GB0007441D0 - A mounting for coupling a turbofan gas turbine engine to an aircraft structure - Google Patents

A mounting for coupling a turbofan gas turbine engine to an aircraft structure

Info

Publication number
GB0007441D0
GB0007441D0 GBGB0007441.9A GB0007441A GB0007441D0 GB 0007441 D0 GB0007441 D0 GB 0007441D0 GB 0007441 A GB0007441 A GB 0007441A GB 0007441 D0 GB0007441 D0 GB 0007441D0
Authority
GB
United Kingdom
Prior art keywords
coupling
mounting
gas turbine
turbine engine
aircraft structure
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Withdrawn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
GBGB0007441.9A
Other versions
GB2360749A (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 GB0007441A priority Critical patent/GB2360749A/en
Publication of GB0007441D0 publication Critical patent/GB0007441D0/en
Publication of GB2360749A publication Critical patent/GB2360749A/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Withdrawn legal-status Critical Current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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB0007441A 2000-03-28 2000-03-28 Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads Withdrawn GB2360749A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0007441A GB2360749A (en) 2000-03-28 2000-03-28 Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0007441A GB2360749A (en) 2000-03-28 2000-03-28 Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads

Publications (2)

Publication Number Publication Date
GB0007441D0 true GB0007441D0 (en) 2000-05-17
GB2360749A GB2360749A (en) 2001-10-03

Family

ID=9888529

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0007441A Withdrawn GB2360749A (en) 2000-03-28 2000-03-28 Aircraft turbofan gas turbine engine upstream core mounting which does not transmit vertical loads

Country Status (1)

Country Link
GB (1) GB2360749A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2394991B (en) * 2002-11-06 2006-02-15 Rolls Royce Plc Mounting arrangement
CA2918320C (en) 2013-07-26 2018-05-15 Mra Systems, Inc. Aircraft engine pylon

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8300748D0 (en) * 1983-01-12 1983-02-16 British Aerospace Power plant attachment for aircraft wings
US4917331A (en) * 1988-11-10 1990-04-17 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter

Also Published As

Publication number Publication date
GB2360749A (en) 2001-10-03

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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)