GB0018947D0 - Air intake duct - Google Patents

Air intake duct

Info

Publication number
GB0018947D0
GB0018947D0 GBGB0018947.2A GB0018947A GB0018947D0 GB 0018947 D0 GB0018947 D0 GB 0018947D0 GB 0018947 A GB0018947 A GB 0018947A GB 0018947 D0 GB0018947 D0 GB 0018947D0
Authority
GB
United Kingdom
Prior art keywords
air intake
intake duct
duct
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.)
Ceased
Application number
GBGB0018947.2A
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.)
BAE Systems PLC
Original Assignee
BAE Systems 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 BAE Systems PLC filed Critical BAE Systems PLC
Priority to GBGB0018947.2A priority Critical patent/GB0018947D0/en
Priority to PCT/GB2001/003332 priority patent/WO2002012690A1/en
Priority to AU2001272671A priority patent/AU2001272671A1/en
Publication of GB0018947D0 publication Critical patent/GB0018947D0/en
Ceased 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
    • F02C7/05—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
    • 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
    • B64D2033/022—Arrangements 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; 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
    • B64D2033/0266—Arrangements 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—Arrangements 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
GBGB0018947.2A 2000-08-03 2000-08-03 Air intake duct Ceased GB0018947D0 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GBGB0018947.2A GB0018947D0 (en) 2000-08-03 2000-08-03 Air intake duct
PCT/GB2001/003332 WO2002012690A1 (en) 2000-08-03 2001-07-24 Air intake duct
AU2001272671A AU2001272671A1 (en) 2000-08-03 2001-07-24 Air intake duct

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0018947.2A GB0018947D0 (en) 2000-08-03 2000-08-03 Air intake duct

Publications (1)

Publication Number Publication Date
GB0018947D0 true GB0018947D0 (en) 2001-08-08

Family

ID=9896829

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB0018947.2A Ceased GB0018947D0 (en) 2000-08-03 2000-08-03 Air intake duct

Country Status (3)

Country Link
AU (1) AU2001272671A1 (en)
GB (1) GB0018947D0 (en)
WO (1) WO2002012690A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1674694B1 (en) 2004-12-23 2014-02-12 Rolls-Royce plc Compressor intake duct
DE102012023718A1 (en) 2012-12-05 2014-06-05 Eads Deutschland Gmbh Inlet for an engine of an aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2109865B (en) * 1981-11-21 1984-11-28 Rolls Royce Gas turbine engine compressor air intake
US4534698A (en) * 1983-04-25 1985-08-13 General Electric Company Blade containment structure
US4617028A (en) 1983-11-03 1986-10-14 General Electric Company Aircraft engine air intake including a foreign object separator
US5160248A (en) * 1991-02-25 1992-11-03 General Electric Company Fan case liner for a gas turbine engine with improved foreign body impact resistance
US5259724A (en) * 1992-05-01 1993-11-09 General Electric Company Inlet fan blade fragment containment shield

Also Published As

Publication number Publication date
WO2002012690A1 (en) 2002-02-14
AU2001272671A1 (en) 2002-02-18

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)