FR1016933A - Anti-icing device, for compressors of aircraft turbo-engines - Google Patents

Anti-icing device, for compressors of aircraft turbo-engines

Info

Publication number
FR1016933A
FR1016933A FR1016933DA FR1016933A FR 1016933 A FR1016933 A FR 1016933A FR 1016933D A FR1016933D A FR 1016933DA FR 1016933 A FR1016933 A FR 1016933A
Authority
FR
France
Prior art keywords
compressors
engines
icing device
aircraft turbo
turbo
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
Other languages
French (fr)
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.)
Canadian Patents and Development Ltd
Original Assignee
Canadian Patents and Development 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 Canadian Patents and Development Ltd filed Critical Canadian Patents and Development Ltd
Application granted granted Critical
Publication of FR1016933A publication Critical patent/FR1016933A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1016933D 1948-11-18 1950-01-27 Anti-icing device, for compressors of aircraft turbo-engines Expired FR1016933A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB29948/48A GB655784A (en) 1948-11-18 1948-11-18 Means for anti-icing of compressors

Publications (1)

Publication Number Publication Date
FR1016933A true FR1016933A (en) 1952-11-26

Family

ID=10299804

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1016933D Expired FR1016933A (en) 1948-11-18 1950-01-27 Anti-icing device, for compressors of aircraft turbo-engines

Country Status (3)

Country Link
US (1) US2655308A (en)
FR (1) FR1016933A (en)
GB (1) GB655784A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2723761A1 (en) * 1994-08-18 1996-02-23 Snecma TURBOREACTOR EQUIPPED WITH A DEFROST SYSTEM ON THE INPUT HOUSING

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3057154A (en) * 1959-07-07 1962-10-09 Rolls Royce De-icer system for a gas turbine engine
DE1184560B (en) * 1960-03-14 1964-12-31 Rolls Royce Heat exchangers, in particular for de-icing inlet struts for gas turbine engines
US4406431A (en) * 1981-11-23 1983-09-27 Omac, Inc. Air scoop lip warmer de-icing system
US4676454A (en) * 1985-05-11 1987-06-30 Thomas Zompolas Backup pump for aircraft instrument system including heater
DE4327376A1 (en) * 1993-08-14 1995-02-16 Abb Management Ag Compressor and method for its operation
GB2348466B (en) * 1999-03-27 2003-07-09 Rolls Royce Plc A gas turbine engine and a rotor for a gas turbine engine
US7246480B2 (en) * 2004-11-04 2007-07-24 Siemens Power Generation, Inc. System for heating an air intake of turbine engine
US8366047B2 (en) * 2005-05-31 2013-02-05 United Technologies Corporation Electrothermal inlet ice protection system
US8172521B2 (en) * 2009-01-15 2012-05-08 General Electric Company Compressor clearance control system using turbine exhaust
US8152457B2 (en) * 2009-01-15 2012-04-10 General Electric Company Compressor clearance control system using bearing oil waste heat
US9067679B2 (en) * 2011-12-30 2015-06-30 Aerospace Filtration Systems, Inc. Heated screen for air intake of aircraft engines
US10655539B2 (en) 2017-10-16 2020-05-19 Rolls-Royce North America Technologies Inc. Aircraft anti-icing system
US10947993B2 (en) * 2017-11-27 2021-03-16 General Electric Company Thermal gradient attenuation structure to mitigate rotor bow in turbine engine
US11879411B2 (en) 2022-04-07 2024-01-23 General Electric Company System and method for mitigating bowed rotor in a gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2268320A (en) * 1938-05-05 1941-12-30 Robert L Brandt Formation of thermal air currents
US2317019A (en) * 1941-01-27 1943-04-20 Altemus James Dobson De-icing device for airplane propellers, wings, and the like
US2409375A (en) * 1942-05-07 1946-10-15 Earl Hovey C Apparatus for contouring the ends of tubular stock
US2408867A (en) * 1942-07-22 1946-10-08 Mccollum Thelma Means for utilizing radiant heat in aircraft
US2446663A (en) * 1944-01-11 1948-08-10 Curtiss Wright Corp Fan deicing or anti-icing means
US2435990A (en) * 1945-08-17 1948-02-17 Westinghouse Electric Corp Gas turbine lubricating oil cooling and air inlet deicing system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2723761A1 (en) * 1994-08-18 1996-02-23 Snecma TURBOREACTOR EQUIPPED WITH A DEFROST SYSTEM ON THE INPUT HOUSING
US5623821A (en) * 1994-08-18 1997-04-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbojet equipped with a deicing system on the intake case

Also Published As

Publication number Publication date
GB655784A (en) 1951-08-01
US2655308A (en) 1953-10-13

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