GB1386014A - Jet pipe and gas deflector for a gas turbine engine - Google Patents
Jet pipe and gas deflector for a gas turbine engineInfo
- Publication number
- GB1386014A GB1386014A GB2093272A GB2093272A GB1386014A GB 1386014 A GB1386014 A GB 1386014A GB 2093272 A GB2093272 A GB 2093272A GB 2093272 A GB2093272 A GB 2093272A GB 1386014 A GB1386014 A GB 1386014A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet pipe
- cowl
- gas
- turbine engine
- deflecting
- 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
-
- 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
- B64C29/0066—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 horizontal jet and jet deflector
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
1386014 Deflecting propulsion jets ROLLSROYCE (1971) Ltd 5 May 1972 20932/72 Heading B7G Jet deflecting apparatus mounting in a jet pipe 18 comprises a hollow partially conical member or cowl 26 mounted within the jet pipe above an opening therein leading to a secondary gas deflecting nozzle 24, both the jet pipe and the cowl being double-walled so as to provide passages 42, 43 for cooling air flow. The base of the cowl 26 is formed as an annulus 28 the cowl being mounted for rotation by a gear drive 32, 44 in bearings 34, 38 with its axis 36 intersecting the axis and wall of the jet pipe so that pipe 18 or nozzle 24 are selectively obturated.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2093272A GB1386014A (en) | 1972-05-05 | 1972-05-05 | Jet pipe and gas deflector for a gas turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2093272A GB1386014A (en) | 1972-05-05 | 1972-05-05 | Jet pipe and gas deflector for a gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1386014A true GB1386014A (en) | 1975-03-05 |
Family
ID=10154251
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2093272A Expired GB1386014A (en) | 1972-05-05 | 1972-05-05 | Jet pipe and gas deflector for a gas turbine engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1386014A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2596809A1 (en) * | 1986-04-08 | 1987-10-09 | Rolls Royce | IMPROVEMENTS IN AIRCRAFT FLYING TUTERS |
CN111186569A (en) * | 2019-11-15 | 2020-05-22 | 陕西飞机工业(集团)有限公司 | Vertical lift fixed wing aircraft |
-
1972
- 1972-05-05 GB GB2093272A patent/GB1386014A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2596809A1 (en) * | 1986-04-08 | 1987-10-09 | Rolls Royce | IMPROVEMENTS IN AIRCRAFT FLYING TUTERS |
CN111186569A (en) * | 2019-11-15 | 2020-05-22 | 陕西飞机工业(集团)有限公司 | Vertical lift fixed wing aircraft |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |