GB857899A - Improvements relating to turbo-jet propulsion units in aircraft - Google Patents
Improvements relating to turbo-jet propulsion units in aircraftInfo
- Publication number
- GB857899A GB857899A GB14952/59A GB1495259A GB857899A GB 857899 A GB857899 A GB 857899A GB 14952/59 A GB14952/59 A GB 14952/59A GB 1495259 A GB1495259 A GB 1495259A GB 857899 A GB857899 A GB 857899A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet propulsion
- turbo
- aircraft
- improvements relating
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
857,899. Generating combustion products under pressure. DAIMLER BENZ A.G. May 1, 1959 [May 2, 1958], No. 14952/59. Class 51 (1). [Also in Groups XXVI and XXXIII] The afterburner section 20 of a jet propulsion engine is provided with flame holders 29 and guide vanes 28 through which fuel is supplied to jets 30 at the rear of the vanes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE857899X | 1958-05-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB857899A true GB857899A (en) | 1961-01-04 |
Family
ID=6789685
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14952/59A Expired GB857899A (en) | 1958-05-02 | 1959-05-01 | Improvements relating to turbo-jet propulsion units in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB857899A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2205903A (en) * | 1987-06-19 | 1988-12-21 | Mtu Muenchen Gmbh | Variable geometry jet engine nacelle |
-
1959
- 1959-05-01 GB GB14952/59A patent/GB857899A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2205903A (en) * | 1987-06-19 | 1988-12-21 | Mtu Muenchen Gmbh | Variable geometry jet engine nacelle |
GB2205903B (en) * | 1987-06-19 | 1991-12-11 | Mtu Muenchen Gmbh | Jet engine nacelle |
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