FR2284036A1 - Systeme d'admission de turbine a gaz - Google Patents

Systeme d'admission de turbine a gaz

Info

Publication number
FR2284036A1
FR2284036A1 FR7527309A FR7527309A FR2284036A1 FR 2284036 A1 FR2284036 A1 FR 2284036A1 FR 7527309 A FR7527309 A FR 7527309A FR 7527309 A FR7527309 A FR 7527309A FR 2284036 A1 FR2284036 A1 FR 2284036A1
Authority
FR
France
Prior art keywords
gas turbine
intake system
turbine intake
gas
turbine
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.)
Withdrawn
Application number
FR7527309A
Other languages
English (en)
French (fr)
Inventor
Gerhard Neumann
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2284036A1 publication Critical patent/FR2284036A1/fr
Withdrawn legal-status Critical Current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
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines

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)
FR7527309A 1974-09-06 1975-09-05 Systeme d'admission de turbine a gaz Withdrawn FR2284036A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/503,750 US3964569A (en) 1974-09-06 1974-09-06 Gas turbine engine noise shield

Publications (1)

Publication Number Publication Date
FR2284036A1 true FR2284036A1 (fr) 1976-04-02

Family

ID=24003356

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7527309A Withdrawn FR2284036A1 (fr) 1974-09-06 1975-09-05 Systeme d'admission de turbine a gaz

Country Status (5)

Country Link
US (1) US3964569A (enExample)
JP (1) JPS5153109A (enExample)
DE (1) DE2539297A1 (enExample)
FR (1) FR2284036A1 (enExample)
IT (1) IT1042130B (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2192234B (en) * 1986-07-02 1991-04-17 Rolls Royce Plc A turbofan gas turbine engine
US5702231A (en) * 1996-08-09 1997-12-30 The Boeing Company Apparatus and method for reducing noise emissions from a gas turbine engine inlet
US5915403A (en) * 1998-04-14 1999-06-29 The Boeing Company Biplanar scarfed nacelle inlet
US7246481B2 (en) * 2004-03-26 2007-07-24 General Electric Company Methods and apparatus for operating gas turbine engines
US7412832B2 (en) * 2004-03-26 2008-08-19 General Electric Company Method and apparatus for operating gas turbine engines
FR2896771B1 (fr) * 2006-01-27 2008-04-25 Snecma Sa Entree d'air de turboreacteur a double flux
DE102007019762A1 (de) * 2007-04-25 2008-10-30 Eads Deutschland Gmbh Schallschutzvorrichtung für ein Strahltriebwerk oder eine Turbine
US10040560B2 (en) * 2015-09-30 2018-08-07 The Boeing Company Trailing edge core compartment vent for an aircraft engine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2970431A (en) * 1959-01-02 1961-02-07 Curtiss Wright Corp Rotating inlet for jet engines
US3027710A (en) * 1960-10-10 1962-04-03 Stephen P Maytner Methods and apparatus for suppressing jet noise
US3545464A (en) * 1967-04-06 1970-12-08 Rolls Royce Air intake duct for a gas turbine engine
US3481427A (en) * 1968-11-29 1969-12-02 Mc Donnell Douglas Corp Acoustical panel structure
US3590944A (en) * 1969-04-17 1971-07-06 Rohr Corp Method and apparatus for suppressing the noise of jet-propelled aircraft
US3565208A (en) * 1970-02-02 1971-02-23 Rohr Corp Retractable silencing shield for jet engine nozzle
US3621933A (en) * 1970-07-27 1971-11-23 Rohr Corp Method and apparatus for suppressing the noise of an aircraft jet engine
US3717163A (en) * 1970-10-08 1973-02-20 Cci Aerospace Corp Precompression shroud for inlets
US3739984A (en) * 1971-08-25 1973-06-19 Rohr Industries Inc Thrust augmenting and south suppressing apparatus and method
GB1353678A (en) * 1971-09-15 1974-05-22 Rolls Royce Air intake for a gas turbine engine
FR2153180B1 (enExample) * 1971-09-23 1975-02-07 Snecma

Also Published As

Publication number Publication date
DE2539297A1 (de) 1976-03-18
IT1042130B (it) 1980-01-30
JPS5153109A (enExample) 1976-05-11
US3964569A (en) 1976-06-22

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Legal Events

Date Code Title Description
ST Notification of lapse