FR2906569B1 - VERSATILE RADIAL AIR INTAKE OF A TURBOMOTOR. - Google Patents

VERSATILE RADIAL AIR INTAKE OF A TURBOMOTOR.

Info

Publication number
FR2906569B1
FR2906569B1 FR0608569A FR0608569A FR2906569B1 FR 2906569 B1 FR2906569 B1 FR 2906569B1 FR 0608569 A FR0608569 A FR 0608569A FR 0608569 A FR0608569 A FR 0608569A FR 2906569 B1 FR2906569 B1 FR 2906569B1
Authority
FR
France
Prior art keywords
turbomotor
versatile
air intake
radial air
radial
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 - Fee Related
Application number
FR0608569A
Other languages
French (fr)
Other versions
FR2906569A1 (en
Inventor
Marc Colaprisco
Daniel Chaniot
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.)
Airbus Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0608569A priority Critical patent/FR2906569B1/en
Publication of FR2906569A1 publication Critical patent/FR2906569A1/en
Application granted granted Critical
Publication of FR2906569B1 publication Critical patent/FR2906569B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0246—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising particle separators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
FR0608569A 2006-09-28 2006-09-28 VERSATILE RADIAL AIR INTAKE OF A TURBOMOTOR. Expired - Fee Related FR2906569B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0608569A FR2906569B1 (en) 2006-09-28 2006-09-28 VERSATILE RADIAL AIR INTAKE OF A TURBOMOTOR.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0608569A FR2906569B1 (en) 2006-09-28 2006-09-28 VERSATILE RADIAL AIR INTAKE OF A TURBOMOTOR.

Publications (2)

Publication Number Publication Date
FR2906569A1 FR2906569A1 (en) 2008-04-04
FR2906569B1 true FR2906569B1 (en) 2012-02-24

Family

ID=38001652

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0608569A Expired - Fee Related FR2906569B1 (en) 2006-09-28 2006-09-28 VERSATILE RADIAL AIR INTAKE OF A TURBOMOTOR.

Country Status (1)

Country Link
FR (1) FR2906569B1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2282031B1 (en) 2009-07-02 2012-06-06 Eurocopter Deutschland GmbH Filtering device with integrated bypass for an air inlet
FR2952401B1 (en) 2009-11-12 2011-11-11 Eurocopter France AIR INTAKE OF AN AIRCRAFT TURBOMOTOR, AIRCRAFT PROVIDED WITH SUCH AIR INTAKE AND METHOD FOR OPTIMIZING THE OPERATION OF A TURBOMOTEUR OF AN AIRCRAFT USING AN AIR INTAKE
US9656760B2 (en) * 2013-11-07 2017-05-23 Sikorsky Aircraft Corporation Variable geometry helicopter engine inlet
US10221764B2 (en) 2014-08-19 2019-03-05 Pratt & Whitney Canada Corp. Variable geometry inlet system
US9951690B2 (en) 2014-08-19 2018-04-24 Pratt & Whitney Canada Corp. Low noise aeroengine inlet system
US10054050B2 (en) 2014-08-19 2018-08-21 Pratt & Whitney Canada Corp. Low noise aeroengine inlet system
US9957889B2 (en) 2014-08-19 2018-05-01 Pratt & Whitney Canada Corp. Low noise aeroengine inlet system
ITUB20152308A1 (en) * 2015-07-20 2017-01-20 Bmc Srl PROPELLER OF AN AIRCRAFT INCLUDING A SUCTION PIPE PROVIDED WITH AN AIR FILTER WITH OPENABLE BOTTOM AND ITS AIR FILTER
ITUB20152299A1 (en) * 2015-07-20 2017-01-20 Bmc Srl PROPELLER OF AN AIRCRAFT INCLUDING AN INTAKE PIPELINE PROVIDED WITH AN AIR FILTER AND BYPASS OPENING OF THE AIR FILTER
ITUB20154090A1 (en) * 2015-10-02 2017-04-02 Bmc Srl AIR INTAKE UNIT FOR THE PROPELLER OF AN AIRCRAFT
DE102015226305A1 (en) * 2015-12-21 2017-06-22 Siemens Aktiengesellschaft Gas turbine plant and method for operating a gas turbine plant
FR3111947B1 (en) 2020-06-30 2022-05-27 Airbus Helicopters self-cleaning media air filtration system and method for an aircraft engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3449891A (en) * 1966-11-15 1969-06-17 United Aircraft Corp Engine inlet air particle separator
US3483676A (en) * 1967-09-29 1969-12-16 Gen Electric Helicopter engine air inlets
US3534548A (en) * 1969-06-30 1970-10-20 Avco Corp Separator apparatus for engine air inlets
FR2250671B1 (en) * 1973-11-09 1980-01-04 Aerospatiale
US6595742B2 (en) * 2000-10-02 2003-07-22 Westar Corporation Aircraft engine air filter and method
US7192462B2 (en) * 2004-04-14 2007-03-20 Aerospace Filtration Systems, Inc. Engine air filter and sealing system

Also Published As

Publication number Publication date
FR2906569A1 (en) 2008-04-04

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