IT8021276A0 - Sistema antighiaccio per ogiva di motore a turbina a gas. - Google Patents

Sistema antighiaccio per ogiva di motore a turbina a gas.

Info

Publication number
IT8021276A0
IT8021276A0 IT8021276A IT2127680A IT8021276A0 IT 8021276 A0 IT8021276 A0 IT 8021276A0 IT 8021276 A IT8021276 A IT 8021276A IT 2127680 A IT2127680 A IT 2127680A IT 8021276 A0 IT8021276 A0 IT 8021276A0
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
ice system
engine nose
nose
Prior art date
Application number
IT8021276A
Other languages
English (en)
Other versions
IT1141553B (it
Inventor
Moore Alan
Harman Geoffrey Edward
Rosser David Gavin
Clapham Edward Faulconbridge
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of IT8021276A0 publication Critical patent/IT8021276A0/it
Application granted granted Critical
Publication of IT1141553B publication Critical patent/IT1141553B/it

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

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)
IT21276/80A 1979-04-17 1980-04-09 Sistema antighiaccio per ogiva di motore a turbina a gas IT1141553B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7913292A GB2046843B (en) 1979-04-17 1979-04-17 Gas turbine engines-de-icing-icing

Publications (2)

Publication Number Publication Date
IT8021276A0 true IT8021276A0 (it) 1980-04-09
IT1141553B IT1141553B (it) 1986-10-01

Family

ID=10504589

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21276/80A IT1141553B (it) 1979-04-17 1980-04-09 Sistema antighiaccio per ogiva di motore a turbina a gas

Country Status (6)

Country Link
US (2) US4485619A (it)
JP (1) JPS55139935A (it)
DE (1) DE3013974C2 (it)
FR (1) FR2454522B1 (it)
GB (1) GB2046843B (it)
IT (1) IT1141553B (it)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2621554B1 (fr) * 1987-10-07 1990-01-05 Snecma Capot d'entree non tournant de turboreacteur a fixation centrale et turboreacteur ainsi equipe
GB2217393B (en) * 1988-04-14 1992-07-08 Rolls Royce Plc Nose bullet anti-icing for gas turbine engines
US5088277A (en) * 1988-10-03 1992-02-18 General Electric Company Aircraft engine inlet cowl anti-icing system
US5240069A (en) * 1992-07-06 1993-08-31 The United States Of America As Represented By The Secretary Of The Air Force Integral cooling system for a jet engine integral starter/generator and the like
FR2705996B1 (fr) * 1993-06-03 1995-07-07 Snecma Système de dégivrage des parties avant d'une turbomachine.
US20030228267A1 (en) * 2001-07-09 2003-12-11 Aust Duncan T. Suncreen composition wit enhanced spf and water resistant properties
CA2456563C (en) * 2004-01-30 2011-12-20 Pratt & Whitney Canada Corp. Anti-icing apparatus and method for aero-engine nose cone
FR2898939B1 (fr) * 2006-03-22 2008-05-09 Snecma Sa Systeme de degivrage d'un cone d'entree de turbomoteur pour aeronef
US7823374B2 (en) * 2006-08-31 2010-11-02 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7938368B2 (en) 2008-04-07 2011-05-10 United Technologies Corporation Nosecone ice protection system for a gas turbine engine
FR2998620B1 (fr) * 2012-11-29 2018-04-06 Safran Aircraft Engines Capot de turbomachine apte a recouvrir un cone de soufflante
WO2014204546A2 (en) 2013-04-03 2014-12-24 United Technologies Corporation Gas turbine engine de-icing system
FR3034401B1 (fr) * 2015-03-31 2018-07-27 Safran Aircraft Engines Systeme et procede de degivrage d'un cone d'entree de turbomachine
JP6666159B2 (ja) * 2016-01-21 2020-03-13 三菱航空機株式会社 防氷装置、及び、航空機
US10612557B2 (en) * 2016-07-15 2020-04-07 Rolls-Royce Corporation Nose cone attachment for turbofan engine
US10393019B2 (en) * 2016-07-28 2019-08-27 Pratt & Whitney Canada Corp. Assembly and method for influencing flow through a fan of a gas turbine engine
DE102021116507A1 (de) 2021-06-25 2022-12-29 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1018538A (en) * 1964-07-06 1966-01-26 Rolls Royce Gas turbine engine
FR2168938B1 (it) * 1972-01-27 1974-12-13 Snecma
US3834157A (en) * 1973-02-05 1974-09-10 Avco Corp Spinner de-icing for gas turbine engines
US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
US3830058A (en) * 1973-02-26 1974-08-20 Avco Corp Fan engine mounting
US3925979A (en) * 1973-10-29 1975-12-16 Gen Electric Anti-icing system for a gas turbine engine
US3905191A (en) * 1974-04-10 1975-09-16 Avco Corp Gas turbine engine with efficient annular bleed manifold
GB2038425B (en) * 1978-12-27 1982-12-01 Rolls Royce Gas turbine engine

Also Published As

Publication number Publication date
FR2454522B1 (fr) 1985-07-19
GB2046843B (en) 1983-01-26
JPS577291B2 (it) 1982-02-09
JPS55139935A (en) 1980-11-01
FR2454522A1 (fr) 1980-11-14
DE3013974A1 (de) 1980-10-23
DE3013974C2 (de) 1982-06-16
US4546604A (en) 1985-10-15
GB2046843A (en) 1980-11-19
US4485619A (en) 1984-12-04
IT1141553B (it) 1986-10-01

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