GB1074068A - Mounting arrangement for gas turbine jet propulsion engines - Google Patents
Mounting arrangement for gas turbine jet propulsion enginesInfo
- 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
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.
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)
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 |
-
1964
- 1964-09-22 GB GB5351866A patent/GB1074068A/en not_active Expired
Cited By (2)
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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