GB950909A - Improvements relating to the mounting of gas turbine engines - Google Patents

Improvements relating to the mounting of gas turbine engines

Info

Publication number
GB950909A
GB950909A GB18311/62A GB1831162A GB950909A GB 950909 A GB950909 A GB 950909A GB 18311/62 A GB18311/62 A GB 18311/62A GB 1831162 A GB1831162 A GB 1831162A GB 950909 A GB950909 A GB 950909A
Authority
GB
United Kingdom
Prior art keywords
engine
conduit
bay
fuel
gas turbine
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
GB18311/62A
Inventor
Ernest Edward Chilvers
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 GB18311/62A priority Critical patent/GB950909A/en
Priority to DE19631406595 priority patent/DE1406595A1/en
Priority to FR934455A priority patent/FR1356681A/en
Publication of GB950909A publication Critical patent/GB950909A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)

Abstract

950,909. Gas turbine plant. ROLLS-ROYCE Ltd. May 11, 1962, No. 18311/62. Heading F1G. [Also in Divisions B7 and F2] A gas turbine installation comprises a fuel conduit and fuel supply control means, the conduit and control means each being constituted by at least two mutually co-operating parts, these parts being so arranged that they are automatically brought into engagement when the engine is correctly installed. An aircraft has underwing pods in which are transversely mounted jet propulsion engines 16 which have rotatably mounted nozzles 23 as described in Specification 913,312. The engine is secured in its bay by means of a pivoted air intake 25 and a split annular member 33 which clamps together adjacent flanges on the engine 16 and casing 32 of the exhaust duct. Each engine is located in its bay by opposed trunnions 34 and a further trunnion vertically above the engine axis. Each trunnion 34 comprises a spring loaded pin 36 mounted in a bearing member 43 clamped between a member 43a and a cap 43b. A ball 45 engages a vertical track and as the engine is installed it guides the bearing 43 to locate it with respect to the member 43a. Lifting tackle is fastened to a yoke 40 (see Fig. 3, not shown). The vertical trunnion extends through the yoke into an annular bearing in the engine bay. A fuel control unit 53 is connected by a linkage to the pilot's throttle lever, the linkage including pivoted arms 61 on the yoke engaging corresponding arms on a pivoted member mounted in the engine bay. These arms are not secured together. The fuel conduits 72, 52 are joined by an internal conical surface of a spring loaded cap on the conduit 72 fitting over an external conical surface on the conduit 52. Similar connections are provided for air conduits 73, 74, and air bleed conduits 63, 65. The engine ignition is provided with an automatically engaged quick release plug and socket connection and a selfsealing conduit taps air from the compressor for aircraft control purposes.
GB18311/62A 1962-05-11 1962-05-11 Improvements relating to the mounting of gas turbine engines Expired GB950909A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB18311/62A GB950909A (en) 1962-05-11 1962-05-11 Improvements relating to the mounting of gas turbine engines
DE19631406595 DE1406595A1 (en) 1962-05-11 1963-05-03 Improved storage for gas turbine jet engines
FR934455A FR1356681A (en) 1962-05-11 1963-05-10 Improvements in the assembly of gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18311/62A GB950909A (en) 1962-05-11 1962-05-11 Improvements relating to the mounting of gas turbine engines

Publications (1)

Publication Number Publication Date
GB950909A true GB950909A (en) 1964-02-26

Family

ID=10110320

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18311/62A Expired GB950909A (en) 1962-05-11 1962-05-11 Improvements relating to the mounting of gas turbine engines

Country Status (2)

Country Link
DE (1) DE1406595A1 (en)
GB (1) GB950909A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2259114A (en) * 1991-08-28 1993-03-03 Gen Electric Aircraft engine nacelle profile
GB2274490A (en) * 1993-01-26 1994-07-27 Short Brothers Plc Nacelle for an aircraft propulsive power unit

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2259114A (en) * 1991-08-28 1993-03-03 Gen Electric Aircraft engine nacelle profile
GB2274490A (en) * 1993-01-26 1994-07-27 Short Brothers Plc Nacelle for an aircraft propulsive power unit
GB2274490B (en) * 1993-01-26 1996-09-18 Short Brothers Plc An aircraft propulsive power unit
US5609313A (en) * 1993-01-26 1997-03-11 Short Brothers Plc Aircraft propulsive power unit

Also Published As

Publication number Publication date
DE1406595A1 (en) 1968-10-31

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