GB1481497A - Deflector blade - Google Patents

Deflector blade

Info

Publication number
GB1481497A
GB1481497A GB37589/75A GB3758975A GB1481497A GB 1481497 A GB1481497 A GB 1481497A GB 37589/75 A GB37589/75 A GB 37589/75A GB 3758975 A GB3758975 A GB 3758975A GB 1481497 A GB1481497 A GB 1481497A
Authority
GB
United Kingdom
Prior art keywords
pivoted
blade
fixed
pivot
skin
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.)
Expired
Application number
GB37589/75A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Dornier GmbH
Original Assignee
Dornier GmbH
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 by Dornier GmbH filed Critical Dornier GmbH
Publication of GB1481497A publication Critical patent/GB1481497A/en
Expired legal-status Critical Current

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)
GB37589/75A 1974-11-12 1975-09-12 Deflector blade Expired GB1481497A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2453558A DE2453558C3 (de) 1974-11-12 1974-11-12 Schubgas-Umlenkschaufel

Publications (1)

Publication Number Publication Date
GB1481497A true GB1481497A (en) 1977-07-27

Family

ID=5930607

Family Applications (1)

Application Number Title Priority Date Filing Date
GB37589/75A Expired GB1481497A (en) 1974-11-12 1975-09-12 Deflector blade

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=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2276131A (en) * 1993-03-13 1994-09-21 Rolls Royce Plc Variable camber vane

Families Citing this family (20)

* 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
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2276131A (en) * 1993-03-13 1994-09-21 Rolls Royce Plc Variable camber vane
US5464175A (en) * 1993-03-13 1995-11-07 Rolls-Royce Plc Variable camber vane
GB2276131B (en) * 1993-03-13 1996-07-31 Rolls Royce Plc Variable camber vane

Also Published As

Publication number Publication date
FR2291089B1 (https=) 1982-09-10
JPS5647037B2 (https=) 1981-11-06
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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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee