GB1032681A - Ice protection systems for aerofoil surfaces - Google Patents

Ice protection systems for aerofoil surfaces

Info

Publication number
GB1032681A
GB1032681A GB17495/61A GB1749561A GB1032681A GB 1032681 A GB1032681 A GB 1032681A GB 17495/61 A GB17495/61 A GB 17495/61A GB 1749561 A GB1749561 A GB 1749561A GB 1032681 A GB1032681 A GB 1032681A
Authority
GB
United Kingdom
Prior art keywords
aerofoil
spanwise
chord
protection systems
jets
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
GB17495/61A
Inventor
John Rendall Conrad Pedersen
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 GB17495/61A priority Critical patent/GB1032681A/en
Publication of GB1032681A publication Critical patent/GB1032681A/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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

1,032,681. De-icing equipment for aerofoils. D. NAPIER & SON Ltd. May 10, 1962 [May 12, 1961], No. 17495/61. Heading B7W. In an aerofoil hot gases flow from a spanwise manifold 11 through a slot 12 into a passage 13 where it heats outer skin 14, the gas escaping the rough spanwise jets 18, 19 placed near the limit of catch, i.e. the rearmost point along a chord of an aerofoil at which water is collected, and is aft of the leading edge by about 15% of the chord. The jets remove water flowing over the aerofoil surface and may be adjustable in width and angle at which the gas is discharged, Fig. 2, not shown.
GB17495/61A 1961-05-12 1961-05-12 Ice protection systems for aerofoil surfaces Expired GB1032681A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB17495/61A GB1032681A (en) 1961-05-12 1961-05-12 Ice protection systems for aerofoil surfaces

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB17495/61A GB1032681A (en) 1961-05-12 1961-05-12 Ice protection systems for aerofoil surfaces

Publications (1)

Publication Number Publication Date
GB1032681A true GB1032681A (en) 1966-06-15

Family

ID=10096173

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17495/61A Expired GB1032681A (en) 1961-05-12 1961-05-12 Ice protection systems for aerofoil surfaces

Country Status (1)

Country Link
GB (1) GB1032681A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
FR2637251A1 (en) * 1989-09-27 1990-04-06 Gen Electric Anti-icing device for the intake cowl of an aircraft engine
US6467730B2 (en) * 2000-01-17 2002-10-22 Dassault Aviation Aircraft airfoil leading edge member equipped with a de-icing device
CN113602503A (en) * 2021-08-31 2021-11-05 中国商用飞机有限责任公司 Flute venturi tube, aircraft defroster and aircraft
CN113844659A (en) * 2021-09-30 2021-12-28 中航通飞华南飞机工业有限公司 Double-skin anti-icing cavity structure of airplane and heat exchange method

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
FR2637251A1 (en) * 1989-09-27 1990-04-06 Gen Electric Anti-icing device for the intake cowl of an aircraft engine
US6467730B2 (en) * 2000-01-17 2002-10-22 Dassault Aviation Aircraft airfoil leading edge member equipped with a de-icing device
CN113602503A (en) * 2021-08-31 2021-11-05 中国商用飞机有限责任公司 Flute venturi tube, aircraft defroster and aircraft
CN113602503B (en) * 2021-08-31 2022-10-28 中国商用飞机有限责任公司 Flute-shaped pipe, aircraft deicing device and aircraft
CN113844659A (en) * 2021-09-30 2021-12-28 中航通飞华南飞机工业有限公司 Double-skin anti-icing cavity structure of airplane and heat exchange method

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