GB0121763D0 - A novel propulsion system for an aircraft - Google Patents
A novel propulsion system for an aircraftInfo
- Publication number
- GB0121763D0 GB0121763D0 GB0121763A GB0121763A GB0121763D0 GB 0121763 D0 GB0121763 D0 GB 0121763D0 GB 0121763 A GB0121763 A GB 0121763A GB 0121763 A GB0121763 A GB 0121763A GB 0121763 D0 GB0121763 D0 GB 0121763D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- propulsion system
- novel propulsion
- novel
- propulsion
- 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.)
- Withdrawn
Links
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
- F02K3/04—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/075—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
-
- 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
- F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
-
- 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
-
- 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
- F02K3/04—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
-
- 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
- F02K3/04—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/077—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 plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type the plant being of the multiple flow type, i.e. having three or more flows
-
- 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
-
- 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
- F02K3/12—Plants including a gas turbine driving a compressor or a ducted fan characterised by having more than one gas turbine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0121763A GB2379483A (en) | 2001-09-08 | 2001-09-08 | Augmented gas turbine propulsion system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0121763A GB2379483A (en) | 2001-09-08 | 2001-09-08 | Augmented gas turbine propulsion system |
Publications (2)
Publication Number | Publication Date |
---|---|
GB0121763D0 true GB0121763D0 (en) | 2001-10-31 |
GB2379483A GB2379483A (en) | 2003-03-12 |
Family
ID=9921758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB0121763A Withdrawn GB2379483A (en) | 2001-09-08 | 2001-09-08 | Augmented gas turbine propulsion system |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2379483A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8480350B2 (en) | 2006-10-12 | 2013-07-09 | United Technologies Corporation | Turbofan engine with variable bypass nozzle exit area and method of operation |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
CA2996284A1 (en) | 2015-09-02 | 2017-04-20 | Jetoptera, Inc. | Fluidic propulsive system |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
BR112019027805A2 (en) | 2017-06-27 | 2020-07-07 | Jetoptera, Inc. | configuration of vertical take-off and landing system for aerial vehicles |
CN109899177B (en) * | 2018-08-08 | 2023-02-17 | 珠海市蓝鹰贸易有限公司 | Multi-core aircraft with afterburner turbofan aviation power system and aircraft |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB948571A (en) * | 1962-10-08 | 1964-02-05 | Rolls Royce | Gas turbine jet propulsion engine |
GB1062376A (en) * | 1964-07-30 | 1967-03-22 | Gen Electric | Improvements in ducted fan powerplant |
US3547379A (en) * | 1967-09-18 | 1970-12-15 | Gen Electric | Aircraft nuclear propulsion system having an alternative power source |
US4043121A (en) * | 1975-01-02 | 1977-08-23 | General Electric Company | Two-spool variable cycle engine |
GB2001136A (en) * | 1977-07-12 | 1979-01-24 | Rolls Royce | Gas turbine jet propulsion engines |
FR2513697A1 (en) * | 1981-09-25 | 1983-04-01 | Snecma | PROPULSION ENGINE, IN PARTICULAR FOR SUPERSONIC AIRCRAFT |
US4815282A (en) * | 1987-02-24 | 1989-03-28 | Teledyne Industries, Inc. | Turbocharged compund cycle ducted fan engine system |
-
2001
- 2001-09-08 GB GB0121763A patent/GB2379483A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2379483A (en) | 2003-03-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |