GB1111215A - Vtol/stol aircraft having turbine driven lift propellers or rotors - Google Patents
Vtol/stol aircraft having turbine driven lift propellers or rotorsInfo
- Publication number
- GB1111215A GB1111215A GB357166A GB357166A GB1111215A GB 1111215 A GB1111215 A GB 1111215A GB 357166 A GB357166 A GB 357166A GB 357166 A GB357166 A GB 357166A GB 1111215 A GB1111215 A GB 1111215A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotors
- nacelle
- wing
- aircraft
- vtol
- 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
- B64C29/0033—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 tiltable relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,111,215. V.T.O.L. aircraft. BÍLKOW G.m.b.H. 26 Jan., 1966 [2 Feb., 1965], No 3571/66. Headings B7G and B7W. A V.T.O.L. fixed-wing aircraft is propelled in forward flight by gas turbine engines 3 mounted above each wing 2 within extensions of nacelles 4 suspended below the wing. The front and rear end of each nacelle carries a lifting rotor 5 positioned as shown for take-off and landing and driven by a turbine 12, Fig. 2, in turn driven by jet gas from engine 3 diverted by a deflector 9, the turbines being connected to each other and to the rotors by gearing and shafting 17, 20, 22. The underside of each nacelle is provided with retractable slats 21 and during forward flight, with the jet gases directed rearwardly, the rotor blades are folded and swung into retracted positions within the nacelle. The jet propulsion engines and rotor-driving turbines may be housed within the fuselage and connected to the rotors by extended shafting and gearing.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB0080350 | 1965-02-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1111215A true GB1111215A (en) | 1968-04-24 |
Family
ID=6980679
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB357166A Expired GB1111215A (en) | 1965-02-02 | 1966-01-26 | Vtol/stol aircraft having turbine driven lift propellers or rotors |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1463582A (en) |
GB (1) | GB1111215A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2264679A (en) * | 1992-03-03 | 1993-09-08 | Secr Defence | Vtol aircraft. |
-
1966
- 1966-01-13 FR FR45848A patent/FR1463582A/en not_active Expired
- 1966-01-26 GB GB357166A patent/GB1111215A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2264679A (en) * | 1992-03-03 | 1993-09-08 | Secr Defence | Vtol aircraft. |
Also Published As
Publication number | Publication date |
---|---|
FR1463582A (en) | 1966-12-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3559921A (en) | Standing take-off and landing vehicle (a gem/stol vehicle) | |
GB1480340A (en) | Aircraft | |
GB1283042A (en) | Improvements relating to aircraft | |
GB1066360A (en) | Aircraft | |
GB1089549A (en) | Aircraft | |
GB1024969A (en) | Helicopter power plant | |
GB895590A (en) | Improvements relating to aircraft for vertical take-off and landing | |
GB927779A (en) | Vtol/stol aircraft | |
US3410506A (en) | Extensible rotor airplane | |
GB1411601A (en) | Ducted fan gas turbine engine supported by an aircraft wing mainspar | |
US3517898A (en) | Lift and propulsion device for a jet aircraft of the hybrid helicopter-autogyro type | |
GB885663A (en) | Improvement relating to aircraft | |
GB1146699A (en) | Compound rotorcraft | |
GB953301A (en) | Convertible helicopter | |
GB861480A (en) | Improvements in aircraft | |
GB1076152A (en) | Improvements in aircraft power plants | |
GB1111215A (en) | Vtol/stol aircraft having turbine driven lift propellers or rotors | |
US2605983A (en) | Gas turbine power plant and boundary layer control system for aircraft | |
GB1394177A (en) | Helicopters | |
US3285537A (en) | Vertical take off and landing aircraft | |
US2564370A (en) | Aircraft | |
GB1405737A (en) | Large flat based aircraft capable of hovering flight particularly for the transport of lengths of pipe line | |
GB900095A (en) | Air-craft having an annular wing and a propulsion means fitted into the latter | |
GB1175073A (en) | Improvements in or relating to Vertical Take-off and Landing Aircraft | |
GB1199923A (en) | Improvements in or relating to Aerodynamic Lift Producing Devices |