GB2240813B - Improvements in hypersonic and trans atmospheric propulsion - Google Patents
Improvements in hypersonic and trans atmospheric propulsionInfo
- Publication number
- GB2240813B GB2240813B GB8620857A GB8620857A GB2240813B GB 2240813 B GB2240813 B GB 2240813B GB 8620857 A GB8620857 A GB 8620857A GB 8620857 A GB8620857 A GB 8620857A GB 2240813 B GB2240813 B GB 2240813B
- Authority
- GB
- United Kingdom
- Prior art keywords
- hypersonic
- trans
- atmospheric propulsion
- propulsion
- atmospheric
- 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 - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/224—Heating fuel before feeding to the burner
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
- F02K9/46—Feeding propellants using pumps
- F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
- F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
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 |
---|---|---|---|
GB8620857A GB2240813B (en) | 1986-08-28 | 1986-08-28 | Improvements in hypersonic and trans atmospheric propulsion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8620857A GB2240813B (en) | 1986-08-28 | 1986-08-28 | Improvements in hypersonic and trans atmospheric propulsion |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2240813A GB2240813A (en) | 1991-08-14 |
GB2240813B true GB2240813B (en) | 1991-11-27 |
Family
ID=10603346
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8620857A Expired - Fee Related GB2240813B (en) | 1986-08-28 | 1986-08-28 | Improvements in hypersonic and trans atmospheric propulsion |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2240813B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108910059A (en) * | 2018-07-18 | 2018-11-30 | 中国人民解放军国防科技大学 | Precooling type air inlet and hypersonic aircraft |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2241536A (en) * | 1988-03-23 | 1991-09-04 | Rolls Royce Plc | Intakes of aerospace propulsors |
DE4131913A1 (en) * | 1991-09-25 | 1993-04-08 | Mtu Muenchen Gmbh | COOLING DEVICE FOR HYPERSONIC AIR JET ENGINES |
US5392595A (en) * | 1993-08-06 | 1995-02-28 | United Technologies Corporation | Endothermic fuel energy management system |
GB2295858A (en) * | 1994-12-09 | 1996-06-12 | Rolls Royce Plc | Liquid hydrogen fuelled powerplant |
DE19617916B4 (en) * | 1996-05-03 | 2007-02-01 | Airbus Deutschland Gmbh | Evaporator for evaporating a cryogenic liquid medium |
CN106014637B (en) * | 2016-06-07 | 2017-12-19 | 中国人民解放军国防科学技术大学 | Air precooling compresses aero-engine and Hypersonic Aircraft |
US10989117B2 (en) * | 2018-09-14 | 2021-04-27 | Raytheon Technologies Corporation | Hybrid expander cycle with pre-compression cooling and turbo-generator |
US11077949B2 (en) * | 2018-10-05 | 2021-08-03 | The Boeing Company | Dual turbine thermal management system (TMS) |
GB2584094B (en) * | 2019-05-20 | 2022-01-26 | Rolls Royce Plc | Engine |
EP3978807A3 (en) | 2020-09-30 | 2022-07-06 | Rolls-Royce plc | Direct fuel injection system |
FR3120393A1 (en) * | 2021-03-08 | 2022-09-09 | Safran | Fuel conditioning system and method configured to supply an aircraft turbine engine with fuel from a cryogenic tank |
EP4187070A1 (en) * | 2021-11-29 | 2023-05-31 | Airbus Operations, S.L.U. | Gas turbine |
CN114352436B (en) * | 2021-12-15 | 2023-01-20 | 西安航天动力研究所 | Metal powder fuel air-water cross-medium engine and control method thereof |
FR3141212A1 (en) * | 2022-10-21 | 2024-04-26 | Safran | Fuel conditioning system for supplying an aircraft turbomachine, method of supplying a turbomachine |
WO2024088516A1 (en) * | 2022-10-25 | 2024-05-02 | Destinus Sa | Air turborocket apparatus with boiler |
-
1986
- 1986-08-28 GB GB8620857A patent/GB2240813B/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108910059A (en) * | 2018-07-18 | 2018-11-30 | 中国人民解放军国防科技大学 | Precooling type air inlet and hypersonic aircraft |
CN108910059B (en) * | 2018-07-18 | 2020-07-31 | 中国人民解放军国防科技大学 | Precooling type air inlet and hypersonic aircraft |
Also Published As
Publication number | Publication date |
---|---|
GB2240813A (en) | 1991-08-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19920828 |