GB870266A - Multistage high altitude engine with single combustion stack - Google Patents

Multistage high altitude engine with single combustion stack

Info

Publication number
GB870266A
GB870266A GB2528557A GB2528557A GB870266A GB 870266 A GB870266 A GB 870266A GB 2528557 A GB2528557 A GB 2528557A GB 2528557 A GB2528557 A GB 2528557A GB 870266 A GB870266 A GB 870266A
Authority
GB
United Kingdom
Prior art keywords
hydrogen
heat
turbine
burnt
supplied
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
Application number
GB2528557A
Inventor
Randolph Samuel Rae
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.)
Garrett Corp
Original Assignee
Garrett Corp
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 Garrett Corp filed Critical Garrett Corp
Priority to GB2528557A priority Critical patent/GB870266A/en
Publication of GB870266A publication Critical patent/GB870266A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/08Heating air supply before combustion, e.g. by exhaust gases
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof

Abstract

870,266. Generating combustion products under pressure. GARRETT CORPORATION. Aug. 9, 1957, No. 25285/57. Class 51 (1). [Also in Group XXVI] A multistage turbine is supplied with heated hydrogen gas as a working fluid. The exhaust hydrogen from the final stage is burnt, with an oxidant, in one side of a heat-exchanger to heat the supply hydrogen to the turbine. The three turbine stages 31, 33, 37 are connected through heat-exchangers 22, 27 and are supplied with hydrogen from tank 12 through the heat-exchanger 17. The latter is heated by exhaust hydrogen from the stage 37, burnt in combustion chamber 39 with liquid oxygen from tank 41. After leaving 17 the hydrogen is cooled in heat-exchangers 22, 27 before entry to the turbine first stage 31. 22 and 27 heat the hydrogen before entry to the succeeding stages 33, 37. In the case of an aircraft engine, the combustion chamber 39 may be supplied with either oxygen or air. In addition, unburnt hydrogen leaving the heatexchanger is burnt in an after-burner in the propulsion unit nozzle. Specification 870,271 is referred to.
GB2528557A 1957-08-09 1957-08-09 Multistage high altitude engine with single combustion stack Expired GB870266A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2528557A GB870266A (en) 1957-08-09 1957-08-09 Multistage high altitude engine with single combustion stack

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2528557A GB870266A (en) 1957-08-09 1957-08-09 Multistage high altitude engine with single combustion stack

Publications (1)

Publication Number Publication Date
GB870266A true GB870266A (en) 1961-06-14

Family

ID=10225233

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2528557A Expired GB870266A (en) 1957-08-09 1957-08-09 Multistage high altitude engine with single combustion stack

Country Status (1)

Country Link
GB (1) GB870266A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636674A1 (en) * 1988-09-16 1990-03-23 Gen Electric DEVICE AND METHOD FOR GENERATING ELECTRICITY

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636674A1 (en) * 1988-09-16 1990-03-23 Gen Electric DEVICE AND METHOD FOR GENERATING ELECTRICITY
GB2225059A (en) * 1988-09-16 1990-05-23 Gen Electric Gas turbine electricity generation

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