GB787581A - Application of electrical surface heating elements - Google Patents

Application of electrical surface heating elements

Info

Publication number
GB787581A
GB787581A GB27050/54A GB2705054A GB787581A GB 787581 A GB787581 A GB 787581A GB 27050/54 A GB27050/54 A GB 27050/54A GB 2705054 A GB2705054 A GB 2705054A GB 787581 A GB787581 A GB 787581A
Authority
GB
United Kingdom
Prior art keywords
stencil
wing
layer
masking tape
electrical surface
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
GB27050/54A
Inventor
Alexander Gordon Farries
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son 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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Priority to GB27050/54A priority Critical patent/GB787581A/en
Publication of GB787581A publication Critical patent/GB787581A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Surface Heating Bodies (AREA)

Abstract

787,581. Electrical surface heating elements. NAPIER & SON, Ltd., D. Sept. 6, 1955 [Sept. 17, 1954], No. 27050/54. Class 39(3) [Also in Group XVI] In forming an electrical surface heating element including a metallic resistance 'heating layer, a stencil is used for indicating the portions of an insulating supporting member to be covered with the metallic layer which layer is prevented from covering the remaining portions of the; supporting member by means of masking tape. A stencil for use in producing deicing or anti-icing means on an aircraft wing part A is formed by applying two or more layers of glass cloth C impregnated with thermo-setting plastic material in fluid state to the part A which is already coated with an insulating layer covered by a separating or " release " agent. After curing or permitting the plastic material to cure, the composite sheet C<SP>1</SP> is removed and slotted C<SP>3</SP> to form a stencil which is used in marking the wing by a dye sprayed through the stencil. After removal of the stencil, masking tape is applied to the wing in a pattern indicated by the dye markings, and the wing is sprayed with a metallic spray. Finally, the masking tape is removed, leaving conducting strips G to form the heating element over which an outer insulating layer is applied. Terminals are provided. Specifications 703,374 and 740,551 are referred to.
GB27050/54A 1954-09-17 1954-09-17 Application of electrical surface heating elements Expired GB787581A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27050/54A GB787581A (en) 1954-09-17 1954-09-17 Application of electrical surface heating elements

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27050/54A GB787581A (en) 1954-09-17 1954-09-17 Application of electrical surface heating elements

Publications (1)

Publication Number Publication Date
GB787581A true GB787581A (en) 1957-12-11

Family

ID=10253346

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27050/54A Expired GB787581A (en) 1954-09-17 1954-09-17 Application of electrical surface heating elements

Country Status (1)

Country Link
GB (1) GB787581A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2225285A (en) * 1988-09-20 1990-05-30 Jennifer Ann Hill Forming design on surfaces
GB2241795A (en) * 1989-10-21 1991-09-11 British Aerospace Mask and method for the production of grooves or ribs in or on a surface.
WO2006085054A1 (en) * 2005-02-09 2006-08-17 Qinetiq Limited Ice protection of aerodynamic surfaces
WO2008119664A2 (en) 2007-03-30 2008-10-09 Airbus España S.L. Leading edge for aircraft made of reinforced composite material
ES2339201A1 (en) * 2007-07-27 2010-05-17 Airbus España, S.L. Structure made of composite material having a metallized surface
WO2011018695A1 (en) * 2009-08-11 2011-02-17 EcoTemp International, Inc. Deicing film for wind turbine air foil
EP3597541A1 (en) * 2018-07-16 2020-01-22 The Boeing Company Aircraft ice protection systems

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2225285A (en) * 1988-09-20 1990-05-30 Jennifer Ann Hill Forming design on surfaces
GB2241795A (en) * 1989-10-21 1991-09-11 British Aerospace Mask and method for the production of grooves or ribs in or on a surface.
US9771158B2 (en) 2005-02-09 2017-09-26 Qinetiq Limited Ice protection of aerodynamic surfaces
WO2006085054A1 (en) * 2005-02-09 2006-08-17 Qinetiq Limited Ice protection of aerodynamic surfaces
WO2008119664A2 (en) 2007-03-30 2008-10-09 Airbus España S.L. Leading edge for aircraft made of reinforced composite material
WO2008119664A3 (en) * 2007-03-30 2010-04-29 Airbus España S.L. Leading edge for aircraft made of reinforced composite material
ES2329324A1 (en) * 2007-03-30 2009-11-24 Airbus España, S.L. Leading edge for aircraft made of reinforced composite material
ES2339201A1 (en) * 2007-07-27 2010-05-17 Airbus España, S.L. Structure made of composite material having a metallized surface
WO2009016093A3 (en) * 2007-07-27 2010-07-29 Airbus España S.L. Structure made of composite material having a metallized surface
WO2011018695A1 (en) * 2009-08-11 2011-02-17 EcoTemp International, Inc. Deicing film for wind turbine air foil
EP3597541A1 (en) * 2018-07-16 2020-01-22 The Boeing Company Aircraft ice protection systems
CN110723294A (en) * 2018-07-16 2020-01-24 波音公司 Aircraft anti-icing system and method of making same
US11008109B2 (en) 2018-07-16 2021-05-18 The Boeing Company Aircraft ice protection systems
CN110723294B (en) * 2018-07-16 2024-09-17 波音公司 Aircraft anti-icing system and method of manufacturing the same

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