GB1383802A - Aircraft control element - Google Patents

Aircraft control element

Info

Publication number
GB1383802A
GB1383802A GB491572A GB491572A GB1383802A GB 1383802 A GB1383802 A GB 1383802A GB 491572 A GB491572 A GB 491572A GB 491572 A GB491572 A GB 491572A GB 1383802 A GB1383802 A GB 1383802A
Authority
GB
United Kingdom
Prior art keywords
control surface
control element
aircraft
torsion elements
control
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
GB491572A
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of GB1383802A publication Critical patent/GB1383802A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • 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
    • Y02T50/40—Weight reduction
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Heating, Cooling, Or Curing Plastics Or The Like In General (AREA)
GB491572A 1971-02-11 1972-02-02 Aircraft control element Expired GB1383802A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR717104579A FR2125111B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1971-02-11 1971-02-11

Publications (1)

Publication Number Publication Date
GB1383802A true GB1383802A (en) 1974-02-12

Family

ID=9071734

Family Applications (1)

Application Number Title Priority Date Filing Date
GB491572A Expired GB1383802A (en) 1971-02-11 1972-02-02 Aircraft control element

Country Status (3)

Country Link
US (1) US3883093A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2125111B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1383802A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103640689A (zh) * 2013-11-28 2014-03-19 江西洪都航空工业集团有限责任公司 一种飞机全动舵面安装结构

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4304376A (en) * 1977-12-05 1981-12-08 The Boeing Company Composite honeycomb core structures and single stage hot bonding method of producing such structures
US4284443A (en) * 1979-02-05 1981-08-18 The Boeing Company Single stage hot bonding method for producing composite honeycomb core structures
US4330100A (en) * 1979-09-28 1982-05-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Means for controlling aerodynamically induced twist
US4305177A (en) * 1979-11-28 1981-12-15 The Boeing Company Hinge assembly for controllable surfaces
US4498647A (en) * 1982-03-15 1985-02-12 Mcdonnel Douglas Corporation Surface hold-down mechanism
US4483498A (en) * 1982-07-14 1984-11-20 Mcdonnell Douglas Corporation Flight control surface coupling system
FR2693701B1 (fr) * 1992-07-16 1994-09-02 France Etat Armement Safrans pour navires de moyen et gros tonnage.
US6000660A (en) * 1998-01-19 1999-12-14 Southwest Research Institute Rotary beam variable stiffness wing spar
DE19909257C2 (de) * 1999-03-03 2001-07-12 Eurocopter Deutschland Verbindungsmittel zum Verbinden einer beweglichen Klappe mit einem Flügel eines Luftfahrzeuges
US6508439B1 (en) * 1999-05-18 2003-01-21 Diversified Technologies, Inc. Flap actuator system
US6513762B2 (en) 1999-05-18 2003-02-04 Diversified Technologies, Inc. Flap actuator system
JP3498838B2 (ja) * 1999-11-01 2004-02-23 川崎重工業株式会社 フラップ支持機構およびフラップ付ロータブレード
DE10156733B4 (de) * 2001-11-19 2006-04-20 Eads Deutschland Gmbh Aerodynamisches Profil mit verstellbarer Klappe
DE60329077D1 (de) * 2003-05-09 2009-10-15 Pilatus Flugzeugwerke Ag Flugzeugflügel
GB2472759A (en) 2009-03-17 2011-02-23 Vestas Wind Sys As Retractable hinge apparatus for wind turbine control surface
GB2470345A (en) * 2009-03-17 2010-11-24 Vestas Wind Systems A S Rotary actuator hinge for connecting first and second wind turbine components.
DE102009051983A1 (de) * 2009-11-05 2011-05-12 Airbus Operations Gmbh Tragflügel eines Flugzeugs
US9643716B2 (en) * 2014-04-01 2017-05-09 The Boeing Company Air vehicle, actuator assembly and associated method of manufacture
US20170106970A1 (en) 2015-10-15 2017-04-20 The Boeing Company Composite failsafe torque tube
US10597141B2 (en) * 2018-03-30 2020-03-24 The Boeing Company Wing flap with torque member and method for forming thereof
US10759516B2 (en) * 2018-03-30 2020-09-01 The Boeing Company Wing flap with torque member and method for forming thereof
US10647407B2 (en) * 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US11623734B2 (en) 2020-12-02 2023-04-11 The Boeing Company Apparatus, system and method for supporting a wing flap of an aircraft
US12151812B2 (en) * 2022-02-02 2024-11-26 Rohr, Inc. Resin pressure molded aerostructure with integrated metal coupling

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1400078A (en) * 1918-04-16 1921-12-13 Westinghouse Electric & Mfg Co Molded tube
GB437034A (en) * 1934-04-23 1935-10-23 Audrey Gretchen Coats Improvements in or relating to helicopter and other rotating wing aircraft
US2400649A (en) * 1942-02-27 1946-05-21 Autogiro Co Of America Molded airfoil, especially for sustaining rotors
US2370844A (en) * 1943-01-29 1945-03-06 Cons Vultee Aircraft Corp Airplane control mechanism of the boost tab type
US2720272A (en) * 1946-06-27 1955-10-11 Gen Electric Rotary propeller having twistable blades
US2573361A (en) * 1947-02-13 1951-10-30 Libbey Owens Ford Glass Co Torsion transmitting glass shaft and method of manufacture
US2696956A (en) * 1951-01-09 1954-12-14 Douglas Aircraft Co Inc Safety mechanism for operating control surfaces
US2852209A (en) * 1955-10-14 1958-09-16 Acrophysics Dev Corp Aircraft control surface deflection apparatus
US2999658A (en) * 1958-07-16 1961-09-12 Pavlecka John Airfoil structure
US3022536A (en) * 1959-06-09 1962-02-27 Unitcast Corp Torsion spring assembly
USRE25594E (en) * 1960-06-17 1964-06-09 Torque limiting sprag mechanism
GB1047568A (en) * 1963-10-09 1966-11-09 Westland Aircraft Ltd Improvements in or relating to aircraft rotors
NL6500558A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1965-01-15 1966-07-18
US3574104A (en) * 1968-01-24 1971-04-06 Plastigage Corp Glass fiber constructional member
FR1572631A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1968-06-17 1969-06-27

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103640689A (zh) * 2013-11-28 2014-03-19 江西洪都航空工业集团有限责任公司 一种飞机全动舵面安装结构

Also Published As

Publication number Publication date
FR2125111A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1972-09-29
US3883093A (en) 1975-05-13
FR2125111B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1974-02-15

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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