GB984955A - Nozzle for a jet engine - Google Patents
Nozzle for a jet engineInfo
- Publication number
- GB984955A GB984955A GB286564A GB286564A GB984955A GB 984955 A GB984955 A GB 984955A GB 286564 A GB286564 A GB 286564A GB 286564 A GB286564 A GB 286564A GB 984955 A GB984955 A GB 984955A
- Authority
- GB
- United Kingdom
- Prior art keywords
- downstream
- fixed
- jet
- nozzle
- jet engine
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Tires In General (AREA)
- Control Of Turbines (AREA)
Abstract
984,955. Jet propelled aircraft. ROLLSROYCE Ltd. Jan. 22, 1964, No. 2865/64. Heading B7G. An aircraft is provided with gas turbine jet lift engines 14 each having an outlet nozzle 15 comprising a fixed upstream part 16, a downstream part 17 rotatable, e.g. by a chain 23, or a gear, meshing with a pinion 24, about the axis of the upstream part to vary the flow direction of the jet gases, and an inner member tapering in the downstream direction and having an upstream part 26 fixed to the part 16, and a downstream part 27 fixed, e.g. by struts 30, to the downstream part 17.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB286564A GB984955A (en) | 1964-01-22 | 1964-01-22 | Nozzle for a jet engine |
DER39515A DE1242454B (en) | 1964-01-22 | 1964-12-21 | Jet nozzle with rotatable outlet part |
FR999421A FR1417902A (en) | 1964-01-22 | 1964-12-21 | Jet engine nozzle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB286564A GB984955A (en) | 1964-01-22 | 1964-01-22 | Nozzle for a jet engine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB984955A true GB984955A (en) | 1965-03-03 |
Family
ID=9747433
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB286564A Expired GB984955A (en) | 1964-01-22 | 1964-01-22 | Nozzle for a jet engine |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1242454B (en) |
GB (1) | GB984955A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1257021B (en) * | 1965-10-04 | 1967-12-21 | Ver Flugtechnische Werke Ges M | Airplane with a rotating hub nozzle |
DE1288439B (en) * | 1965-10-19 | 1969-01-30 | Rolls Royce | Airplane with jet engines, each with a large number of individual nozzles |
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 |
WO2008127260A1 (en) | 2006-06-09 | 2008-10-23 | Bell Helicopter Textron Inc. | Engine exhaust system with directional nozzle |
-
1964
- 1964-01-22 GB GB286564A patent/GB984955A/en not_active Expired
- 1964-12-21 DE DER39515A patent/DE1242454B/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1257021B (en) * | 1965-10-04 | 1967-12-21 | Ver Flugtechnische Werke Ges M | Airplane with a rotating hub nozzle |
DE1288439B (en) * | 1965-10-19 | 1969-01-30 | Rolls Royce | Airplane with jet engines, each with a large number of individual nozzles |
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 |
WO2008127260A1 (en) | 2006-06-09 | 2008-10-23 | Bell Helicopter Textron Inc. | Engine exhaust system with directional nozzle |
EP2032829A1 (en) * | 2006-06-09 | 2009-03-11 | Bell Helicopter Textron Inc. | Engine exhaust system with directional nozzle |
EP2032829A4 (en) * | 2006-06-09 | 2012-10-10 | Bell Helicopter Textron Inc | Engine exhaust system with directional nozzle |
Also Published As
Publication number | Publication date |
---|---|
DE1242454B (en) | 1967-06-15 |
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