GB1252077A - - Google Patents
Info
- Publication number
- GB1252077A GB1252077A GB1233869A GB1252077DA GB1252077A GB 1252077 A GB1252077 A GB 1252077A GB 1233869 A GB1233869 A GB 1233869A GB 1252077D A GB1252077D A GB 1252077DA GB 1252077 A GB1252077 A GB 1252077A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzles
- duct
- nozzle
- terminating
- aircraft
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 239000012530 fluid Substances 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 238000001228 spectrum Methods 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1233869 | 1969-03-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1252077A true GB1252077A (de) | 1971-11-03 |
Family
ID=10002660
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1233869A Expired GB1252077A (de) | 1969-03-08 | 1969-03-08 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1252077A (de) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3520015A1 (de) * | 1985-06-04 | 1987-01-08 | Gerhard Nerenberg | Duesenanordnung bei einem triebwerk |
GB2231009A (en) * | 1984-11-17 | 1990-11-07 | Rolls Royce | Diverter valve with bypass duct obturator for twin gas turbine engine installation |
US4979363A (en) * | 1984-11-17 | 1990-12-25 | Rolls-Royce Plc | Diverter valve with bypass duct obturator |
GB2391846A (en) * | 2002-06-28 | 2004-02-18 | Ashley Christopher Bryant | Ducted air power plant |
-
1969
- 1969-03-08 GB GB1233869A patent/GB1252077A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2231009A (en) * | 1984-11-17 | 1990-11-07 | Rolls Royce | Diverter valve with bypass duct obturator for twin gas turbine engine installation |
US4979363A (en) * | 1984-11-17 | 1990-12-25 | Rolls-Royce Plc | Diverter valve with bypass duct obturator |
GB2231009B (en) * | 1984-11-17 | 1991-01-23 | Rolls Royce | Diverter valve with bypass duct obturator |
DE3520015A1 (de) * | 1985-06-04 | 1987-01-08 | Gerhard Nerenberg | Duesenanordnung bei einem triebwerk |
GB2391846A (en) * | 2002-06-28 | 2004-02-18 | Ashley Christopher Bryant | Ducted air power plant |
GB2391846B (en) * | 2002-06-28 | 2005-10-05 | Ashley Christopher Bryant | Ducted air power plant |
US7581381B2 (en) | 2002-06-28 | 2009-09-01 | Vtol Technologies Limited | Ducted air power plant |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |