GB486549A - A new or improved apparatus for preventing ice formation on aircraft surfaces - Google Patents

A new or improved apparatus for preventing ice formation on aircraft surfaces

Info

Publication number
GB486549A
GB486549A GB33503/36A GB3350336A GB486549A GB 486549 A GB486549 A GB 486549A GB 33503/36 A GB33503/36 A GB 33503/36A GB 3350336 A GB3350336 A GB 3350336A GB 486549 A GB486549 A GB 486549A
Authority
GB
United Kingdom
Prior art keywords
aircraft
blower
tube
engine
heated air
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
GB33503/36A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB33503/36A priority Critical patent/GB486549A/en
Publication of GB486549A publication Critical patent/GB486549A/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
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application

Abstract

486,549. Preventing formation of ice on aircraft. HEADEN, L. A. Dec. 7, 1936, No. 33503. [Class 4] Apparatus for preventing ice formation on aircraft in which an air heater on the engine is in communication with a tube located in the leading portion of the aircraft surfaces comprises a blower C, Fig. 1, for forcing air heated from a muff A surrounding the engine exhaust manifold into tubes H, J located in the leading edges of the wings and formed with forwardly directed jet apertures such that the heated air is maintained at such a pressure in the tube that it is directed as jets against the interior of the leading edge parts K, Fig. 2. Blower C is driven by a windmill which, with its drive shaft, is readily detachable. Pipes H, J are formed in two lengths of differing diameter, H<1>, H2 and J<1>, J<2> respectively, formed with jet apertures H<3>, J<3> of increasing diameter or frequency outwardly. The aggregate cross-sectional areas of all the apertures are less than the mean cross-sectional area of the tube. The connection between the pipe portions may be telescopic to facilitate wing removal. A pipe L provided with a valve L<1> may be used to provide heated air to the cockpit. A byepass valve L<2> permits use of blower C for evacuating heated air from the neighbourhood of the engine in hot climates where wing heating is unnecessary.
GB33503/36A 1936-12-07 1936-12-07 A new or improved apparatus for preventing ice formation on aircraft surfaces Expired GB486549A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33503/36A GB486549A (en) 1936-12-07 1936-12-07 A new or improved apparatus for preventing ice formation on aircraft surfaces

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33503/36A GB486549A (en) 1936-12-07 1936-12-07 A new or improved apparatus for preventing ice formation on aircraft surfaces

Publications (1)

Publication Number Publication Date
GB486549A true GB486549A (en) 1938-06-07

Family

ID=10353804

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33503/36A Expired GB486549A (en) 1936-12-07 1936-12-07 A new or improved apparatus for preventing ice formation on aircraft surfaces

Country Status (1)

Country Link
GB (1) GB486549A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2507044A (en) * 1943-09-20 1950-05-09 Curtiss Wright Corp Deicing system for aircraft
US2514105A (en) * 1945-12-07 1950-07-04 Thomas Wilfred Airfoil conditioning means
EP0634985A1 (en) * 1993-02-09 1995-01-25 Grumman Aerospace Corporation Strain isolator assembly
CN101962076A (en) * 2010-09-15 2011-02-02 北京航空航天大学 Gas film ice prevention structure of leading edge of nacelle of airplane
WO2013091642A1 (en) * 2011-12-21 2013-06-27 Vestas Wind Systems A/S De-icing of a wind turbine blade
US20150108233A1 (en) * 2013-10-18 2015-04-23 The Boeing Company Anti-Icing System for Aircraft
EP3196123A1 (en) * 2016-01-21 2017-07-26 Mitsubishi Aircraft Corporation Anti-icing system and aircraft
EP3205580A1 (en) * 2016-02-12 2017-08-16 Mitsubishi Aircraft Corporation Anti-icing system and aircraft
EP3878750A1 (en) * 2020-03-12 2021-09-15 Rohr, Inc. Variable diameter piccolo tube for anti-icing system
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
US11577844B2 (en) 2020-03-12 2023-02-14 Rohr, Inc. Variable diameter piccolo tube for anti-icing system

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2507044A (en) * 1943-09-20 1950-05-09 Curtiss Wright Corp Deicing system for aircraft
US2514105A (en) * 1945-12-07 1950-07-04 Thomas Wilfred Airfoil conditioning means
EP0634985A1 (en) * 1993-02-09 1995-01-25 Grumman Aerospace Corporation Strain isolator assembly
EP0634985A4 (en) * 1993-02-09 1995-05-31 Grumman Aerospace Corp Strain isolator assembly.
CN101962076A (en) * 2010-09-15 2011-02-02 北京航空航天大学 Gas film ice prevention structure of leading edge of nacelle of airplane
WO2013091642A1 (en) * 2011-12-21 2013-06-27 Vestas Wind Systems A/S De-icing of a wind turbine blade
US10041477B2 (en) 2011-12-21 2018-08-07 Vestas Wind Systems A/S De-icing of a wind turbine blade
US20150108233A1 (en) * 2013-10-18 2015-04-23 The Boeing Company Anti-Icing System for Aircraft
US9764847B2 (en) * 2013-10-18 2017-09-19 The Boeing Company Anti-icing system for aircraft
US10589866B2 (en) 2016-01-21 2020-03-17 Mitsubishi Aircraft Corporation Anti-icing system and aircraft
EP3196123A1 (en) * 2016-01-21 2017-07-26 Mitsubishi Aircraft Corporation Anti-icing system and aircraft
EP3205580A1 (en) * 2016-02-12 2017-08-16 Mitsubishi Aircraft Corporation Anti-icing system and aircraft
US10889381B2 (en) 2016-02-12 2021-01-12 Mitsubishi Aircraft Corporation Anti-icing system and aircraft
EP3878750A1 (en) * 2020-03-12 2021-09-15 Rohr, Inc. Variable diameter piccolo tube for anti-icing system
US11577844B2 (en) 2020-03-12 2023-02-14 Rohr, Inc. Variable diameter piccolo tube for anti-icing system
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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