GB1074067A - Mounting arrangement for jet propulsion engines - Google Patents

Mounting arrangement for jet propulsion engines

Info

Publication number
GB1074067A
GB1074067A GB25840/64A GB2584064A GB1074067A GB 1074067 A GB1074067 A GB 1074067A GB 25840/64 A GB25840/64 A GB 25840/64A GB 2584064 A GB2584064 A GB 2584064A GB 1074067 A GB1074067 A GB 1074067A
Authority
GB
United Kingdom
Prior art keywords
engine
aircraft
spigot
yoke
socket
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
GB25840/64A
Inventor
Alexander Stewart
Roger Anthony Cresswell
Martin Hume Bryan-Brown
Peter Arthur Ward
John Albert Mullins
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 GB25840/64A priority Critical patent/GB1074067A/en
Priority to US463581A priority patent/US3327971A/en
Priority to DE1965R0040923 priority patent/DE1252537B/de
Publication of GB1074067A publication Critical patent/GB1074067A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/005—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being fixed relative to the fuselage
    • 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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Rolling Contact Bearings (AREA)
  • Transmission Devices (AREA)

Abstract

1,074,067. Aircraft engine mountings. ROLLS-ROYCE Ltd. June 15, 1965 [June 23, 1964; July 10, 1964; Sept. 22, 1964], Nos. 25840/64, 28725/64 and 38705/64. Heading B7G. [Also in Division F1] A jet propulsion engine has an exhaust gas deflector fixed to the engine (e.g. by a sleeve (27) around the engine casing) and attached to the structure of an aircraft by a mounting that transmits all the engine thrust and some of the load, the remaining portion of the weight being carried by a second mounting comprising a yoke (28, Figs. 2-4, not shown) attached to diametrically opposed points on the engine casing by spigot and socket joints (31) and supported on the aircraft by a ball-and-socket joint (29). There may be two ball-and-socket joints (Figs. 5 and 6, not shown), one at each end of a link (134), one connecting the link to the aircraft structure, and one connecting it to the yoke. A spigot (132) on the yoke then engages the engine casing to prevent the yoke pivoting about the diametrically opposed spigot and socket joints (131). The engine is a gas turbine engine mounted in a pod under an aircraft wing, with its axis parallel to the transverse axis of the aircraft. The deflector comprises a ring (22, Figs. 2-4, not shown) fixed to the sleeve (27) and containing a rotatable cascade (15), and the first mounting comprises a spigot and socket joint (19) and a ball-and-socket joint (20) at opposite ends of a horizontal diameter of the ring (22), the socket being in structural members of the pod.
GB25840/64A 1964-06-23 1964-06-23 Mounting arrangement for jet propulsion engines Expired GB1074067A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB25840/64A GB1074067A (en) 1964-06-23 1964-06-23 Mounting arrangement for jet propulsion engines
US463581A US3327971A (en) 1964-06-23 1965-06-14 Mounting arrangement for lift engines
DE1965R0040923 DE1252537B (en) 1964-06-23 1965-06-22

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB25840/64A GB1074067A (en) 1964-06-23 1964-06-23 Mounting arrangement for jet propulsion engines
GB2872564 1964-07-10
GB3870564 1964-09-22

Publications (1)

Publication Number Publication Date
GB1074067A true GB1074067A (en) 1967-06-28

Family

ID=605477

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25840/64A Expired GB1074067A (en) 1964-06-23 1964-06-23 Mounting arrangement for jet propulsion engines

Country Status (2)

Country Link
DE (1) DE1252537B (en)
GB (1) GB1074067A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4500054A (en) * 1982-10-29 1985-02-19 Rolls-Royce Limited Mounting system for coupled turboshaft gas turbine engines
GB2434836A (en) * 2006-02-04 2007-08-08 Rolls Royce Plc A mounting system for use in mounting a gas turbine engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014003214B4 (en) * 2014-03-06 2018-12-13 Ernst Spielvogel Arrangement of wings on or in an airframe and or bodywork.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4500054A (en) * 1982-10-29 1985-02-19 Rolls-Royce Limited Mounting system for coupled turboshaft gas turbine engines
GB2434836A (en) * 2006-02-04 2007-08-08 Rolls Royce Plc A mounting system for use in mounting a gas turbine engine
GB2434836B (en) * 2006-02-04 2008-12-10 Rolls Royce Plc Mounting system for use in mounting a gas turbine engine
US7815145B2 (en) 2006-02-04 2010-10-19 Rolls-Royce Plc Mounting system for use in mounting a gas turbine engine

Also Published As

Publication number Publication date
DE1252537B (en) 1967-10-19

Similar Documents

Publication Publication Date Title
GB1455603A (en) Thrust mount arrangeement for gas turbine engines
GB2010969A (en) Mounting for Gas Turbine Jet Propulsion Engine
GB1318748A (en) Gas turgine ducted fan engines for aircraft
GB735122A (en) Improvements in or relating to jet nozzles
US5226288A (en) Torque link fan jet engine support for reducing engine bending
US3318554A (en) Mounting arrangement for engines
GB1074067A (en) Mounting arrangement for jet propulsion engines
US2936973A (en) Vtol aircraft
GB1024894A (en) Improvements in aircraft jet-propulsion power-plants
GB1151729A (en) Improvements in Flexible Connections for Ducts
US2818225A (en) Power plant installations for aircraft
GB1071075A (en) Improvements in aircraft
US3057582A (en) Improved engine mounting
GB1066268A (en) Jet propulsion power plant
GB721558A (en) Improvements relating to jet nozzles for jet propulsion units
GB1224230A (en) Improvements in devices for coaxially securing a centrebody inside a hollow body
GB1074068A (en) Mounting arrangement for gas turbine jet propulsion engines
GB1210939A (en) An aircraft jet propulsion engine incorporating a nozzle having a thrust-directing arrangement
GB1484484A (en) Exhaust duct for a thrust jet engine and an engine equipped with such a duct
GB743205A (en) Improvements in or relating to power-plant installations for aircraft
GB1302228A (en)
GB886201A (en) Jet noise silencer for an aircraft
GB1093050A (en) Aircraft engine mounting
GB1091573A (en) Combustion apparatus for gas turbine engines
GB715486A (en) Improvements in or relating to aircraft