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
Application number
JP12646275A
Other languages
Japanese (ja)
Other versions
JPS5164300A (https=
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.)
Filing date
Publication date
Application filed filed Critical
Publication of JPS5164300A publication Critical patent/JPS5164300A/ja
Publication of JPS5647037B2 publication Critical patent/JPS5647037B2/ja
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying 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)
JP12646275A 1974-11-12 1975-10-22 Expired JPS5647037B2 (https=)

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 (https=) 1976-06-03
JPS5647037B2 true JPS5647037B2 (https=) 1981-11-06

Family

ID=5930607

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12646275A Expired JPS5647037B2 (https=) 1974-11-12 1975-10-22

Country Status (5)

Country Link
US (1) US4000868A (https=)
JP (1) JPS5647037B2 (https=)
DE (1) DE2453558C3 (https=)
FR (1) FR2291089A1 (https=)
GB (1) GB1481497A (https=)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
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
AU1345692A (en) * 1991-02-04 1992-09-07 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
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
US9976514B2 (en) 2015-08-27 2018-05-22 Rolls-Royce North American Technologies, Inc. Propulsive force vectoring
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
US10718221B2 (en) 2015-08-27 2020-07-21 Rolls Royce North American Technologies Inc. Morphing vane
US10267160B2 (en) 2015-08-27 2019-04-23 Rolls-Royce North American Technologies Inc. Methods of creating fluidic barriers in turbine engines
US10125622B2 (en) 2015-08-27 2018-11-13 Rolls-Royce North American Technologies Inc. Splayed inlet guide vanes
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
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

Family Cites Families (8)

* Cited by examiner, † Cited by third party
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
US3836099A (en) * 1973-09-28 1974-09-17 Us Navy Airfoil camber change system

Also Published As

Publication number Publication date
GB1481497A (en) 1977-07-27
FR2291089B1 (https=) 1982-09-10
DE2453558C3 (de) 1979-08-30
JPS5164300A (https=) 1976-06-03
DE2453558B2 (de) 1979-01-04
US4000868A (en) 1977-01-04
FR2291089A1 (fr) 1976-06-11
DE2453558A1 (de) 1976-05-20

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