GB966522A - Improvements relating to aerial vehicles having jet propulsion engines - Google Patents
Improvements relating to aerial vehicles having jet propulsion enginesInfo
- Publication number
- GB966522A GB966522A GB3684/60A GB368460A GB966522A GB 966522 A GB966522 A GB 966522A GB 3684/60 A GB3684/60 A GB 3684/60A GB 368460 A GB368460 A GB 368460A GB 966522 A GB966522 A GB 966522A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vehicle
- closed
- pin
- dogs
- collar
- 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
- 241000282472 Canis lupus familiaris Species 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
-
- 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
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
966,522. Self-propelled missiles. BRISTOL SIDDELEY ENGINES Ltd. Jan. 31, 1961 [Feb. 2, 1960], No. 3684/60. Heading F3A. [Also in Divisions B7 and F1] An aerial vehicle has a jet-propulsion engine supported externally from the vehicle and having a water-tight casing 17, 18 with a water-tight closure 19 for closing an opening adjacent the exhaust nozzle. The engine is a reverse flow gas-turbine engine fixed at 15a to fuselage 9 provided with a launching rocket motor 11. The closure member 19 mounted on the vehicle by a pin 29 is opened and closed by a rod 31a and a lever 31 pivotally mounted by a collar 30 on pin 29, dogs 34 on collar 30 engaging dogs 35 on a further collar 30 splined to pin 29 and carrying a lever 32 connected by an over-centre spring 33 to the vehicle, a limited lost-motion existing between dogs 34, 35. The spring 33 holds member 19 either in a water-tight closed position against casing 17, 18, or in an open position where it acts as a heat shield. In Figs. 4, 5 (not shown), an additional sliding closure member is mounted at a forwardly located air intake, both closure members may be operated together or independently. Prior to launching the closure member or members are closed and are again closed prior to landing (e.g. in the sea) to protect the engine and to enable the casing to act as a buoyancy tank.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3684/60A GB966522A (en) | 1960-02-02 | 1960-02-02 | Improvements relating to aerial vehicles having jet propulsion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3684/60A GB966522A (en) | 1960-02-02 | 1960-02-02 | Improvements relating to aerial vehicles having jet propulsion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB966522A true GB966522A (en) | 1964-08-12 |
Family
ID=9762981
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3684/60A Expired GB966522A (en) | 1960-02-02 | 1960-02-02 | Improvements relating to aerial vehicles having jet propulsion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB966522A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3465990A (en) * | 1966-10-05 | 1969-09-09 | Raymond Prunty Holland Jr | Aircraft having energy-conserving means |
GB2225060A (en) * | 1988-09-28 | 1990-05-23 | Short Brothers Plc | Ducted fan turbine engine |
GB2381249B (en) * | 2001-10-11 | 2005-01-12 | Short Brothers Plc | Aircraft Propulsive Power Unit and a Nacelle Structure |
CN112758334A (en) * | 2021-01-28 | 2021-05-07 | 中南大学 | Water-air cross-medium engine and cross-medium aircraft with same |
-
1960
- 1960-02-02 GB GB3684/60A patent/GB966522A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3465990A (en) * | 1966-10-05 | 1969-09-09 | Raymond Prunty Holland Jr | Aircraft having energy-conserving means |
GB2225060A (en) * | 1988-09-28 | 1990-05-23 | Short Brothers Plc | Ducted fan turbine engine |
US5136839A (en) * | 1988-09-28 | 1992-08-11 | Short Brothers Plc | Ducted fan turbine engine |
GB2225060B (en) * | 1988-09-28 | 1993-03-24 | Short Brothers Plc | Ducted fan turbine engine |
GB2381249B (en) * | 2001-10-11 | 2005-01-12 | Short Brothers Plc | Aircraft Propulsive Power Unit and a Nacelle Structure |
CN112758334A (en) * | 2021-01-28 | 2021-05-07 | 中南大学 | Water-air cross-medium engine and cross-medium aircraft with same |
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