JPS6340254B2 - - Google Patents

Info

Publication number
JPS6340254B2
JPS6340254B2 JP57203522A JP20352282A JPS6340254B2 JP S6340254 B2 JPS6340254 B2 JP S6340254B2 JP 57203522 A JP57203522 A JP 57203522A JP 20352282 A JP20352282 A JP 20352282A JP S6340254 B2 JPS6340254 B2 JP S6340254B2
Authority
JP
Japan
Prior art keywords
air intake
turbine engine
gas turbine
duct
wall portion
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
JP57203522A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5893938A (ja
Inventor
Rarufu Pero Terensu
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.)
ROORUSU ROISU PLC
Original Assignee
ROORUSU ROISU PLC
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 ROORUSU ROISU PLC filed Critical ROORUSU ROISU PLC
Publication of JPS5893938A publication Critical patent/JPS5893938A/ja
Publication of JPS6340254B2 publication Critical patent/JPS6340254B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/022Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0293Arrangements 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

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)
  • Output Control And Ontrol Of Special Type Engine (AREA)
JP57203522A 1981-11-21 1982-11-19 ガスタービンエンジン圧縮機用エアインテーク Granted JPS5893938A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8135122 1981-11-21
GB8135122 1981-11-21

Publications (2)

Publication Number Publication Date
JPS5893938A JPS5893938A (ja) 1983-06-03
JPS6340254B2 true JPS6340254B2 (US20110009641A1-20110113-C00116.png) 1988-08-10

Family

ID=10526053

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57203522A Granted JPS5893938A (ja) 1981-11-21 1982-11-19 ガスタービンエンジン圧縮機用エアインテーク

Country Status (6)

Country Link
US (1) US4713934A (US20110009641A1-20110113-C00116.png)
JP (1) JPS5893938A (US20110009641A1-20110113-C00116.png)
CA (1) CA1205295A (US20110009641A1-20110113-C00116.png)
DE (1) DE3242248C2 (US20110009641A1-20110113-C00116.png)
FR (1) FR2516979B1 (US20110009641A1-20110113-C00116.png)
IT (1) IT1153044B (US20110009641A1-20110113-C00116.png)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0198044U (US20110009641A1-20110113-C00116.png) * 1987-12-22 1989-06-29

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5725180A (en) * 1995-12-29 1998-03-10 General Electric Company Aircraft engine pitot plenum intake
USD433029S (en) * 1999-06-10 2000-10-31 Ross Eidson Jet engine intake deflection guard
DE102012023718A1 (de) * 2012-12-05 2014-06-05 Eads Deutschland Gmbh Einlauf für ein Triebwerk eines Luftfahrzeugs
US10589869B2 (en) 2018-07-25 2020-03-17 General Electric Company Nacelle inlet lip fuse structure
US11499478B2 (en) * 2020-11-19 2022-11-15 Honeywell International Inc. Asymmetric inlet particle separator for gas turbine engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2802618A (en) * 1953-06-29 1957-08-13 Gen Motors Corp Foreign object separator
US3148043A (en) * 1962-03-29 1964-09-08 Boeing Co Moisture and particle removing means for engines
US3329377A (en) * 1965-10-11 1967-07-04 United Aircraft Canada Protection for aircraft engines against snow, ice and airborne particles
US3324999A (en) * 1965-10-23 1967-06-13 Reynolds Metals Co Container and blanks for making same
US3952972A (en) * 1974-12-24 1976-04-27 United Aircraft Of Canada Limited Inertial separator
US3971218A (en) * 1974-12-26 1976-07-27 Delaval Turbine Inc. Means for preventing an engine turbocharger from being damaged by foreign objects
US4250703A (en) * 1979-03-15 1981-02-17 Avco Corporation Swinging door particle separator and deicing system
US4354346A (en) * 1979-05-24 1982-10-19 British Aerospace Intake ducts for aircraft jet propulsion plant
CA1116418A (en) * 1979-07-18 1982-01-19 Pratt & Whitney Aircraft Of Canada Limited Vane fairing for inertial separator
US4378069A (en) * 1981-04-21 1983-03-29 Magna Technologies, Inc. Pouch with pour spout

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0198044U (US20110009641A1-20110113-C00116.png) * 1987-12-22 1989-06-29

Also Published As

Publication number Publication date
IT8224279A0 (it) 1982-11-16
DE3242248A1 (de) 1983-06-01
IT1153044B (it) 1987-01-14
DE3242248C2 (de) 1984-08-23
FR2516979B1 (fr) 1986-08-22
JPS5893938A (ja) 1983-06-03
CA1205295A (en) 1986-06-03
US4713934A (en) 1987-12-22
IT8224279A1 (it) 1984-05-16
FR2516979A1 (fr) 1983-05-27

Similar Documents

Publication Publication Date Title
CA1229494A (en) Aircraft engine air intake including a foreign object separator
US5139545A (en) Air intakes for gas turbine engines
JP2877345B2 (ja) 内部冷却タービンブレード及び内部冷却タービンブレード用塵埃除去装置
US3720045A (en) Dynamic blade particle separator
US3483676A (en) Helicopter engine air inlets
CA2209881C (en) Apparatus and method for reducing noise emissions from a gas turbine engine inlet
US5906334A (en) Aircraft intake method
GB2114233A (en) Containment shell for a fan section of a gas turbine engine
EP0241404A2 (en) Gas turbine engine nacelle
US20080253881A1 (en) Engine
EP1793086A2 (en) Turbine blade
GB2131882A (en) Gas turbine engine air inlet particle separator
JPS5857616B2 (ja) ガスタ−ビンエンジン吸気部
US4425756A (en) Gas turbine engine and its associated air intake system
US2802618A (en) Foreign object separator
JPH05193587A (ja) 円弧輪郭を有する航空機エンジンナセル
JPS6340254B2 (US20110009641A1-20110113-C00116.png)
US6116015A (en) Breather outlet
GR3002607T3 (en) Turbine thrust reverser having a device for re-orientating the gas flow
US3513641A (en) Foreign particle separator for an air moving member
EP0439923A1 (en) Gearbox breather outlet
US6948457B2 (en) Fan arrangement of a portable handheld work apparatus driven by an internal combustion engine
EP0074068A1 (en) Cooling device of automotive alternator
JPS6035199A (ja) 送風機のインペラ
GB2109865A (en) Gas turbine engine compressor air intake