GB0202047D0 - Gas turbine engines - Google Patents

Gas turbine engines

Info

Publication number
GB0202047D0
GB0202047D0 GB0202047A GB0202047A GB0202047D0 GB 0202047 D0 GB0202047 D0 GB 0202047D0 GB 0202047 A GB0202047 A GB 0202047A GB 0202047 A GB0202047 A GB 0202047A GB 0202047 D0 GB0202047 D0 GB 0202047D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engines
engines
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.)
Withdrawn
Application number
GB0202047A
Other versions
GB2384827A (en
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 GB0202047A priority Critical patent/GB2384827A/en
Publication of GB0202047D0 publication Critical patent/GB0202047D0/en
Publication of GB2384827A publication Critical patent/GB2384827A/en
Withdrawn legal-status Critical Current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
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

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)
GB0202047A 2002-01-30 2002-01-30 A Fastening Between The C-Duct and Core of a Ducted Fan Gas Turbine Engine. Withdrawn GB2384827A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0202047A GB2384827A (en) 2002-01-30 2002-01-30 A Fastening Between The C-Duct and Core of a Ducted Fan Gas Turbine Engine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0202047A GB2384827A (en) 2002-01-30 2002-01-30 A Fastening Between The C-Duct and Core of a Ducted Fan Gas Turbine Engine.

Publications (2)

Publication Number Publication Date
GB0202047D0 true GB0202047D0 (en) 2002-03-13
GB2384827A GB2384827A (en) 2003-08-06

Family

ID=9929978

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0202047A Withdrawn GB2384827A (en) 2002-01-30 2002-01-30 A Fastening Between The C-Duct and Core of a Ducted Fan Gas Turbine Engine.

Country Status (1)

Country Link
GB (1) GB2384827A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0505184D0 (en) * 2005-03-14 2005-04-20 Rolls Royce Plc Thrust reverser mounting structure
FR2905990A1 (en) * 2006-09-20 2008-03-21 Snecma Sa PROPULSIVE SYSTEM WITH INTEGRATED PYLONE FOR AIRCRAFT.
FR2920140B1 (en) * 2007-08-20 2009-10-30 Aircelle Sa NACELLE DE TURBOREACTEUR, INTENDED TO EQUIP AN AIRCRAFT
FR2920137B1 (en) * 2007-08-20 2009-09-18 Aircelle Sa FIXING A STRUCTURE OF A TURBOJET NACELLE BY A REINFORCED KNIFE / GRIP BRIDGE
FR2920198B1 (en) 2007-08-20 2009-10-30 Aircelle Sa STRUCTURE FOR PUSH INVERTER
FR2920141B1 (en) * 2007-08-20 2009-10-30 Aircelle Sa NACELLE DE TURBOREACTEUR, INTENDED TO EQUIP AN AIRCRAFT
FR2978494B1 (en) * 2011-07-25 2013-08-02 Aircelle Sa DEVICE FOR CONNECTING A FRAME FRONT TO A BLOWER HOUSING
US10759541B2 (en) * 2016-10-14 2020-09-01 Rohr, Inc. Nacelle bifurcation with leading edge structure

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2560854B1 (en) * 1984-03-07 1986-09-12 Snecma STRUCTURAL HOODS PARTICIPATING IN THE ASSEMBLY RIGIDITY OF A TURBO-JET
US5101621A (en) * 1989-09-25 1992-04-07 Rohr Industries, Inc. Integrated corner for ducted fan engine shrouds
US5083426A (en) * 1989-10-02 1992-01-28 Rohr Industries, Inc. Integrated engine shroud for gas turbine engines
US5251435A (en) * 1991-10-30 1993-10-12 General Electric Company Reverser inner cowl with integral bifurcation walls and core cowl

Also Published As

Publication number Publication date
GB2384827A (en) 2003-08-06

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)