GB664286A - Electrically heated aircraft de-icing means - Google Patents

Electrically heated aircraft de-icing means

Info

Publication number
GB664286A
GB664286A GB9740/49A GB974049A GB664286A GB 664286 A GB664286 A GB 664286A GB 9740/49 A GB9740/49 A GB 9740/49A GB 974049 A GB974049 A GB 974049A GB 664286 A GB664286 A GB 664286A
Authority
GB
United Kingdom
Prior art keywords
skin
aircraft
electrically heated
icing means
bars
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
GB9740/49A
Inventor
Sydney Lucas
John Archibald Baines
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.)
Lucas Support Services Ltd
Original Assignee
Rotax 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 Rotax Ltd filed Critical Rotax Ltd
Priority to GB9740/49A priority Critical patent/GB664286A/en
Publication of GB664286A publication Critical patent/GB664286A/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

Landscapes

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

Abstract

664,286. De-icing aircraft by electric heating. ROTAX, Ltd. March 10, 1950 [April 11, 1949], No. 9740/49. Class 39(iii) The wing a or other metal skin of an aircraft has on its rear side metal studs c connecting the skin at adjacent points to at least two bus-bars b, so that a current may be passed through the skin for deicing. The studs c are welded to the skin and to a pair of metal strips or perforated aluminium plates b arranged parallel with each other and with the skin to form the bus-bars.
GB9740/49A 1949-04-11 1949-04-11 Electrically heated aircraft de-icing means Expired GB664286A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9740/49A GB664286A (en) 1949-04-11 1949-04-11 Electrically heated aircraft de-icing means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9740/49A GB664286A (en) 1949-04-11 1949-04-11 Electrically heated aircraft de-icing means

Publications (1)

Publication Number Publication Date
GB664286A true GB664286A (en) 1952-01-02

Family

ID=9877861

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9740/49A Expired GB664286A (en) 1949-04-11 1949-04-11 Electrically heated aircraft de-icing means

Country Status (1)

Country Link
GB (1) GB664286A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2559618A3 (en) * 2007-12-21 2016-10-05 Goodrich Corporation Ice protection system for a multi-segment aircraft component

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2559618A3 (en) * 2007-12-21 2016-10-05 Goodrich Corporation Ice protection system for a multi-segment aircraft component
EP3333081A1 (en) * 2007-12-21 2018-06-13 Goodrich Corporation Ice protection system for a multi-segment aircraft component

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