GB993899A - An arrangement of jet propulsion units in aircraft - Google Patents
An arrangement of jet propulsion units in aircraftInfo
- Publication number
- GB993899A GB993899A GB4222762A GB4222762A GB993899A GB 993899 A GB993899 A GB 993899A GB 4222762 A GB4222762 A GB 4222762A GB 4222762 A GB4222762 A GB 4222762A GB 993899 A GB993899 A GB 993899A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- engine
- jet propulsion
- arrangement
- propulsion units
- 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)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
993,899. Jet-propelled aircraft. MESSERSCHMITT A.G. Nov. 8, 1962 [Jan. 18, 1962], No. 42227/62. Heading B7G. An aircraft has two jet propulsion engines 1, 2, with swivellable nozzles 3, 4, mounted one in the nose and one at the rear of the aircraft and having their axes parallel to the longitudinal axis of the aircraft. The rear engine is the main propulsion engine, selected for cruise performance, whereas the forward engine has a high thrust: weight ratio and is intended for use only during take-off and climb, and in the event of failure of the main engine. The forward engine is lowered from the aircraft for the latter operation, and its intakes may be covered during cruising flight.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEM0051494 | 1962-01-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB993899A true GB993899A (en) | 1965-06-02 |
Family
ID=7307140
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4222762A Expired GB993899A (en) | 1962-01-18 | 1962-11-08 | An arrangement of jet propulsion units in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB993899A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4206894A (en) * | 1975-02-19 | 1980-06-10 | Walter Becke | Aircraft control |
GB2263675A (en) * | 1992-01-28 | 1993-08-04 | Rolls Royce Plc | Propulsion system for braking aircraft. |
-
1962
- 1962-11-08 GB GB4222762A patent/GB993899A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4206894A (en) * | 1975-02-19 | 1980-06-10 | Walter Becke | Aircraft control |
GB2263675A (en) * | 1992-01-28 | 1993-08-04 | Rolls Royce Plc | Propulsion system for braking aircraft. |
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