GB1030521A - Mounting arrangement for gas turbine engines in aircraft - Google Patents

Mounting arrangement for gas turbine engines in aircraft

Info

Publication number
GB1030521A
GB1030521A GB704764A GB704764A GB1030521A GB 1030521 A GB1030521 A GB 1030521A GB 704764 A GB704764 A GB 704764A GB 704764 A GB704764 A GB 704764A GB 1030521 A GB1030521 A GB 1030521A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
engine
aircraft
turbine engines
mounting arrangement
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
GB704764A
Inventor
James Alexander Petrie
Harry Hurdis
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 GB704764A priority Critical patent/GB1030521A/en
Publication of GB1030521A publication Critical patent/GB1030521A/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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,030,521. Mounting jet propulsion engines. ROLLS-ROYCE. Feb. 17, 1965 [Feb. 20, 1964], No. 7047/64. Heading B7G. [Also in Division F1] A by-pass or ducted fan gas turbine jet propulsion engine is mounted on a beam which passes into the by-pass duct, and thus has a smaller frontal area than an engine mounted on a conventional beam passing partly circumferentially around its outer casing. The beam 18 may be of the lattice frame type (Fig. 2, not shown), connected to the engine by links 46. Alternatively the beam may comprise two apertured I-beams, spaced apart in the fore-andaft direction and connected by a metal sheet.
GB704764A 1964-02-20 1964-02-20 Mounting arrangement for gas turbine engines in aircraft Expired GB1030521A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB704764A GB1030521A (en) 1964-02-20 1964-02-20 Mounting arrangement for gas turbine engines in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB704764A GB1030521A (en) 1964-02-20 1964-02-20 Mounting arrangement for gas turbine engines in aircraft

Publications (1)

Publication Number Publication Date
GB1030521A true GB1030521A (en) 1966-05-25

Family

ID=9825622

Family Applications (1)

Application Number Title Priority Date Filing Date
GB704764A Expired GB1030521A (en) 1964-02-20 1964-02-20 Mounting arrangement for gas turbine engines in aircraft

Country Status (1)

Country Link
GB (1) GB1030521A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3420057A (en) * 1965-03-30 1969-01-07 Bristol Siddeley Engines Ltd Engine drive
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4171786A (en) * 1976-09-15 1979-10-23 Vereinigte Flugtechnische Werke-Fokker Gmbh Aircraft wing with engine mount
GB2394991A (en) * 2002-11-06 2004-05-12 Rolls Royce Plc Engine mounting arrangement
GB2434836A (en) * 2006-02-04 2007-08-08 Rolls Royce Plc A mounting system for use in mounting a gas turbine engine
FR3079211A1 (en) * 2018-03-23 2019-09-27 Airbus Operations PROPELLANT AIRCRAFT ASSEMBLY COMPRISING TWO ADJACENT ENGINES, WHOSE OUTLETS HOLES HAVE A RIGHT PORTION CLOSE TO A MEDIAN PLAN OF THE PROPULSIVE ASSEMBLY

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3420057A (en) * 1965-03-30 1969-01-07 Bristol Siddeley Engines Ltd Engine drive
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4171786A (en) * 1976-09-15 1979-10-23 Vereinigte Flugtechnische Werke-Fokker Gmbh Aircraft wing with engine mount
GB2394991A (en) * 2002-11-06 2004-05-12 Rolls Royce Plc Engine mounting arrangement
US6976655B2 (en) 2002-11-06 2005-12-20 Rolls-Royce Plc Mounting arrangement
GB2394991B (en) * 2002-11-06 2006-02-15 Rolls Royce Plc Mounting arrangement
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
FR3079211A1 (en) * 2018-03-23 2019-09-27 Airbus Operations PROPELLANT AIRCRAFT ASSEMBLY COMPRISING TWO ADJACENT ENGINES, WHOSE OUTLETS HOLES HAVE A RIGHT PORTION CLOSE TO A MEDIAN PLAN OF THE PROPULSIVE ASSEMBLY
US11878809B2 (en) 2018-03-23 2024-01-23 Airbus Operations S.A.S. Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly

Similar Documents

Publication Publication Date Title
GB1069033A (en) Improvements in or relating to gas turbine jet propulsion engines
GB1328993A (en) Air intakes for gas turbine engines
GB1318748A (en) Gas turgine ducted fan engines for aircraft
GB1130268A (en) Improvements in or relating to gas turbine by-pass engines
GB1316029A (en) Turbofan engine thrust reversers
GB1085619A (en) Gas turbine engine
GB1466385A (en) Containment shields for gas turbine engines
GB1030521A (en) Mounting arrangement for gas turbine engines in aircraft
GB1014260A (en) Improvements in gas turbine ducted fan powerplant
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.
GB1228806A (en)
GB1073458A (en) Improvements relating to by-pass ducted for gas-turbine aircraft engines
GB1375868A (en)
GB1032274A (en) Mounting of ducted fan turbine engines in the tail of an aircraft
GB1190364A (en) Gas Turbine Engines
GB1357370A (en) Ducted fan gas turbine jet propulsion engine with thrust control means
GB1195027A (en) Improvements relating to Cowls for Turbo-Fan Aircraft Engines.
GB974384A (en) An arrangement of turbo jet engines at the tail end of an aircraft
GB1074068A (en) Mounting arrangement for gas turbine jet propulsion engines
GB1507914A (en) Device for preventing foreign matters from being sucked into a gas turbine engine for an aircraft
GB983051A (en) Aircraft
GB1127653A (en) Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner
GB1041048A (en) Improvements in aircraft having jet-propulsion power-plants
GB1131378A (en) Air intake for a gas turbine engine
GB888943A (en) Improvements in or relating to fan units