IT8119377A0 - Presa d'aria per motore a turbina a gas. - Google Patents

Presa d'aria per motore a turbina a gas.

Info

Publication number
IT8119377A0
IT8119377A0 IT8119377A IT1937781A IT8119377A0 IT 8119377 A0 IT8119377 A0 IT 8119377A0 IT 8119377 A IT8119377 A IT 8119377A IT 1937781 A IT1937781 A IT 1937781A IT 8119377 A0 IT8119377 A0 IT 8119377A0
Authority
IT
Italy
Prior art keywords
gas turbine
air intake
turbine engine
engine
intake
Prior art date
Application number
IT8119377A
Other languages
English (en)
Other versions
IT1135210B (it
Inventor
John Richard Hobbs
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 IT8119377A0 publication Critical patent/IT8119377A0/it
Application granted granted Critical
Publication of IT1135210B publication Critical patent/IT1135210B/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
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/052—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with dust-separation devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Separating Particles In Gases By Inertia (AREA)
  • Exhaust Silencers (AREA)
IT19377/81A 1980-02-09 1981-01-28 Presa d'aria per motore a turbina a gas IT1135210B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8004401A GB2069053B (en) 1980-02-09 1980-02-09 Water separator in gas turbine inlet

Publications (2)

Publication Number Publication Date
IT8119377A0 true IT8119377A0 (it) 1981-01-28
IT1135210B IT1135210B (it) 1986-08-20

Family

ID=10511232

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19377/81A IT1135210B (it) 1980-02-09 1981-01-28 Presa d'aria per motore a turbina a gas

Country Status (7)

Country Link
US (1) US4493185A (it)
JP (1) JPS5924253B2 (it)
CA (1) CA1166026A (it)
DE (1) DE3103603C2 (it)
FR (1) FR2475627B1 (it)
GB (1) GB2069053B (it)
IT (1) IT1135210B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4685942A (en) * 1982-12-27 1987-08-11 General Electric Company Axial flow inlet particle separator
US4928480A (en) * 1988-03-04 1990-05-29 General Electric Company Separator having multiple particle extraction passageways
GB2509886B (en) * 1992-09-22 2015-03-18 Rolls Royce Plc Improvements in or relating to engine intake protection and supression of engine infra-red emissions
US5746789A (en) * 1995-11-28 1998-05-05 Innovatech, Inc. Apparatus for separating particulates from a fluid stream
US9003759B2 (en) * 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
EP2466097A1 (en) * 2005-06-20 2012-06-20 Rolls-Royce North American Technologies, Inc. Clustered inlet particle selector
JP4912805B2 (ja) * 2006-09-15 2012-04-11 公益財団法人鉄道総合技術研究所 磁気浮上式鉄道用地上コイルの異状検知センサ及びその異状検知システム
US7802433B2 (en) * 2006-09-27 2010-09-28 General Electric Company Adaptive inertial particle separators and methods of use
US7678165B2 (en) * 2006-12-28 2010-03-16 General Electric Company Particle separator using boundary layer control
US20080203218A1 (en) * 2007-02-26 2008-08-28 Honeywell International, Inc. Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area
FR2951503B1 (fr) * 2009-10-16 2011-11-18 Snecma Entree d air de moteur a turbine a gaz dans une nacelle
US8679210B2 (en) * 2012-01-17 2014-03-25 Hamilton Sundstrand Corporation Shrouded particle separator
US9631554B2 (en) * 2014-01-14 2017-04-25 Honeywell International Inc. Electrostatic charge control inlet particle separator system
FR3044357B1 (fr) * 2015-11-27 2020-06-05 Safran Aircraft Engines Turbomachine comprenant un piege de corps etrangers circulant dans un flux d'air

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2000741A (en) * 1933-10-26 1935-05-07 Gen Electric Fluid jet pump
FR1211340A (fr) * 1955-12-09 1960-03-15 Bristol Aeroplane Co Ltd Procédé et moyens pour éliminer l'humidité d'un courant gazeux
US3143043A (en) * 1961-04-03 1964-08-04 Holley Carburetor Co Spring biased diaphragm device
US3148043A (en) * 1962-03-29 1964-09-08 Boeing Co Moisture and particle removing means for engines
US3368332A (en) * 1963-07-30 1968-02-13 Boeing Co Foreign particle separator for an air moving member
US3477455A (en) * 1965-10-15 1969-11-11 Lockheed Aircraft Corp Supersonic inlet for jet engines
US3338049A (en) * 1966-02-01 1967-08-29 Gen Electric Gas turbine engine including separator for removing extraneous matter
US3616616A (en) * 1968-03-11 1971-11-02 Tech Dev Inc Particle separator especially for use in connection with jet engines
US3513641A (en) * 1968-08-22 1970-05-26 Boeing Co Foreign particle separator for an air moving member
DE2103035C3 (de) * 1970-02-05 1975-03-27 Secretary Of State For Defence Of The United Kingdom Of Great Britain And Northern Ireland, London Lufteinlaß für Gasturbinentriebwerke
FR2265615A1 (en) * 1974-03-28 1975-10-24 Bertin & Cie Protective device for helicopter engine air intake - extracts clean air from intake air and ejects dirt
US3977811A (en) * 1975-10-23 1976-08-31 Avco Corporation Air pump for use in dusty environment

Also Published As

Publication number Publication date
DE3103603A1 (de) 1982-01-07
FR2475627A1 (fr) 1981-08-14
GB2069053B (en) 1983-04-13
CA1166026A (en) 1984-04-24
US4493185A (en) 1985-01-15
FR2475627B1 (fr) 1986-05-23
IT1135210B (it) 1986-08-20
JPS5924253B2 (ja) 1984-06-08
DE3103603C2 (de) 1984-03-15
JPS56129723A (en) 1981-10-12
GB2069053A (en) 1981-08-19

Similar Documents

Publication Publication Date Title
IT8021936A0 (it) Presa d'aria ad asse incurvato per turbomotore a gas.
IT7926656A0 (it) Turbina raffreddata ad aria per motore a turbina a gas.
IT8321934A0 (it) Carburatore per turbomotore a gas.
IT8423443A0 (it) Complesso di combustione per motore a turbina a gas.
GB2019500B (en) Air manifold for a gas turbine engine
IT8321591A0 (it) Guarnizione di tenuta all'aria esterna rivestita in ceramica per motori a turbina a gas.
JPS5720539A (en) Exhaust nozzle for gas turbine engine
IT7921628A0 (it) Motore a turbina a gas.
IT7926822A0 (it) Tenuta per l'aria di raffreddamento di turbomotori a gas.
IT8020445A0 (it) Motore a turbina a gas.
ZA777122B (en) Inlet air cleaner assembly for turbine engines
GB2073325B (en) Gas turbine aircraft engine air intake
IT8119377A0 (it) Presa d'aria per motore a turbina a gas.
IT8119348A0 (it) Complesso di aspirazione per turbomotori a gas.
IT9020544A0 (it) apparato motore a turbogas
IT8021011A0 (it) Impianto di aspirazione dell'aria per un motore endotermico pluricilindrico.
IT8220226A0 (it) Motore a turbina a gas e suo sistema di presa d'aria associato.
IT8321090A0 (it) Prediffusore per motori a turbina a gas.
IT8521926A0 (it) Ugello di scarico orientabile per un motore a turbina a gas.
IT7830190A0 (it) Pre-depuratore d'aria per motori acombustione.
IT8025620A0 (it) Motore a turbina a gas modulare.
AU529701B2 (en) Inlet air cleaner for gas turbine engine
IT1098277B (it) Presa d'aria per combustori di turbine a gas
IT8224279A0 (it) Presa d'aria per motore a turbina a gas.
DE69006868T2 (de) Gasturbinenluftstrahltriebwerk.