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DE3378137D1 - Air intake system for engine - Google Patents

Air intake system for engine

Info

Publication number
DE3378137D1
DE3378137D1 DE8383304390T DE3378137T DE3378137D1 DE 3378137 D1 DE3378137 D1 DE 3378137D1 DE 8383304390 T DE8383304390 T DE 8383304390T DE 3378137 T DE3378137 T DE 3378137T DE 3378137 D1 DE3378137 D1 DE 3378137D1
Authority
DE
Germany
Prior art keywords
engine
air intake
intake system
air
intake
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
Application number
DE8383304390T
Other languages
English (en)
Inventor
Frederick Lewis Gilbertson
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.)
Bombardier Inc
Original Assignee
De Havilland Aircraft of Canada 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
Application filed by De Havilland Aircraft of Canada Ltd filed Critical De Havilland Aircraft of Canada Ltd
Application granted granted Critical
Publication of DE3378137D1 publication Critical patent/DE3378137D1/de
Expired 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—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
    • 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; 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
    • B64D2033/022—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections
    • 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
    • B64D2033/0293—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 turboprop engines
    • 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)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
DE8383304390T 1982-08-17 1983-07-29 Air intake system for engine Expired DE3378137D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA000409600A CA1201894A (en) 1982-08-17 1982-08-17 Air intake system for engine

Publications (1)

Publication Number Publication Date
DE3378137D1 true DE3378137D1 (en) 1988-11-03

Family

ID=4123425

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8383304390T Expired DE3378137D1 (en) 1982-08-17 1983-07-29 Air intake system for engine

Country Status (3)

Country Link
EP (1) EP0103384B1 (de)
CA (1) CA1201894A (de)
DE (1) DE3378137D1 (de)

Families Citing this family (15)

* 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
GB2203801B (en) * 1987-04-14 1991-11-27 Rolls Royce Plc A gas turbine engine
US4938021A (en) * 1988-10-27 1990-07-03 Sundstrand Corporation Sustainer propulsion system
US5123240A (en) * 1990-03-19 1992-06-23 General Electric Co. Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine
GB2259328B (en) * 1991-09-03 1995-07-19 Gen Electric Gas turbine engine variable bleed pivotal flow splitter
GB9906621D0 (en) 1999-03-23 1999-05-19 British Aerospace Vehicle propulsion systems
RU2174616C2 (ru) * 1999-09-21 2001-10-10 Государственное унитарное предприятие "Завод им. В.Я. Климова" - дочернее предприятие государственного унитарного предприятия Военно-промышленный комплекс "МАПО" Входное устройство для турбовинтового двигателя
RU2189474C1 (ru) * 2000-12-27 2002-09-20 Общество с ограниченной ответственностью "Проектно-конструкторское бюро "Энергия" Способ подачи и отвода потока очищенного охлаждающего воздуха к турбогенератору
DE602005017810D1 (de) * 2004-09-15 2009-12-31 Ntt Docomo Inc Mobilkommunikationssystem, drahtlose steuerstation, drahtlose basisstation, mobilstation und mobilkommunikationsverfahren
EP1674694B1 (de) * 2004-12-23 2014-02-12 Rolls-Royce plc Saugkanal für einen Verdichter
DE602008004790D1 (de) * 2008-11-28 2011-03-10 Alcatel Lucent Ausrüstungsschutzverfahren und -vorrichtung
US20120070271A1 (en) 2010-09-21 2012-03-22 Urban Justin R Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events
US9500129B2 (en) 2012-10-29 2016-11-22 Honeywell International Inc. Turboshaft engines having improved inlet particle scavenge systems and methods for the manufacture thereof
FR3039209B1 (fr) * 2015-07-23 2017-07-14 Snecma Manche d’entree d’air pour un turbopropulseur d’aeronef
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3329377A (en) * 1965-10-11 1967-07-04 United Aircraft Canada Protection for aircraft engines against snow, ice and airborne particles
US3371471A (en) * 1965-10-15 1968-03-05 Avco Corp Sand and dust collector for engine air inlets
US3952972A (en) * 1974-12-24 1976-04-27 United Aircraft Of Canada Limited Inertial separator

Also Published As

Publication number Publication date
EP0103384B1 (de) 1988-09-28
EP0103384A3 (en) 1984-07-11
CA1201894A (en) 1986-03-18
EP0103384A2 (de) 1984-03-21

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: BOEING CANADA TECHNOLOGY LTD., DOWNSVIEW, ONTARIO,

8327 Change in the person/name/address of the patent owner

Owner name: BOEING OF CANADA LTD., DOWNSVIEW, ONTARIO, CA

8327 Change in the person/name/address of the patent owner

Owner name: DE HAVILLAND INC., DOWNSVIEW, ONTARIO, CA