | 1973-05-07 | 1976-08-24 | All American Industries, Inc. | Semibuoyant composite aircraft |
US3946554A (en) * | 1974-09-06 | 1976-03-30 | General Electric Company | Variable pitch turbofan engine and a method for operating same |
US4486146A (en) * | 1980-08-08 | 1984-12-04 | British Aerospace Public Limited Company | Aircraft propulsion means |
US4569199A (en) * | 1982-09-29 | 1986-02-11 | The Boeing Company | Turboprop engine and method of operating the same |
US4817382A (en) * | 1985-12-31 | 1989-04-04 | The Boeing Company | Turboprop propulsion apparatus |
US4815273A (en) * | 1985-12-31 | 1989-03-28 | Peter Rudolph | Single propeller turboprop propulsion apparatus |
DE3708596A1 (en) * | 1987-03-17 | 1988-09-29 | Mtu Muenchen Gmbh | GAS TURBINE SYSTEM FOR HELICOPTERS |
US4864820A (en) * | 1987-10-22 | 1989-09-12 | United Technologies Corporation | Exhaust nozzle |
US4917336A (en) * | 1988-02-19 | 1990-04-17 | The Boeing Company | Mounting assembly for unducted prop engine and method |
US4892269A (en) * | 1988-04-28 | 1990-01-09 | Allied-Signal Inc. | Spinner ducted exhaust for pusher turboprop engines |
DE3837994A1 (en) * | 1988-11-09 | 1990-05-10 | Mtu Muenchen Gmbh | DEVICE FOR ADJUSTING THE ROTOR BLADES OF A PROPFAN / TURBO PROPOWER PLANT |
US5683225A (en) * | 1991-10-28 | 1997-11-04 | General Electric Company | Jet engine variable area turbine nozzle |
US5397215A (en) * | 1993-06-14 | 1995-03-14 | United Technologies Corporation | Flow directing assembly for the compression section of a rotary machine |
US5483791A (en) * | 1994-06-14 | 1996-01-16 | Alliedsignal Inc. | Turboprop with impeller inlet strake |
US5791138A (en) * | 1996-01-11 | 1998-08-11 | Burbank Aeuronautical Corporation Ii | Turbofan engine with reduced noise |
US5706651A (en) * | 1995-08-29 | 1998-01-13 | Burbank Aeronautical Corporation Ii | Turbofan engine with reduced noise |
US5961067A (en) * | 1996-09-10 | 1999-10-05 | Allison Engine Company | Method for reducing turboprop noise |
US6041589A (en) * | 1998-01-09 | 2000-03-28 | General Electric Company | Asymmetric turboprop booster |
US6464459B2 (en) * | 1999-05-21 | 2002-10-15 | Avionic Instruments, Inc. | Lifting platform with energy recovery |
US6616094B2 (en) * | 1999-05-21 | 2003-09-09 | Vortex Holding Company | Lifting platform |
US6471158B1 (en) * | 1999-07-15 | 2002-10-29 | Robert P. Davis | Vertical take-off and landing vehicle configured as a compound autogyro |
US6848649B2 (en) * | 2000-10-03 | 2005-02-01 | Charles Gilpin Churchman | V/STOL biplane aircraft |
EP1407130B1 (en) * | 2001-07-18 | 2012-11-07 | Jae-Chang Lee | Jet engine using exhaust gas |
US6974308B2 (en) * | 2001-11-14 | 2005-12-13 | Honeywell International, Inc. | High effectiveness cooled turbine vane or blade |
US6561456B1 (en) * | 2001-12-06 | 2003-05-13 | Michael Thomas Devine | Vertical/short take-off and landing aircraft |
US6769874B2 (en) * | 2002-03-15 | 2004-08-03 | Hamilton Sundstrand | Permanent magnet alternator for a gas turbine engine |
US6811376B2 (en) * | 2002-03-19 | 2004-11-02 | Hamilton Sundstrand | Actuation system for a controllable pitch propeller |
AU2003233159A1 (en) * | 2002-06-26 | 2004-01-19 | R-Jet Engineering Ltd. | Orbiting combustion nozzle engine |
US6981844B2 (en) * | 2003-10-08 | 2006-01-03 | Hamilton Sundstrand | Cyclic actuation system for a controllable pitch propeller and a method of providing aircraft control therewith |
US7163718B2 (en) * | 2003-10-15 | 2007-01-16 | General Electric Company | Method of selective region vapor phase aluminizing |
US6971241B2 (en) * | 2003-11-10 | 2005-12-06 | Honeywell International Inc. | Dual mode power unit having a combustor bypass system |
US6905728B1 (en) * | 2004-03-22 | 2005-06-14 | Honeywell International, Inc. | Cold gas-dynamic spray repair on gas turbine engine components |
US7186070B2 (en) * | 2004-10-12 | 2007-03-06 | Honeywell International, Inc. | Method for modifying gas turbine nozzle area |
US7422419B2 (en) * | 2005-08-17 | 2008-09-09 | Hamilton Sundstrand Corporation | Propeller blade retention system |
US7296969B2 (en) * | 2005-10-12 | 2007-11-20 | Hamilton Sundstrand Corporation | Propeller pitch change system |
-
2009
- 2009-07-13 US US12/501,520 patent/US20100014977A1/en not_active Abandoned
- 2009-07-15 GB GB0912343A patent/GB2461811B/en active Active
- 2009-07-15 GB GB1013244A patent/GB2469769B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5445105A (en) * | 1994-09-30 | 1995-08-29 | The United States Of America As Represented By The Secretary Of The Navy | Torque balanced postswirl propulsor unit and method for eliminating torque on a submerged body |
WO2004033295A1 (en) * | 2002-10-11 | 2004-04-22 | Stefan Unzicker | Vertical take-off and landing aircraft |
US20060186261A1 (en) * | 2002-10-11 | 2006-08-24 | Stefan Unzicker | Vertical take-off and landing aircraft |
EP1955944A1 (en) * | 2007-02-06 | 2008-08-13 | Daewoo Shipbuilding & Marine Engineering Co., Ltd | Asymmetric preswirl stator of ship |
Also Published As
Publication number | Publication date |
---|---|
US20100014977A1 (en) | 2010-01-21 |
GB0912343D0 (en) | 2009-08-26 |
GB2461811A (en) | 2010-01-20 |
GB2469769A (en) | 2010-10-27 |
GB2461811B (en) | 2010-09-22 |
GB201013244D0 (en) | 2010-09-22 |
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