IT940595B - Schermo para fiamma per motore a turbina a gas - Google Patents

Schermo para fiamma per motore a turbina a gas

Info

Publication number
IT940595B
IT940595B IT31082/71A IT3108271A IT940595B IT 940595 B IT940595 B IT 940595B IT 31082/71 A IT31082/71 A IT 31082/71A IT 3108271 A IT3108271 A IT 3108271A IT 940595 B IT940595 B IT 940595B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engine
flame shield
flame
shield
Prior art date
Application number
IT31082/71A
Other languages
English (en)
Original Assignee
Secr Defence Brit
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 Secr Defence Brit filed Critical Secr Defence Brit
Application granted granted Critical
Publication of IT940595B publication Critical patent/IT940595B/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
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/62—Insulation or other protection; Elements or use of specified material therefor
    • E04B1/92—Protection against other undesired influences or dangers
    • E04B1/94—Protection against other undesired influences or dangers against fire
    • E04B1/941—Building elements specially adapted therefor
    • 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)
  • Architecture (AREA)
  • Electromagnetism (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Thermal Insulation (AREA)
  • Laminated Bodies (AREA)
IT31082/71A 1970-11-30 1971-11-13 Schermo para fiamma per motore a turbina a gas IT940595B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB56738/70A GB1291939A (en) 1970-11-30 1970-11-30 Flame shield for a gas turbine engine

Publications (1)

Publication Number Publication Date
IT940595B true IT940595B (it) 1973-02-20

Family

ID=10477412

Family Applications (1)

Application Number Title Priority Date Filing Date
IT31082/71A IT940595B (it) 1970-11-30 1971-11-13 Schermo para fiamma per motore a turbina a gas

Country Status (6)

Country Link
US (1) US3779006A (it)
JP (1) JPS5717165B1 (it)
DE (1) DE2158307C3 (it)
FR (1) FR2115184B1 (it)
GB (1) GB1291939A (it)
IT (1) IT940595B (it)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4068470A (en) * 1974-11-08 1978-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with convertible accessories
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
DE3111596A1 (de) * 1981-03-24 1982-10-07 G + H Montage Gmbh, 6700 Ludwigshafen Hitzbestaendig ausgekleidete, verformungen ausgesetzte wand, sowie blanket hierfuer
JPS5941884A (ja) * 1982-08-31 1984-03-08 Fujitsu Ltd 半導体発光装置
JPS6041066U (ja) * 1983-08-30 1985-03-23 日本電気株式会社 光半導体装置
JPS60111219A (ja) * 1983-11-22 1985-06-17 Toshiba Corp コリメ−ト光学装置
GB2151544B (en) * 1983-12-21 1987-04-15 Rolls Royce Method of manufacture of a non-metallic laminate
DE3481290D1 (de) * 1984-01-09 1990-03-15 Boeing Co Kompositmaterialstruktur mit vollem feuerschutz.
DE3446649A1 (de) * 1984-12-20 1986-06-26 G + H Montage Gmbh, 6700 Ludwigshafen Auskleidung fuer hochtemperatur-gasturbinen
FR2633667B1 (fr) * 1988-06-30 1991-02-08 Snecma Dispositif de prelevement d'air dans la veine secondaire d'un turboreacteur
GB8917709D0 (en) * 1989-08-02 1989-09-20 Insumat Ltd Gas turbine engine flame breakout shields
US5264244A (en) * 1991-12-20 1993-11-23 United Technologies Corporation Inhibiting coke formation by coating gas turbine elements with alumina
US5336560A (en) * 1991-12-20 1994-08-09 United Technologies Corporation Gas turbine elements bearing alumina-silica coating to inhibit coking
US5269137A (en) * 1991-12-20 1993-12-14 United Technologies Corporation Gas turbine elements bearing coke inhibiting coatings of alumina
US5324544A (en) * 1991-12-20 1994-06-28 United Technologies Corporation Inhibiting coke formation by coating gas turbine elements with alumina-silica sol gel
RU2115812C1 (ru) * 1994-02-16 1998-07-20 Юнайтед Технолоджиз Корпорейшн Способ и устройство удержания расплавленного материала в процессе горения в газотурбинном двигателе (варианты)
US5910094A (en) * 1996-09-10 1999-06-08 The Boeing Company Aircraft labyrinth fire seal
GB2435918B (en) * 2006-03-10 2008-05-14 Siemens Magnet Technology Ltd Thermal diffusion barrier
US7918081B2 (en) 2006-12-19 2011-04-05 United Technologies Corporation Flame prevention device
US8222165B2 (en) * 2008-10-27 2012-07-17 Pratt & Whitney Canada Corp. Composite fire shield
FR2979829B1 (fr) * 2011-09-09 2013-09-27 Astrium Sas Bouclier pare flamme perfectionne
US8425836B1 (en) * 2011-11-16 2013-04-23 Rolls-Royce Plc Chromium alloy
BR112015016935B1 (pt) * 2013-01-15 2022-01-11 United Technologies Corporation Motor de turbina a gás, e, método para fornecer proteção contra fogo para uma unidade de potência auxiliar
FR3014841B1 (fr) 2013-12-17 2017-12-08 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage
FR3014840B1 (fr) 2013-12-17 2017-10-13 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage
FR3015431B1 (fr) * 2013-12-19 2017-12-15 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
US20180237120A1 (en) * 2017-02-22 2018-08-23 General Electric Company Aircraft with Under Wing Direct Drive Low Pressure Turbine
US11421627B2 (en) * 2017-02-22 2022-08-23 General Electric Company Aircraft and direct drive engine under wing installation
US10920613B2 (en) * 2018-09-05 2021-02-16 Raytheon Technologies Corporation Retention system for improved fire protection
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711631A (en) * 1949-06-21 1955-06-28 Hartford Nat Bank & Trust Co Gas turbine power plant
US2706382A (en) * 1949-07-09 1955-04-19 Carborundum Co Devices for confinement and release of high velocity, hot gases
US2805192A (en) * 1954-05-28 1957-09-03 Gen Electric Plated refractory metals
GB868197A (en) * 1956-09-28 1961-05-17 Rolls Royce Improvements in or relating to protective arrangements for use with rotating parts
US3122883A (en) * 1959-11-20 1964-03-03 Thompson Ramo Wooldridge Inc Heat resistant wall structure for rocket motor nozzles and the like
US3264135A (en) * 1962-11-28 1966-08-02 Noel T Wakelyn Method of coating carbonaceous base to prevent oxidation destruction and coated base
US3321922A (en) * 1964-10-29 1967-05-30 Jr William T Latto Small rocket engine
US3357657A (en) * 1966-04-27 1967-12-12 Mc Donnell Douglas Corp Fire barrier
US3460759A (en) * 1967-03-07 1969-08-12 Nasa Combustion chamber
GB1245415A (en) * 1968-09-13 1971-09-08 Rolls Royce Improvements in or relating to fluid flow machines

Also Published As

Publication number Publication date
FR2115184B1 (it) 1975-02-21
JPS5717165B1 (it) 1982-04-09
US3779006A (en) 1973-12-18
DE2158307B2 (de) 1978-05-24
DE2158307A1 (de) 1972-09-07
DE2158307C3 (de) 1979-01-18
GB1291939A (en) 1972-10-04
FR2115184A1 (it) 1972-07-07

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