JPS5647037B2 - - Google Patents
Info
- Publication number
- JPS5647037B2 JPS5647037B2 JP12646275A JP12646275A JPS5647037B2 JP S5647037 B2 JPS5647037 B2 JP S5647037B2 JP 12646275 A JP12646275 A JP 12646275A JP 12646275 A JP12646275 A JP 12646275A JP S5647037 B2 JPS5647037 B2 JP S5647037B2
- Authority
- JP
- Japan
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
- Control Of Turbines (AREA)
- Mechanical Control Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2453558A DE2453558C3 (de) | 1974-11-12 | 1974-11-12 | Schubgas-Umlenkschaufel |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5164300A JPS5164300A (ja) | 1976-06-03 |
JPS5647037B2 true JPS5647037B2 (ja) | 1981-11-06 |
Family
ID=5930607
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12646275A Expired JPS5647037B2 (ja) | 1974-11-12 | 1975-10-22 |
Country Status (5)
Country | Link |
---|---|
US (1) | US4000868A (ja) |
JP (1) | JPS5647037B2 (ja) |
DE (1) | DE2453558C3 (ja) |
FR (1) | FR2291089A1 (ja) |
GB (1) | GB1481497A (ja) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4235397A (en) * | 1978-04-29 | 1980-11-25 | British Aerospace | Flow deflector blades |
US5181678A (en) * | 1991-02-04 | 1993-01-26 | Flex Foil Technology, Inc. | Flexible tailored elastic airfoil section |
WO1992013758A1 (en) * | 1991-02-04 | 1992-08-20 | Flex Foil Technology, Inc. | Flexible tailored elastic airfoil section |
US5207558A (en) * | 1991-10-30 | 1993-05-04 | The United States Of America As Represented By The Secretary Of The Air Force | Thermally actuated vane flow control |
GB9203168D0 (en) * | 1992-02-13 | 1992-04-01 | Rolls Royce Plc | Guide vanes for gas turbine engines |
GB2276131B (en) * | 1993-03-13 | 1996-07-31 | Rolls Royce Plc | Variable camber vane |
US9650903B2 (en) * | 2009-08-28 | 2017-05-16 | United Technologies Corporation | Combustor turbine interface for a gas turbine engine |
US8844879B2 (en) * | 2011-12-12 | 2014-09-30 | The Boeing Company | Wing variable camber trailing edge tip |
US9909530B2 (en) * | 2013-08-05 | 2018-03-06 | United Technologies Corporation | Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsion |
US10280872B2 (en) | 2015-08-27 | 2019-05-07 | Rolls-Royce North American Technologies Inc. | System and method for a fluidic barrier from the upstream splitter |
US10267159B2 (en) | 2015-08-27 | 2019-04-23 | Rolls-Royce North America Technologies Inc. | System and method for creating a fluidic barrier with vortices from the upstream splitter |
US10267160B2 (en) | 2015-08-27 | 2019-04-23 | Rolls-Royce North American Technologies Inc. | Methods of creating fluidic barriers in turbine engines |
US9976514B2 (en) | 2015-08-27 | 2018-05-22 | Rolls-Royce North American Technologies, Inc. | Propulsive force vectoring |
US10233869B2 (en) | 2015-08-27 | 2019-03-19 | Rolls Royce North American Technologies Inc. | System and method for creating a fluidic barrier from the leading edge of a fan blade |
US10718221B2 (en) | 2015-08-27 | 2020-07-21 | Rolls Royce North American Technologies Inc. | Morphing vane |
US9915149B2 (en) | 2015-08-27 | 2018-03-13 | Rolls-Royce North American Technologies Inc. | System and method for a fluidic barrier on the low pressure side of a fan blade |
US10125622B2 (en) | 2015-08-27 | 2018-11-13 | Rolls-Royce North American Technologies Inc. | Splayed inlet guide vanes |
US20170057649A1 (en) | 2015-08-27 | 2017-03-02 | Edward C. Rice | Integrated aircraft propulsion system |
CN107444612B (zh) * | 2017-08-15 | 2023-04-18 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种λ机翼飞翼布局无人飞行器的变机翼前缘装置 |
CN111959746B (zh) * | 2020-08-31 | 2022-10-11 | 哈尔滨工业大学 | 一种平行连杆式变形翼骨架 |
US12000359B2 (en) | 2022-08-18 | 2024-06-04 | General Electric Company | Cascade thrust reverser actuation assembly for a turbofan engine |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3836099A (en) * | 1973-09-28 | 1974-09-17 | Us Navy | Airfoil camber change system |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191515290A (en) * | 1915-10-29 | 1916-10-30 | Varioplane Company Ltd | Improvements in and relating to Planes or the like for Aeroplanes. |
FR574803A (fr) * | 1922-12-30 | 1924-07-19 | Perfectionnements apportés à des ailes fluido-dynamiques, variables, telles que les ailes pour aéroplanes | |
US2740597A (en) * | 1951-05-11 | 1956-04-03 | Sylvester J Wittman | Airfoil |
US2929580A (en) * | 1956-06-18 | 1960-03-22 | Piasecki Aircraft Corp | Aircraft for vertical or short takeoff, and integrated propulsion lifting and propeller slip stream deflecting unit therefor |
US3109613A (en) * | 1960-11-28 | 1963-11-05 | Mabel Wilson Raspet | Variable-camber airfoil |
US3212731A (en) * | 1963-09-09 | 1965-10-19 | Gen Electric | Fan powered aircraft |
US3698668A (en) * | 1971-04-08 | 1972-10-17 | Boeing Co | Variable camber airfoil |
-
1974
- 1974-11-12 DE DE2453558A patent/DE2453558C3/de not_active Expired
-
1975
- 1975-09-12 GB GB37589/75A patent/GB1481497A/en not_active Expired
- 1975-10-22 JP JP12646275A patent/JPS5647037B2/ja not_active Expired
- 1975-10-24 FR FR7533300A patent/FR2291089A1/fr active Granted
- 1975-11-10 US US05/630,184 patent/US4000868A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3836099A (en) * | 1973-09-28 | 1974-09-17 | Us Navy | Airfoil camber change system |
Also Published As
Publication number | Publication date |
---|---|
US4000868A (en) | 1977-01-04 |
DE2453558A1 (de) | 1976-05-20 |
JPS5164300A (ja) | 1976-06-03 |
FR2291089A1 (fr) | 1976-06-11 |
GB1481497A (en) | 1977-07-27 |
FR2291089B1 (ja) | 1982-09-10 |
DE2453558C3 (de) | 1979-08-30 |
DE2453558B2 (de) | 1979-01-04 |