GB688231A - Adjustable exhaust pipes for jet propelled aircraft - Google Patents
Adjustable exhaust pipes for jet propelled aircraftInfo
- Publication number
- GB688231A GB688231A GB25701/50A GB2570150A GB688231A GB 688231 A GB688231 A GB 688231A GB 25701/50 A GB25701/50 A GB 25701/50A GB 2570150 A GB2570150 A GB 2570150A GB 688231 A GB688231 A GB 688231A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet
- exhaust pipes
- adjustable exhaust
- propelled aircraft
- jet propelled
- 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
- B64C29/0091—Accessories not provided for elsewhere
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Exhaust Silencers (AREA)
Abstract
688,231. Jet-propulsion plant. STONE, W. C. Oct. 21, 1950, No. 25701/50. Class 110(iii) [Also in Group XXXIII] The end portion 13 of an aircraft jet discharge nozzle is flexible and connected to oppositely disposed pairs of cables 16 operable by control levers 17, 19 so that the jet may be deflected in any direction, the cables 16 passing through blocks 24 slidable along guides 20 under the influence of opposed compression springs 26 tending to return the blocks to their central positions.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25701/50A GB688231A (en) | 1950-10-21 | 1950-10-21 | Adjustable exhaust pipes for jet propelled aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25701/50A GB688231A (en) | 1950-10-21 | 1950-10-21 | Adjustable exhaust pipes for jet propelled aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB688231A true GB688231A (en) | 1953-03-04 |
Family
ID=10231899
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25701/50A Expired GB688231A (en) | 1950-10-21 | 1950-10-21 | Adjustable exhaust pipes for jet propelled aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB688231A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1192058B (en) * | 1962-07-28 | 1965-04-29 | Dornier Werke Gmbh | Beam deflection device made up of several pivotable rings arranged one behind the other |
DE1227781B (en) * | 1961-08-04 | 1966-10-27 | Ver Flugtechnische Werke Ges M | Dual-circuit jet engine for aircraft with jet deflector blades |
-
1950
- 1950-10-21 GB GB25701/50A patent/GB688231A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1227781B (en) * | 1961-08-04 | 1966-10-27 | Ver Flugtechnische Werke Ges M | Dual-circuit jet engine for aircraft with jet deflector blades |
DE1192058B (en) * | 1962-07-28 | 1965-04-29 | Dornier Werke Gmbh | Beam deflection device made up of several pivotable rings arranged one behind the other |
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