GB0312490D0 - Aeroengine nacelle - Google Patents

Aeroengine nacelle

Info

Publication number
GB0312490D0
GB0312490D0 GBGB0312490.6A GB0312490A GB0312490D0 GB 0312490 D0 GB0312490 D0 GB 0312490D0 GB 0312490 A GB0312490 A GB 0312490A GB 0312490 D0 GB0312490 D0 GB 0312490D0
Authority
GB
United Kingdom
Prior art keywords
aeroengine
nacelle
aeroengine nacelle
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
GBGB0312490.6A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce 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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GBGB0312490.6A priority Critical patent/GB0312490D0/en
Priority to GB0315800A priority patent/GB2403774B/en
Publication of GB0312490D0 publication Critical patent/GB0312490D0/en
Priority to US10/697,945 priority patent/US7090165B2/en
Priority to FR0400494A priority patent/FR2855497B1/en
Ceased 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/08—Inspection panels for power plants
    • 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
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • 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)
  • Wind Motors (AREA)
GBGB0312490.6A 2003-06-02 2003-06-02 Aeroengine nacelle Ceased GB0312490D0 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GBGB0312490.6A GB0312490D0 (en) 2003-06-02 2003-06-02 Aeroengine nacelle
GB0315800A GB2403774B (en) 2003-06-02 2003-07-07 Aeroengine nacelle
US10/697,945 US7090165B2 (en) 2003-06-02 2003-10-31 Aeroengine nacelle
FR0400494A FR2855497B1 (en) 2003-06-02 2004-01-20 NACELLE FOR A GAS TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0312490.6A GB0312490D0 (en) 2003-06-02 2003-06-02 Aeroengine nacelle

Publications (1)

Publication Number Publication Date
GB0312490D0 true GB0312490D0 (en) 2003-07-09

Family

ID=9959080

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0312490.6A Ceased GB0312490D0 (en) 2003-06-02 2003-06-02 Aeroengine nacelle
GB0315800A Expired - Fee Related GB2403774B (en) 2003-06-02 2003-07-07 Aeroengine nacelle

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB0315800A Expired - Fee Related GB2403774B (en) 2003-06-02 2003-07-07 Aeroengine nacelle

Country Status (1)

Country Link
GB (2) GB0312490D0 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2890378B1 (en) * 2005-09-08 2009-01-16 Airbus France Sas NACELLE HOOD FOR TURBOJET AND NACELLE COMPRISING AT LEAST ONE SUCH HOOD.
ES2301304B1 (en) 2005-10-31 2009-05-01 Airbus España, S.L. OPENING AND CLOSING SECURITY SYSTEM FOR DOORS.
US9126691B2 (en) 2007-05-30 2015-09-08 United Technologies Corporation Access door for gas turbine engine components
US9290274B2 (en) 2014-06-02 2016-03-22 Mra Systems, Inc. Acoustically attenuating sandwich panel constructions

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
FR2622507B1 (en) * 1987-10-28 1990-01-26 Snecma
FR2661213B1 (en) * 1990-04-19 1992-07-03 Snecma AVIATION ENGINE WITH VERY HIGH DILUTION RATES AND OF THE SAID TYPE FRONT CONTRAFAN.
GB9116986D0 (en) * 1991-08-07 1991-10-09 Rolls Royce Plc Gas turbine engine nacelle assembly
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
GB9407632D0 (en) * 1994-04-18 1994-06-08 Short Brothers Plc An aircraft propulsive power unit
US6364603B1 (en) * 1999-11-01 2002-04-02 Robert P. Czachor Fan case for turbofan engine having a fan decoupler
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit

Also Published As

Publication number Publication date
GB0315800D0 (en) 2003-08-13
GB2403774B (en) 2006-09-06
GB2403774A (en) 2005-01-12

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Legal Events

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