GB1215461A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB1215461A GB1215461A GB858467A GB858467A GB1215461A GB 1215461 A GB1215461 A GB 1215461A GB 858467 A GB858467 A GB 858467A GB 858467 A GB858467 A GB 858467A GB 1215461 A GB1215461 A GB 1215461A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- aircraft
- nozzles
- lift
- wings
- 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
- B64C29/005—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 the motors being fixed relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Turbines (AREA)
- Toys (AREA)
Abstract
1,215,461. Jet-lift aircraft. HAWKER SIDDELEY AVIATION Ltd. 14 Feb., 1968 [22 Feb., 1967], No. 8584/67. Heading B7G. A V.T.O.L. or S.T.O.L. aircraft comprises a continuously rated vectored thrust propulsion engine 11 having two laterally-spaced dirigible nozzles 12 at its aft end, and a lift engine 16 mounted (e.g. with its axis vertical) substantially between the two nozzles, so that the thrust lines 15 and 17 of the dirigible nozzles when directed downwardly, and of the lift engine, lie close to one another. The aircraft attitude may be controlled by auxiliary jets 19 (20), Fig. 3 (not shown), at the extremities of the fuselage 10 and wings 21, these jets being fed by either or both the engines 11, 16. The engine 16 has its intake 18 above the wings 21 to avoid ingestion of gases exhausted from the engine 11. The engines 11 and 16 may be mounted in a nacelle which may be attached to the aircraft wing 21.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB858467A GB1215461A (en) | 1967-02-22 | 1967-02-22 | Improvements in or relating to aircraft |
| DE19681556403 DE1556403A1 (en) | 1967-02-22 | 1968-02-21 | Engine arrangement for aircraft with vertical or short-range take-off properties |
| FR1562215D FR1562215A (en) | 1967-02-22 | 1968-02-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB858467A GB1215461A (en) | 1967-02-22 | 1967-02-22 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1215461A true GB1215461A (en) | 1970-12-09 |
Family
ID=9855287
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB858467A Expired GB1215461A (en) | 1967-02-22 | 1967-02-22 | Improvements in or relating to aircraft |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE1556403A1 (en) |
| FR (1) | FR1562215A (en) |
| GB (1) | GB1215461A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE450480B (en) * | 1982-08-30 | 1987-06-29 | Tech Gerete Und Entwicklungsge | STUFFED FLIGHT BODY |
-
1967
- 1967-02-22 GB GB858467A patent/GB1215461A/en not_active Expired
-
1968
- 1968-02-21 FR FR1562215D patent/FR1562215A/fr not_active Expired
- 1968-02-21 DE DE19681556403 patent/DE1556403A1/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| FR1562215A (en) | 1969-04-04 |
| DE1556403A1 (en) | 1970-01-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1480340A (en) | Aircraft | |
| GB1172782A (en) | Lift Fan Installations for Vertical Take Off and Landing Aircraft. | |
| GB1040510A (en) | Improvements in jet propulsion engines having thrust deflectors | |
| GB1009269A (en) | Improvements in or relating to aircraft | |
| GB1079296A (en) | A system and method for generating lift of aircraft | |
| US3164337A (en) | Jet aircraft with orientable nozzles for vertical or forward movement | |
| GB1258202A (en) | ||
| GB1012832A (en) | Improvements in or relating to vertical take off and landing aircraft | |
| GB1397068A (en) | Aircraft | |
| GB1157822A (en) | VTOL Aircraft | |
| GB1381646A (en) | Aircraft with short take-off and landing characteristics | |
| GB1187474A (en) | Improvements in or relating to Aircraft | |
| GB1041132A (en) | Improvements relating to the propulsion of aircraft | |
| GB1215461A (en) | Improvements in or relating to aircraft | |
| GB1076152A (en) | Improvements in aircraft power plants | |
| GB1071075A (en) | Improvements in aircraft | |
| GB1061397A (en) | Improvements in or relating to aircraft | |
| US5149016A (en) | Prop jet airplane propelling system | |
| GB1135946A (en) | Improvements in aircraft | |
| GB1029106A (en) | Aircraft | |
| GB788290A (en) | Improvements relating to aircraft | |
| GB951373A (en) | Improvements in or relating to aircraft | |
| US3172623A (en) | Aircraft power plant | |
| GB1302228A (en) | ||
| GB890703A (en) | An improved tiltable pod for jet power units on aircraft |