GB2240813B - Improvements in hypersonic and trans atmospheric propulsion - Google Patents

Improvements in hypersonic and trans atmospheric propulsion

Info

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
Application number
GB8620857A
Other versions
GB2240813A (en
Inventor
Ralph Murch Denning
Gordon Manns Lewis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB8620857A priority Critical patent/GB2240813B/en
Publication of GB2240813A publication Critical patent/GB2240813A/en
Application granted granted Critical
Publication of GB2240813B publication Critical patent/GB2240813B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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)
GB8620857A 1986-08-28 1986-08-28 Improvements in hypersonic and trans atmospheric propulsion Expired - Fee Related GB2240813B (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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