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GB798832A - Improvements in or relating to flexible mounting systems for vibrating bodies - Google Patents

Improvements in or relating to flexible mounting systems for vibrating bodies

Info

Publication number
GB798832A
GB798832A GB3450/55A GB345055A GB798832A GB 798832 A GB798832 A GB 798832A GB 3450/55 A GB3450/55 A GB 3450/55A GB 345055 A GB345055 A GB 345055A GB 798832 A GB798832 A GB 798832A
Authority
GB
United Kingdom
Prior art keywords
casing
secured
longitudinal direction
engine
bonded
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
GB3450/55A
Inventor
Philip Burrows Smith
William Herbert Brown
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 GB3450/55A priority Critical patent/GB798832A/en
Publication of GB798832A publication Critical patent/GB798832A/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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

798,832. Gas-turbine plant. ROLLS-ROYCE Ltd. Feb. 3, 1956 [Feb. 4, 1955], No. 3450/55. Class 110 (3). [Also in Groups XXXII and XXXIII] A flexible mounting for an aircraft engine 17 comprises a pair of front mountings 10 secured to the compressor casing 11, each consisting of a tubular core secured rigidly to fixed bracing members 19, the core being flexibly mounted within an outer tube secured to casing 11 by a bonded rubber sleeve which provides low stiffness in the longitudinal direction of the engine and high stiffness at right angles to the longitudinal direction. The mounting further comprises a pair of rear mountings 12 arranged to provide high stiffness in the longitudinal direction and low stiffness transversely of the engine. Each mounting 12 consists of alternate rubber and metal discs 21 bonded together and to each side of a flange 22 provided internally of a cylindrical casing 23. The discs 21 are bonded also to end plates 24 which are connected by a bolt 28 to the aircraft structure 20. The casing 23 has connections 30, capable of universal movement, with a horseshoe-shaped fitting 35 and stays 37, the fitting 35 being secured to the turbine casing 13 by one connection 33 that enables it to swing in its own plane and another connection 34 that permits movement transverse to such plane. The stays 37 are connected on their rearward ends to the turbine casing by means of spherical joints formed in brackets 38. Specification 561,940, [Group XXXIII], is referred to.
GB3450/55A 1955-02-04 1955-02-04 Improvements in or relating to flexible mounting systems for vibrating bodies Expired GB798832A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3450/55A GB798832A (en) 1955-02-04 1955-02-04 Improvements in or relating to flexible mounting systems for vibrating bodies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3450/55A GB798832A (en) 1955-02-04 1955-02-04 Improvements in or relating to flexible mounting systems for vibrating bodies

Publications (1)

Publication Number Publication Date
GB798832A true GB798832A (en) 1958-07-30

Family

ID=9758558

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3450/55A Expired GB798832A (en) 1955-02-04 1955-02-04 Improvements in or relating to flexible mounting systems for vibrating bodies

Country Status (1)

Country Link
GB (1) GB798832A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844115A (en) * 1973-02-14 1974-10-29 Gen Electric Load distributing thrust mount
EP0257665A1 (en) * 1986-08-11 1988-03-02 The Boeing Company Aircraft engine mount with vertical vibration isolation
GB2202279A (en) * 1987-03-13 1988-09-21 Gen Electric Vibration isolating aircraft engine mount
US5028001A (en) * 1987-03-13 1991-07-02 General Electric Company Method of vibration isolating an aircraft engine
GB2271390A (en) * 1992-10-12 1994-04-13 Rolls Royce Plc Mounting for a gas turbine engine
GB2351480A (en) * 1999-06-30 2001-01-03 Seneca Tech Ltd Aircraft engine mounting
FR2914907A1 (en) * 2007-04-16 2008-10-17 Snecma Sa SOFT SUSPENSION WITH COMB FOR TURBOMOTEUR
FR2955311A1 (en) * 2010-01-15 2011-07-22 Airbus Operations Sas DEVICE FOR ATTACHING A TURBOPROPULSER, PREFERABLY UNDER AN AIRCRAFT VESSEL
EP3147465A1 (en) * 2015-09-24 2017-03-29 Siemens Aktiengesellschaft Support of a machine, rotating machine engine and a method for assembling of such a rotating machine

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844115A (en) * 1973-02-14 1974-10-29 Gen Electric Load distributing thrust mount
EP0257665A1 (en) * 1986-08-11 1988-03-02 The Boeing Company Aircraft engine mount with vertical vibration isolation
GB2202279A (en) * 1987-03-13 1988-09-21 Gen Electric Vibration isolating aircraft engine mount
US4875655A (en) * 1987-03-13 1989-10-24 General Electric Company Vibration isolating engine mount
US5028001A (en) * 1987-03-13 1991-07-02 General Electric Company Method of vibration isolating an aircraft engine
GB2202279B (en) * 1987-03-13 1991-11-06 Gen Electric Vibration isolating engine mount
GB2271390A (en) * 1992-10-12 1994-04-13 Rolls Royce Plc Mounting for a gas turbine engine
US5427348A (en) * 1992-10-12 1995-06-27 Rolls-Royce Plc Mounting for a gas turbine engine
GB2271390B (en) * 1992-10-12 1995-07-05 Rolls Royce Plc Mounting for a gas turbine engine
GB2351480B (en) * 1999-06-30 2002-09-25 Seneca Tech Ltd Aircraft engine mounting
GB2351480A (en) * 1999-06-30 2001-01-03 Seneca Tech Ltd Aircraft engine mounting
FR2914907A1 (en) * 2007-04-16 2008-10-17 Snecma Sa SOFT SUSPENSION WITH COMB FOR TURBOMOTEUR
EP1982915A1 (en) * 2007-04-16 2008-10-22 Snecma Flexible suspension for a turboengine
US7909285B2 (en) 2007-04-16 2011-03-22 Snecma Flexible suspension for turbine engine
RU2472021C2 (en) * 2007-04-16 2013-01-10 Снекма Suspension device of gas-turbine engine, and gas-turbine engine containing such suspension device
FR2955311A1 (en) * 2010-01-15 2011-07-22 Airbus Operations Sas DEVICE FOR ATTACHING A TURBOPROPULSER, PREFERABLY UNDER AN AIRCRAFT VESSEL
US8474751B2 (en) 2010-01-15 2013-07-02 Airbus Operations S.A.S. Device for fastening a turboprop, preferably under an aircraft wing
EP3147465A1 (en) * 2015-09-24 2017-03-29 Siemens Aktiengesellschaft Support of a machine, rotating machine engine and a method for assembling of such a rotating machine
WO2017050457A1 (en) * 2015-09-24 2017-03-30 Siemens Aktiengesellschaft Support of a machine, rotating machine engine and a method for assembling of such a rotating machine
CN108026787A (en) * 2015-09-24 2018-05-11 西门子股份公司 Machine supporting item, rotary machine engine and the method for assembling rotary machine

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