GB828884A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB828884A GB828884A GB3687054A GB3687054A GB828884A GB 828884 A GB828884 A GB 828884A GB 3687054 A GB3687054 A GB 3687054A GB 3687054 A GB3687054 A GB 3687054A GB 828884 A GB828884 A GB 828884A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- fans
- gases
- turbine
- 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
- B64C29/0016—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 free or ducted propellers or by blowers
- B64C29/0025—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 free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
828,884. Gas turbine plant. BOULTON PAUL AIRCRAFT Ltd. March 21, 1956 [Dec. 21, 1954], No. 36870/54. Class 110(3). [Also in Group XXXIII] Direct lift for an aircraft is provided by means of two or more fans mounted for rotation about a common axis parallel to the axis of yaw and adapted to be driven in opposite or alternate directions. As shown in Fig. 1, part or the whole of the exhaust gases of the gas turbine engines 2, 3 may be diverted by means of valves 21-24 into volutes 12 and 15 and used to drive the fans. Referring to Fig. 2, the gases from the volutes discharge through nozzles 113 on to turbine blades 13 mounted on the outside of a peripheral ring carried on the fan blades 6 ; the gases then pass through fixed guide vanes 19 to the turbine blades 18 mounted on the fan blades 7. By appropriately relating the angles of the blades 6 and 13 on the upper fan and turbine assembly to the angles of the blades 7 and 18 of the lower assembly, an aerodynamic meshing effect is obtained which causes the fans to contra-rotate at the required rotational speed without the aid of any mechanical gearing between them.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3687054A GB828884A (en) | 1954-12-21 | 1954-12-21 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3687054A GB828884A (en) | 1954-12-21 | 1954-12-21 | Improvements in or relating to aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB828884A true GB828884A (en) | 1960-02-24 |
Family
ID=10391836
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3687054A Expired GB828884A (en) | 1954-12-21 | 1954-12-21 | Improvements in or relating to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB828884A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1235149B (en) * | 1962-01-23 | 1967-02-23 | Ryan Aeronautical Co | Blower for a wing blower screw plane |
US3519224A (en) * | 1966-03-18 | 1970-07-07 | Turbo Circle Wing Inc | Vertical takeoff and landing aircraft |
GB2209314A (en) * | 1987-09-02 | 1989-05-10 | Manuel Munoz Saiz | Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft |
GB2261203A (en) * | 1991-11-08 | 1993-05-12 | Keith Ralbert Sherriff | VTOL Aircraft |
GB2264679A (en) * | 1992-03-03 | 1993-09-08 | Secr Defence | Vtol aircraft. |
-
1954
- 1954-12-21 GB GB3687054A patent/GB828884A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1235149B (en) * | 1962-01-23 | 1967-02-23 | Ryan Aeronautical Co | Blower for a wing blower screw plane |
US3519224A (en) * | 1966-03-18 | 1970-07-07 | Turbo Circle Wing Inc | Vertical takeoff and landing aircraft |
GB2209314A (en) * | 1987-09-02 | 1989-05-10 | Manuel Munoz Saiz | Lifting arrangement by direct thrust of the engine flow to vertical take-off aircraft |
GB2261203A (en) * | 1991-11-08 | 1993-05-12 | Keith Ralbert Sherriff | VTOL Aircraft |
GB2261203B (en) * | 1991-11-08 | 1996-02-28 | Keith Ralbert Sherriff | A V.T.O.L hover bike aircraft |
GB2264679A (en) * | 1992-03-03 | 1993-09-08 | Secr Defence | Vtol aircraft. |
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