GB951373A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB951373A GB951373A GB4665662A GB4665662A GB951373A GB 951373 A GB951373 A GB 951373A GB 4665662 A GB4665662 A GB 4665662A GB 4665662 A GB4665662 A GB 4665662A GB 951373 A GB951373 A GB 951373A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engines
- fitted
- engine
- rearwardly
- nacelle
- 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
- B64C29/0058—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 vertical jet
Abstract
951,373. Vertical take-off and landing aircraft. DORNIER-WERKE G.m.b.H. Dec. 11, 1962 [Dec. 19, 1961], No. 46656/62. Heading B7G. A vertical take-off and landing aircraft has a battery of lifting engines 5, 5<SP>1</SP>, 5<SP>11</SP>, 5<SP>111</SP>, at least the front one of which has means for deflecting its jet rearwardly to deflect the jets of other engines away from the vertical to reduce ground erosion. The deflecting means, shown fitted to the front engine only, may comprise an eyelid (Fig. 2) hingedly mounted on the engine, or a curved deflector 10 (Fig. 3), which may form part of a nacelle in which the engines are mounted, and which, when required, is moved rearwardly and swung into position 10<SP>1</SP>. Alternatively, the engine may be tilted (Fig. 4) with cascades 11 adjustable either to deflect the jet downwardly or rearwardly as required. The engines may be fitted in a nacelle, as shown, or in the wings or in the fuselage, and are fitted with deflectors 8 by which their jets can be deflected by a few degrees.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED37721A DE1219333B (en) | 1961-12-19 | 1961-12-19 | Airplane with lift engines arranged close together |
Publications (1)
Publication Number | Publication Date |
---|---|
GB951373A true GB951373A (en) | 1964-03-04 |
Family
ID=7043741
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4665662A Expired GB951373A (en) | 1961-12-19 | 1962-12-11 | Improvements in or relating to aircraft |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1219333B (en) |
FR (1) | FR1340795A (en) |
GB (1) | GB951373A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1237905B (en) * | 1964-04-16 | 1967-03-30 | M A N Turbo G M B H | Twin-flow turbine jet engine for aircraft taking off and landing vertically |
DE1274893B (en) * | 1966-03-03 | 1968-08-08 | M A N Turbo G M B H | Twin-flow turbine jet engine for aircraft taking off and landing vertically |
US4456203A (en) * | 1982-08-02 | 1984-06-26 | Ltv Aerospace And Defense Company | Aircraft propulsion system having a translatable, directionable exhaust nozzle |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1136339A (en) * | 1967-06-19 | 1968-12-11 | Rolls Royce | Gas turbine by-pass engine |
DE102017101320A1 (en) | 2017-01-24 | 2018-07-26 | Voestalpine Automotive Components Deutschland Gmbh | Method for fastening a baffle plate in a trough-like metal component and such a trough-like metal component with a baffle plate |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1109530B (en) * | 1959-01-08 | 1961-06-22 | Rolls Royce | Vertical take off aircraft |
-
1961
- 1961-12-19 DE DED37721A patent/DE1219333B/en active Pending
-
1962
- 1962-12-11 GB GB4665662A patent/GB951373A/en not_active Expired
- 1962-12-13 FR FR7604A patent/FR1340795A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1237905B (en) * | 1964-04-16 | 1967-03-30 | M A N Turbo G M B H | Twin-flow turbine jet engine for aircraft taking off and landing vertically |
DE1274893B (en) * | 1966-03-03 | 1968-08-08 | M A N Turbo G M B H | Twin-flow turbine jet engine for aircraft taking off and landing vertically |
US4456203A (en) * | 1982-08-02 | 1984-06-26 | Ltv Aerospace And Defense Company | Aircraft propulsion system having a translatable, directionable exhaust nozzle |
Also Published As
Publication number | Publication date |
---|---|
DE1219333B (en) | 1966-06-16 |
FR1340795A (en) | 1963-10-18 |
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