GB921398A - Aircraft - Google Patents
AircraftInfo
- Publication number
- GB921398A GB921398A GB1885561A GB1885561A GB921398A GB 921398 A GB921398 A GB 921398A GB 1885561 A GB1885561 A GB 1885561A GB 1885561 A GB1885561 A GB 1885561A GB 921398 A GB921398 A GB 921398A
- Authority
- GB
- United Kingdom
- Prior art keywords
- duct
- inlet
- engines
- air
- aircraft
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
921,398. Jet propulsion plant. W. A. HOWIE. May 25, 1961 [June 15, 1960], No. 18855/61. Class 110 (3). [Also in Group XXXIII] An aircraft jet propulsion plant comprises two gas turbine engines 124, each located in a duct 120 with radial clearance and supplied from an inlet 121 controlled by a flap 123. The turbine exhaust, together with air entrained around engine 124 is discharged through an afterburner (not shown) and a nozzle 125. Lifting force, or further propulsive force, is supplied by turbo-fan engines 112, each located in a duct 110 fed from an inlet 108 controlled by flap 113 and discharging into the throat of a convergent-divergent duct 102 running through the aircraft, so as to entrain air through the duct inlet 103 and discharge it through an outlet 104. In a modification, Figs. 5 and 6 (not shown), the engines 112 are replaced by gas turbine engines located in the duct inlet 103, and air is entrained from ducts similar to ducts 110.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA801114 | 1960-06-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB921398A true GB921398A (en) | 1963-03-20 |
Family
ID=4141218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1885561A Expired GB921398A (en) | 1960-06-15 | 1961-05-25 | Aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB921398A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2231622A (en) * | 1989-03-16 | 1990-11-21 | Harold Birkett | Engine for v.t.o.l. and other aircraft |
WO2004030783A2 (en) * | 2002-09-27 | 2004-04-15 | Dieter Wagels | Flying device |
-
1961
- 1961-05-25 GB GB1885561A patent/GB921398A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2231622A (en) * | 1989-03-16 | 1990-11-21 | Harold Birkett | Engine for v.t.o.l. and other aircraft |
GB2231622B (en) * | 1989-03-16 | 1993-10-27 | Harold Birkett | Engine for V.T.O.L. Aircraft |
WO2004030783A2 (en) * | 2002-09-27 | 2004-04-15 | Dieter Wagels | Flying device |
WO2004030783A3 (en) * | 2002-09-27 | 2004-09-30 | Dieter Wagels | Flying device |
CN100368044C (en) * | 2002-09-27 | 2008-02-13 | 迪特尔·瓦格尔斯 | Flying device |
US7465236B2 (en) | 2002-09-27 | 2008-12-16 | Dieter Wagels | Flying arrangement |
US7722470B2 (en) | 2002-09-27 | 2010-05-25 | Dieter Wagels | Flying arrangement |
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