GB1236917A - Improvements in or relating to means for supporting a gas turbine engine in an aircraft - Google Patents

Improvements in or relating to means for supporting a gas turbine engine in an aircraft

Info

Publication number
GB1236917A
GB1236917A GB27415/67A GB2741567A GB1236917A GB 1236917 A GB1236917 A GB 1236917A GB 27415/67 A GB27415/67 A GB 27415/67A GB 2741567 A GB2741567 A GB 2741567A GB 1236917 A GB1236917 A GB 1236917A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
aircraft
links
supporting
turbine engine
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
GB27415/67A
Inventor
Peter Roderick King
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 GB27415/67A priority Critical patent/GB1236917A/en
Publication of GB1236917A publication Critical patent/GB1236917A/en
Expired 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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)
  • Tires In General (AREA)

Abstract

1,236,917. Gas turbine engines; mounting in aircraft. ROLLS-ROYCE Ltd. 28 May, 1968 [14 June, 1967], No. 27415/67. Heading B7G. [Also in Divisions E2 and F1] Support means for a gas turbine engine in an aircraft includes a set of supporting links that takes the full load, together with additional links that only take a load upon failure of one or more of the supporting links. The links are distributed tangentially to the engine in transverse planes at the front and back of the engine casing and also longitudinally there of either parallel to the axis or at an acute angle thereto (Figs. 2, 3, 4, not shown) the additional links are provided with resilient bushes so that they do not normally carry load (see Division E2).
GB27415/67A 1967-06-14 1967-06-14 Improvements in or relating to means for supporting a gas turbine engine in an aircraft Expired GB1236917A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB27415/67A GB1236917A (en) 1967-06-14 1967-06-14 Improvements in or relating to means for supporting a gas turbine engine in an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB27415/67A GB1236917A (en) 1967-06-14 1967-06-14 Improvements in or relating to means for supporting a gas turbine engine in an aircraft

Publications (1)

Publication Number Publication Date
GB1236917A true GB1236917A (en) 1971-06-23

Family

ID=10259201

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27415/67A Expired GB1236917A (en) 1967-06-14 1967-06-14 Improvements in or relating to means for supporting a gas turbine engine in an aircraft

Country Status (1)

Country Link
GB (1) GB1236917A (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4013246A (en) * 1974-12-24 1977-03-22 Rolls-Royce (1971) Limited Mounting bypass gas turbines engines on aircraft
US4065077A (en) * 1976-04-30 1977-12-27 Rolls-Royce Limited Attachment for attaching jet propulsion engines to fixed structure
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
FR2599708A1 (en) * 1986-06-10 1987-12-11 Snecma DEVICE FOR REARLY SECURING A TURBOJET ENGINE ON AN AIRCRAFT MAT
EP0431800A1 (en) * 1989-12-05 1991-06-12 ROLLS-ROYCE plc Failure tolerant engine mounting
US5181675A (en) * 1991-05-23 1993-01-26 Societe Nationale D'etude Et Moteurs D'aviation S.N.E. Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft
EP0527672A1 (en) * 1991-08-14 1993-02-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Rear suspension device for an engine turbine unit
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
EP0741074A1 (en) * 1995-05-03 1996-11-06 The Boeing Company Three link failsafe engine mount
EP0744338A1 (en) * 1995-03-24 1996-11-27 The Boeing Company Fail-safe mount system
EP1103463A1 (en) * 1999-11-20 2001-05-30 ROLLS-ROYCE plc A gas turbine engine mounting arrangement
FR2887850A1 (en) * 2005-06-29 2007-01-05 Airbus France Sas Aircraft engine mounting structure has thrust force take-up assembly fixed to point on rigid structure separate from front and rear coupling points
FR2890377A1 (en) * 2005-09-05 2007-03-09 Airbus France Sas ARRANGEMENT SUITABLE FOR CONNECTING A PALONNIER TO AN AIRCRAFT ENGINE HITCHING MAT
EP1847457A3 (en) * 2006-04-22 2010-03-10 Rolls-Royce plc Aeroengine mounting
FR2961172A1 (en) * 2010-06-14 2011-12-16 Snecma SUSPENSION OF A TURBOMOTOR OR THE LIKE TO AN AIRCRAFT PYLON WITH INTEGRATED SAFETY.
CN102774502A (en) * 2011-05-12 2012-11-14 空中客车营运有限公司 Device for attaching an aircraft engine, comprising clamping wedges for engine attachment with corner effect
CN105620766A (en) * 2014-10-28 2016-06-01 中国航空工业集团公司西安飞机设计研究所 Main installation joint for truss type engine

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4013246A (en) * 1974-12-24 1977-03-22 Rolls-Royce (1971) Limited Mounting bypass gas turbines engines on aircraft
US4065077A (en) * 1976-04-30 1977-12-27 Rolls-Royce Limited Attachment for attaching jet propulsion engines to fixed structure
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
FR2599708A1 (en) * 1986-06-10 1987-12-11 Snecma DEVICE FOR REARLY SECURING A TURBOJET ENGINE ON AN AIRCRAFT MAT
EP0249553A1 (en) * 1986-06-10 1987-12-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Rear suspension device for an engine turbine unit attached to an aircraft engine pylon
US4742975A (en) * 1986-06-10 1988-05-10 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Mounting structure for a turbojet engine
EP0431800A1 (en) * 1989-12-05 1991-06-12 ROLLS-ROYCE plc Failure tolerant engine mounting
US5078342A (en) * 1989-12-05 1992-01-07 Rolls-Royce, Plc Failure tolerant engine mounting
US5181675A (en) * 1991-05-23 1993-01-26 Societe Nationale D'etude Et Moteurs D'aviation S.N.E. Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft
EP0527672A1 (en) * 1991-08-14 1993-02-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Rear suspension device for an engine turbine unit
FR2680353A1 (en) * 1991-08-14 1993-02-19 Snecma REAR HANGING STRUCTURE OF A TURBOREACTOR.
US5238206A (en) * 1991-08-14 1993-08-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Rear hanging structure for a turbojet engine
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
EP0744338A1 (en) * 1995-03-24 1996-11-27 The Boeing Company Fail-safe mount system
EP0741074A1 (en) * 1995-05-03 1996-11-06 The Boeing Company Three link failsafe engine mount
EP1103463A1 (en) * 1999-11-20 2001-05-30 ROLLS-ROYCE plc A gas turbine engine mounting arrangement
FR2887850A1 (en) * 2005-06-29 2007-01-05 Airbus France Sas Aircraft engine mounting structure has thrust force take-up assembly fixed to point on rigid structure separate from front and rear coupling points
JP4864971B2 (en) * 2005-09-05 2012-02-01 エアバス・フランス System for connecting crossbar to aircraft engine pylon
FR2890377A1 (en) * 2005-09-05 2007-03-09 Airbus France Sas ARRANGEMENT SUITABLE FOR CONNECTING A PALONNIER TO AN AIRCRAFT ENGINE HITCHING MAT
WO2007028764A1 (en) * 2005-09-05 2007-03-15 Airbus France System for connecting a crossbar to an aircraft engine pylon
US8087608B2 (en) 2005-09-05 2012-01-03 Airbus Operations Sas System for connecting a crossbar to an aircraft engine pylon
EP1847457A3 (en) * 2006-04-22 2010-03-10 Rolls-Royce plc Aeroengine mounting
US8444084B2 (en) 2006-04-22 2013-05-21 Rolls-Royce Plc Aeroengine mounting
WO2011157931A1 (en) 2010-06-14 2011-12-22 Snecma Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system
FR2961172A1 (en) * 2010-06-14 2011-12-16 Snecma SUSPENSION OF A TURBOMOTOR OR THE LIKE TO AN AIRCRAFT PYLON WITH INTEGRATED SAFETY.
US9067688B2 (en) 2010-06-14 2015-06-30 Snecma Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system
RU2583243C2 (en) * 2010-06-14 2016-05-10 Снекма Gas turbine engine mounted on pylon of aircraft fuselage by apparatus ensuring safety of suspension
CN102774502A (en) * 2011-05-12 2012-11-14 空中客车营运有限公司 Device for attaching an aircraft engine, comprising clamping wedges for engine attachment with corner effect
CN105620766A (en) * 2014-10-28 2016-06-01 中国航空工业集团公司西安飞机设计研究所 Main installation joint for truss type engine

Similar Documents

Publication Publication Date Title
GB1236917A (en) Improvements in or relating to means for supporting a gas turbine engine in an aircraft
CA702551A (en) Lubrication system for gas turbine engine
GB1213347A (en) Rotor with pin mounted blades
GB1504290A (en) Gas turbine engine mounting systems
GB1030521A (en) Mounting arrangement for gas turbine engines in aircraft
GB1131378A (en) Air intake for a gas turbine engine
GB1190364A (en) Gas Turbine Engines
OPRECHT Problems related to the development of a gas turbine in the 10-30 hp class(Shaft-power turbine design, including rotor vibration problems, computer high speed testing, application as auxiliary power supply in turbojets, etc)
SZCZECINSKI Specifics of the loads acting on the assemblies and components of two-spool and ducted-fan turbine engines(Stress analysis of loads acting on components of two spool and ducted fan turbine engines, considering optimum design and reliability)
MCGINNIS et al. Requirements versus cost- Small controls(Small gas turbine engine controls, discussing design, development and cost factors)
GB1074068A (en) Mounting arrangement for gas turbine jet propulsion engines
CA800250A (en) Gas turbine engine fuel system
AU417712B2 (en) Fuel systems for gas turbine engines
GB983051A (en) Aircraft
CA802531A (en) Fuel systems for gas turbine engines
AU437182B2 (en) Fuel systems for gas turbine engines
AU437874B2 (en) Fuel systems for gas turbine engines
AU434885B2 (en) Fuel systems for gas turbine engines
AU421536B2 (en) Fuel systems for gas turbine engines
AU430625B2 (en) Fuel systems for gas turbine engines
CA718614A (en) Gas turbine engine fuel system
AU1866867A (en) Fuel systems for gas turbine engines
AU682166A (en) Fuel systems for gas turbine engines
AU409686B2 (en) Gas turbine engine fuel systems
AU415881B2 (en) Acceleration controls for gas turbine engine fuel systems