FR2305595A1 - Dispositif pour empecher l'introduction, par aspiration, de corps etrangers dans un moteur a turbine a gaz d'un aeronef - Google Patents

Dispositif pour empecher l'introduction, par aspiration, de corps etrangers dans un moteur a turbine a gaz d'un aeronef

Info

Publication number
FR2305595A1
FR2305595A1 FR7509828A FR7509828A FR2305595A1 FR 2305595 A1 FR2305595 A1 FR 2305595A1 FR 7509828 A FR7509828 A FR 7509828A FR 7509828 A FR7509828 A FR 7509828A FR 2305595 A1 FR2305595 A1 FR 2305595A1
Authority
FR
France
Prior art keywords
aircraft
introduction
suction
prevent
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.)
Granted
Application number
FR7509828A
Other languages
English (en)
Other versions
FR2305595B1 (fr
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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
Priority to US05/561,869 priority Critical patent/US4004760A/en
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to FR7509828A priority patent/FR2305595A1/fr
Priority to DE2514551A priority patent/DE2514551C3/de
Publication of FR2305595A1 publication Critical patent/FR2305595A1/fr
Application granted granted Critical
Publication of FR2305595B1 publication Critical patent/FR2305595B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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—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
    • 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
    • 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—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
    • B64D2033/022—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
FR7509828A 1975-03-25 1975-03-28 Dispositif pour empecher l'introduction, par aspiration, de corps etrangers dans un moteur a turbine a gaz d'un aeronef Granted FR2305595A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US05/561,869 US4004760A (en) 1975-03-25 1975-03-25 Device for preventing foreign matters from being sucked into a gas turbine engine for an aircraft
FR7509828A FR2305595A1 (fr) 1975-03-25 1975-03-28 Dispositif pour empecher l'introduction, par aspiration, de corps etrangers dans un moteur a turbine a gaz d'un aeronef
DE2514551A DE2514551C3 (de) 1975-03-25 1975-04-03 Einlaufschutzvorrichtung des Ansaugens von Fremdkörpern in den Einlauf eines Flugzeugtriebwerkes

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US05/561,869 US4004760A (en) 1975-03-25 1975-03-25 Device for preventing foreign matters from being sucked into a gas turbine engine for an aircraft
FR7509828A FR2305595A1 (fr) 1975-03-25 1975-03-28 Dispositif pour empecher l'introduction, par aspiration, de corps etrangers dans un moteur a turbine a gaz d'un aeronef
DE2514551A DE2514551C3 (de) 1975-03-25 1975-04-03 Einlaufschutzvorrichtung des Ansaugens von Fremdkörpern in den Einlauf eines Flugzeugtriebwerkes

Publications (2)

Publication Number Publication Date
FR2305595A1 true FR2305595A1 (fr) 1976-10-22
FR2305595B1 FR2305595B1 (fr) 1980-01-04

Family

ID=27186330

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7509828A Granted FR2305595A1 (fr) 1975-03-25 1975-03-28 Dispositif pour empecher l'introduction, par aspiration, de corps etrangers dans un moteur a turbine a gaz d'un aeronef

Country Status (3)

Country Link
US (1) US4004760A (fr)
DE (1) DE2514551C3 (fr)
FR (1) FR2305595A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4337281A1 (de) * 1993-11-02 1995-05-04 Abb Management Ag Verdichter

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4230292A (en) * 1978-06-09 1980-10-28 The Garrett Corporation Propulsion/control for VTOL vehicle
GB2140090B (en) * 1982-12-23 1986-10-01 Rolls Royce Air intakes of helicopter mounted gas turbine engines
DE3635085A1 (de) * 1986-10-15 1988-06-16 Schmid Rudolf Martin Selbstreinigendes filter fuer gasfoermige medien kompakt-system mit staubeintrittsueberhoehung verfahren und ausfuehrung dazu
WO2001083297A2 (fr) * 2000-05-04 2001-11-08 Jangshik Yun Turbomoteur a gaz d'avion comportant une centrifugeuse
US6702873B2 (en) 2002-04-23 2004-03-09 The Boeing Company High particle separation efficiency system
US6764043B2 (en) * 2002-12-11 2004-07-20 The Boeing Company Rotatable scarf inlet for an aircraft engine and method of using the same
US6883751B2 (en) * 2003-05-02 2005-04-26 The Boeing Company Apparatus and method for preventing foreign object damage to an aircraft
DE102005007940A1 (de) * 2005-02-22 2006-08-24 Mtu Aero Engines Gmbh Triebwerk
US7491253B2 (en) * 2005-05-31 2009-02-17 Aerospace Filtrations Systems, Inc. Engine intake system with accessible, interchangeable air filters
US20070048122A1 (en) * 2005-08-30 2007-03-01 United Technologies Corporation Debris-filtering technique for gas turbine engine component air cooling system
US7625415B2 (en) * 2006-08-23 2009-12-01 Pratt & Whitney Canada Corp. Strainer for a gas turbine engine
US20080152500A1 (en) * 2006-12-20 2008-06-26 Carsten Mehring Inertial particle separator for compressor shroud bleed
US7927408B2 (en) 2007-11-30 2011-04-19 Honeywell International Inc. Inlet particle separator systems and methods
EP2379409B1 (fr) 2008-12-30 2017-12-20 Sikorsky Aircraft Corporation Séparateur de particules d'air pour moteur
US9249727B2 (en) * 2009-01-16 2016-02-02 Jeffrey A. Matos Retractable bird and debris deflector for an aircraft jet engine
US20100284791A1 (en) * 2009-05-11 2010-11-11 Robert Jesse Flores Apparatuses, systems, and methods for preventing foreign objects from being ingested into a jet engine
US8052083B1 (en) * 2009-09-17 2011-11-08 John Patrick Moran Bird deflector and air replacement system technical field
US8452516B1 (en) 2012-01-31 2013-05-28 United Technologies Corporation Variable vane scheduling based on flight conditions for inclement weather

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3400902A (en) * 1966-01-13 1968-09-10 Ben J. King Gas inlet conversion and protection means
US3338049A (en) * 1966-02-01 1967-08-29 Gen Electric Gas turbine engine including separator for removing extraneous matter
US3421296A (en) * 1966-11-15 1969-01-14 United Aircraft Corp Engine inlet air particle separator
US3733814A (en) * 1972-02-22 1973-05-22 Gen Electric Translatable engine inlet particle separator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4337281A1 (de) * 1993-11-02 1995-05-04 Abb Management Ag Verdichter

Also Published As

Publication number Publication date
DE2514551B2 (de) 1981-02-19
US4004760A (en) 1977-01-25
DE2514551A1 (de) 1976-10-07
FR2305595B1 (fr) 1980-01-04
DE2514551C3 (de) 1981-11-05

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Legal Events

Date Code Title Description
ST Notification of lapse