GB1074068A - Mounting arrangement for gas turbine jet propulsion engines - Google Patents

Mounting arrangement for gas turbine jet propulsion engines

Info

Publication number
GB1074068A
GB1074068A GB5351866A GB5351866A GB1074068A GB 1074068 A GB1074068 A GB 1074068A GB 5351866 A GB5351866 A GB 5351866A GB 5351866 A GB5351866 A GB 5351866A GB 1074068 A GB1074068 A GB 1074068A
Authority
GB
United Kingdom
Prior art keywords
engine
mounting
axis
jet propulsion
stays
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
GB5351866A
Inventor
Peter Arthur Ward
John Albert Mullins
Martin Hume Bryan-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 GB5351866A priority Critical patent/GB1074068A/en
Publication of GB1074068A publication Critical patent/GB1074068A/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
    • B64C29/0066—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 with horizontal jet and jet deflector

Landscapes

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

Abstract

1,074,068. Mounting jet propulsion engines. ROLLS ROYCE Ltd. June 15, 1965 [Sept. 22, 1964], No. 53518/66. Divided out of 1,074,067. Heading B7G. [Also in Division F1] A gas turbine jet propulsion engine has an exhaust gas deflector fixed to the engine and attached to the structure of an aircraft by a mounting that transmits all the engine thrust and some of the weight, the mounting comprising a swinging link (23) pivoted about an axis parallel to the engine axis, which takes all the thrust loads, and a stay or stays (26) which prevent angular movement of the engine about its axis. The two stays (26) described lie at a tangent to the engine casing and depend from a single suspension point attached to the aircraft structure. A second mounting (Fig. 3, not shown) carries the rest of the weight of the engine and comprises two similar stays (30). The engine is mounted parallel to the longitudinal axis of the aircraft in a wing mounted pod and has a forward propulsion nozzle (17) and a deflector (15) for diverting the exhaust through a downwardly directed nozzle (18) of the cascade or elbow-bend type. The deflector is mounted on the engine casing by a sleeve (14) and flange (15), and the first mounting is attached to the sleeve.
GB5351866A 1964-09-22 1964-09-22 Mounting arrangement for gas turbine jet propulsion engines Expired GB1074068A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5351866A GB1074068A (en) 1964-09-22 1964-09-22 Mounting arrangement for gas turbine jet propulsion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5351866A GB1074068A (en) 1964-09-22 1964-09-22 Mounting arrangement for gas turbine jet propulsion engines

Publications (1)

Publication Number Publication Date
GB1074068A true GB1074068A (en) 1967-06-28

Family

ID=10468098

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5351866A Expired GB1074068A (en) 1964-09-22 1964-09-22 Mounting arrangement for gas turbine jet propulsion engines

Country Status (1)

Country Link
GB (1) GB1074068A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2550525A1 (en) * 1974-11-13 1976-05-20 Snecma DEVICE FOR ATTACHING A JET ENGINE TO AN AIRPLANE
US7313920B2 (en) 2003-12-11 2008-01-01 Rolls-Royce Plc Aircraft engine mounting

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2550525A1 (en) * 1974-11-13 1976-05-20 Snecma DEVICE FOR ATTACHING A JET ENGINE TO AN AIRPLANE
US7313920B2 (en) 2003-12-11 2008-01-01 Rolls-Royce Plc Aircraft engine mounting

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