GB1117843A - Improvements relating to anti-icing heating apparatus - Google Patents

Improvements relating to anti-icing heating apparatus

Info

Publication number
GB1117843A
GB1117843A GB8544/66A GB854466A GB1117843A GB 1117843 A GB1117843 A GB 1117843A GB 8544/66 A GB8544/66 A GB 8544/66A GB 854466 A GB854466 A GB 854466A GB 1117843 A GB1117843 A GB 1117843A
Authority
GB
United Kingdom
Prior art keywords
heating element
temperature sensitive
sensitive device
neoprene
gas turbine
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
GB8544/66A
Inventor
William Sherlaw
Anthony Gordon Neaverson
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8544/66A priority Critical patent/GB1117843A/en
Publication of GB1117843A publication Critical patent/GB1117843A/en
Expired legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • H05B3/20—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater
    • H05B3/22—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible
    • H05B3/26—Heating elements having extended surface area substantially in a two-dimensional plane, e.g. plate-heater non-flexible heating conductor mounted on insulating base
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B3/00—Ohmic-resistance heating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B2214/00—Aspects relating to resistive heating, induction heating and heating using microwaves, covered by groups H05B3/00, H05B6/00
    • H05B2214/02—Heaters specially designed for de-icing or protection against icing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Resistance Heating (AREA)

Abstract

1117843 Gas turbine plant ROLLS ROYCE Ltd 22 March 1967 [25 Feb 1966] 8544/66 Heading F1G [Also in Division G3] Apparatus for preventing the formation of ice on a surface - such as the surface of the air intake of a gas turbine engine - comprises an electrical heating element disposed adjacent the surface but insulated therefrom by a layer of neoprene and a temperature sensitive resistor device disposed adjacent the heating element and which extends throughout the whole surface area of the heating element, the temperature sensitive device and the heating element being insulated from one another by means of a further layer of neoprene. The heating element and the temperature sensitive device may both be formed by a sinuous pattern of nickel foil. The temperature sensitive device controls the supply of energy to the heating element by the increase with temperature of its resistance, with or without the aid of a magnetic amplifier.
GB8544/66A 1966-02-25 1966-02-25 Improvements relating to anti-icing heating apparatus Expired GB1117843A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8544/66A GB1117843A (en) 1966-02-25 1966-02-25 Improvements relating to anti-icing heating apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8544/66A GB1117843A (en) 1966-02-25 1966-02-25 Improvements relating to anti-icing heating apparatus

Publications (1)

Publication Number Publication Date
GB1117843A true GB1117843A (en) 1968-06-26

Family

ID=9854497

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8544/66A Expired GB1117843A (en) 1966-02-25 1966-02-25 Improvements relating to anti-icing heating apparatus

Country Status (1)

Country Link
GB (1) GB1117843A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1715159A1 (en) * 2005-04-22 2006-10-25 Rohr, Inc. Aircraft engine nacelle inlet having access opening for electrical ice protection system
GB2425448A (en) * 2005-04-22 2006-10-25 Bernard Bollons Carburettor with electrically heated throttle valve disc
GB2428275A (en) * 2005-07-14 2007-01-24 Goodrich Corp Aircraft engine nacelle ice protection system
FR2898868A1 (en) * 2006-03-24 2007-09-28 Aircelle Sa Lip structure for air intake nozzle of jet engine, has heating electric element connected to power supply, where heating electric element is situated between internal skin and external skin of structure
WO2007135383A1 (en) * 2006-05-23 2007-11-29 Gkn Aerospace Services Limited Heating system for leading edge of aircraft
US7513458B2 (en) 2005-04-22 2009-04-07 Rohr, Inc. Aircraft engine nacelle inlet having electrical ice protection system
US7556221B2 (en) 2006-06-28 2009-07-07 Goodrich Corporation Aircraft ice protection method
US7832983B2 (en) 2006-05-02 2010-11-16 Goodrich Corporation Nacelles and nacelle components containing nanoreinforced carbon fiber composite material
WO2013130593A1 (en) * 2012-02-27 2013-09-06 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
US8561934B2 (en) 2009-08-28 2013-10-22 Teresa M. Kruckenberg Lightning strike protection
US8752279B2 (en) 2007-01-04 2014-06-17 Goodrich Corporation Methods of protecting an aircraft component from ice formation
US8962130B2 (en) 2006-03-10 2015-02-24 Rohr, Inc. Low density lightning strike protection for use in airplanes
EP3031726A1 (en) * 2014-12-08 2016-06-15 Zodiac Aerotechnics Wing element for aircraft
FR3120851A1 (en) * 2021-03-16 2022-09-23 Airbus Operations (S.A.S.) Method of operating an ice treatment system combining at least two heating mats and an aircraft outer wall comprising an ice treatment system operating according to this method

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7364139B2 (en) 2005-04-22 2008-04-29 Bernard Bollons Carburetors
GB2425448A (en) * 2005-04-22 2006-10-25 Bernard Bollons Carburettor with electrically heated throttle valve disc
EP1715159A1 (en) * 2005-04-22 2006-10-25 Rohr, Inc. Aircraft engine nacelle inlet having access opening for electrical ice protection system
US7631838B2 (en) 2005-04-22 2009-12-15 Rohr, Inc. Aircraft engine nacelle inlet having access opening for electrical ice protection system
EP1715174A3 (en) * 2005-04-22 2008-07-02 Bernard Bollons Carburettors
GB2425448B (en) * 2005-04-22 2008-12-24 Bernard Bollons Carburettors
US7469862B2 (en) 2005-04-22 2008-12-30 Goodrich Corporation Aircraft engine nacelle inlet having access opening for electrical ice protection system
US7513458B2 (en) 2005-04-22 2009-04-07 Rohr, Inc. Aircraft engine nacelle inlet having electrical ice protection system
US7681838B2 (en) 2005-04-22 2010-03-23 Rohr, Inc. Aircraft engine nacelle inlet having access opening for electrical ice protection system
EP2112353A1 (en) 2005-04-22 2009-10-28 Rohr, Inc. Aircraft engine nacelle inlet
GB2428275A (en) * 2005-07-14 2007-01-24 Goodrich Corp Aircraft engine nacelle ice protection system
GB2428275B (en) * 2005-07-14 2011-04-06 Goodrich Corp Aircraft engine nacelle ice protection system
US7780117B2 (en) 2005-07-14 2010-08-24 Goodrich Corporation Aircraft engine nacelle ice protection system
US8962130B2 (en) 2006-03-10 2015-02-24 Rohr, Inc. Low density lightning strike protection for use in airplanes
FR2898868A1 (en) * 2006-03-24 2007-09-28 Aircelle Sa Lip structure for air intake nozzle of jet engine, has heating electric element connected to power supply, where heating electric element is situated between internal skin and external skin of structure
WO2007110494A1 (en) * 2006-03-24 2007-10-04 Aircelle Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
US8240982B2 (en) 2006-03-24 2012-08-14 Aircelle Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
CN101405184B (en) * 2006-03-24 2013-06-12 埃尔塞乐公司 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
US7832983B2 (en) 2006-05-02 2010-11-16 Goodrich Corporation Nacelles and nacelle components containing nanoreinforced carbon fiber composite material
WO2007135383A1 (en) * 2006-05-23 2007-11-29 Gkn Aerospace Services Limited Heating system for leading edge of aircraft
US7556221B2 (en) 2006-06-28 2009-07-07 Goodrich Corporation Aircraft ice protection method
US8752279B2 (en) 2007-01-04 2014-06-17 Goodrich Corporation Methods of protecting an aircraft component from ice formation
US8561934B2 (en) 2009-08-28 2013-10-22 Teresa M. Kruckenberg Lightning strike protection
WO2013130593A1 (en) * 2012-02-27 2013-09-06 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
US20130248511A1 (en) * 2012-02-27 2013-09-26 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
JP2015513178A (en) * 2012-02-27 2015-04-30 ワトロウ エレクトリック マニュファクチュアリング カンパニー Temperature detection and control system for layered heating elements
US9078293B2 (en) * 2012-02-27 2015-07-07 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
US20150264746A1 (en) * 2012-02-27 2015-09-17 Watlow Electric Manufacturing Company Temperature Detection And Control System For Layered Heaters
US10104718B2 (en) * 2012-02-27 2018-10-16 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
US20190029076A1 (en) * 2012-02-27 2019-01-24 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
US11304264B2 (en) * 2012-02-27 2022-04-12 Watlow Electric Manufacturing Company Temperature detection and control system for layered heaters
EP3031726A1 (en) * 2014-12-08 2016-06-15 Zodiac Aerotechnics Wing element for aircraft
US9932115B2 (en) 2014-12-08 2018-04-03 Zodiac Aerotechnics Aircraft wing element
FR3120851A1 (en) * 2021-03-16 2022-09-23 Airbus Operations (S.A.S.) Method of operating an ice treatment system combining at least two heating mats and an aircraft outer wall comprising an ice treatment system operating according to this method
US11975848B2 (en) 2021-03-16 2024-05-07 Airbus Operations Sas Method for operating a frost treatment system combining at least two heating mats and outer aircraft wall comprising a frost treatment system operating according to this method

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