GB1110217A - Improvements in or relating to aircraft de-icing systems - Google Patents

Improvements in or relating to aircraft de-icing systems

Info

Publication number
GB1110217A
GB1110217A GB36503/64A GB3650364A GB1110217A GB 1110217 A GB1110217 A GB 1110217A GB 36503/64 A GB36503/64 A GB 36503/64A GB 3650364 A GB3650364 A GB 3650364A GB 1110217 A GB1110217 A GB 1110217A
Authority
GB
United Kingdom
Prior art keywords
mat
aircraft
bonded
leading edge
wing leading
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
GB36503/64A
Inventor
Thomas Edward Godden
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.)
M H GODDEN Ltd
Original Assignee
M H GODDEN Ltd
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 M H GODDEN Ltd filed Critical M H GODDEN Ltd
Priority to GB36503/64A priority Critical patent/GB1110217A/en
Publication of GB1110217A publication Critical patent/GB1110217A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating

Abstract

1,110,217. Aircraft de-icing systems. M. H. GODDEN Ltd. 31 Aug., 1965 [5 Sept., 1964; 3 Nov., 1964], Nos. 36503/64 and 44684/64. Heading B7W. An aircraft de-icing system comprises an electrical resistance mat 1 bonded to the inner side of a metal skin 2 defining the surface to be de-iced, as described, a wing leading edge. The mat comprises continuously heated parting strips 4, and cyclically heated areas 5, 6, 7, and is bonded to the skin by an epoxy resin to which aluminium powder has been added to improve its thermal conductivity. The mat consists of glass fibre fabric in which are woven the P.T.F.E. insulated heating wires, and into which are moulded strengthening ribs dimensioned to suit the shape of the wing leading edge. The mat is covered by a plastics or rubber insulating layer 8.
GB36503/64A 1964-09-05 1964-09-05 Improvements in or relating to aircraft de-icing systems Expired GB1110217A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB36503/64A GB1110217A (en) 1964-09-05 1964-09-05 Improvements in or relating to aircraft de-icing systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB36503/64A GB1110217A (en) 1964-09-05 1964-09-05 Improvements in or relating to aircraft de-icing systems

Publications (1)

Publication Number Publication Date
GB1110217A true GB1110217A (en) 1968-04-18

Family

ID=10388770

Family Applications (1)

Application Number Title Priority Date Filing Date
GB36503/64A Expired GB1110217A (en) 1964-09-05 1964-09-05 Improvements in or relating to aircraft de-icing systems

Country Status (1)

Country Link
GB (1) GB1110217A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5174024A (en) * 1990-09-17 1992-12-29 Sterrett Terry L Tail rotor abrasive strip
US5542820A (en) * 1994-12-23 1996-08-06 United Technologies Corporation Engineered ceramic components for the leading edge of a helicopter rotor blade
GB2319942A (en) * 1996-11-27 1998-06-03 Eurocopter Aeroport Internatio Aerofoil heating device
US5765779A (en) * 1995-02-15 1998-06-16 Dunlop Limited Ice protection device
EP1486417A1 (en) * 2003-06-14 2004-12-15 PANAGHE, Stylianos A heated aerofoil
GB2438389A (en) * 2006-05-23 2007-11-28 Gkn Aerospace Transparency Sys Heating system for leading edge of aircraft
GB2439825A (en) * 2006-06-28 2008-01-09 Goodrich Corp Aircraft Ice Protection Method
WO2009050454A1 (en) * 2007-10-18 2009-04-23 Gkn Aerospace Services Limited Structural bonding arrangement
WO2010128299A1 (en) 2009-05-06 2010-11-11 Gkn Aerospace Services Limited Heating system
CN103538724A (en) * 2012-07-13 2014-01-29 Mra系统有限公司 Aircraft ice protection system and method
GB2505994A (en) * 2012-07-13 2014-03-19 Mra Systems Inc Electrically heated aircraft component ice protection system
US9758237B2 (en) 2009-06-04 2017-09-12 Airbus Operations Limited Aircraft wire fairing
CN107914866A (en) * 2016-10-11 2018-04-17 空中客车防卫和太空有限责任公司 The method for the Crossflow Instabilities for influencing to wave on body and the system system that waves
EP3546364A1 (en) * 2018-03-28 2019-10-02 Ratier-Figeac SAS De-icing apparatus

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5174024A (en) * 1990-09-17 1992-12-29 Sterrett Terry L Tail rotor abrasive strip
US5542820A (en) * 1994-12-23 1996-08-06 United Technologies Corporation Engineered ceramic components for the leading edge of a helicopter rotor blade
US5765779A (en) * 1995-02-15 1998-06-16 Dunlop Limited Ice protection device
GB2319942A (en) * 1996-11-27 1998-06-03 Eurocopter Aeroport Internatio Aerofoil heating device
GB2319942B (en) * 1996-11-27 2000-08-02 Eurocopter France Device for heating an aerofoil
EP1486417A1 (en) * 2003-06-14 2004-12-15 PANAGHE, Stylianos A heated aerofoil
GB2438389A (en) * 2006-05-23 2007-11-28 Gkn Aerospace Transparency Sys Heating system for leading edge of aircraft
GB2439825B (en) * 2006-06-28 2011-07-06 Goodrich Corp Aircraft ice protection method
GB2439825A (en) * 2006-06-28 2008-01-09 Goodrich Corp Aircraft Ice Protection Method
US7556221B2 (en) 2006-06-28 2009-07-07 Goodrich Corporation Aircraft ice protection method
US8714489B2 (en) 2007-10-18 2014-05-06 Gkn Aerospace Services Limited Structural bonding arrangement
GB2453934B (en) * 2007-10-18 2012-09-05 Gkn Aerospace Services Ltd Aircraft leading edge component with thermoplastic heater
WO2009050454A1 (en) * 2007-10-18 2009-04-23 Gkn Aerospace Services Limited Structural bonding arrangement
WO2010128299A1 (en) 2009-05-06 2010-11-11 Gkn Aerospace Services Limited Heating system
US9758237B2 (en) 2009-06-04 2017-09-12 Airbus Operations Limited Aircraft wire fairing
CN103538724A (en) * 2012-07-13 2014-01-29 Mra系统有限公司 Aircraft ice protection system and method
GB2505994A (en) * 2012-07-13 2014-03-19 Mra Systems Inc Electrically heated aircraft component ice protection system
GB2505994B (en) * 2012-07-13 2014-10-15 Mra Systems Inc Aircraft ice protection system and method
US9193466B2 (en) 2012-07-13 2015-11-24 Mra Systems, Inc. Aircraft ice protection system and method
US9309001B2 (en) 2012-07-13 2016-04-12 MRA Systems Inc. Aircraft ice protection system and method
CN107914866A (en) * 2016-10-11 2018-04-17 空中客车防卫和太空有限责任公司 The method for the Crossflow Instabilities for influencing to wave on body and the system system that waves
EP3309065A1 (en) * 2016-10-11 2018-04-18 Airbus Defence and Space GmbH Method for influencing cross-flow instabilities in a fluid flow body and flow body system
EP3546364A1 (en) * 2018-03-28 2019-10-02 Ratier-Figeac SAS De-icing apparatus

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