GB471887A - Working process and apparatus for gas turbines - Google Patents

Working process and apparatus for gas turbines

Info

Publication number
GB471887A
GB471887A GB34106/35A GB3410635A GB471887A GB 471887 A GB471887 A GB 471887A GB 34106/35 A GB34106/35 A GB 34106/35A GB 3410635 A GB3410635 A GB 3410635A GB 471887 A GB471887 A GB 471887A
Authority
GB
United Kingdom
Prior art keywords
turbine
pipe
gas
air
heated
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
GB34106/35A
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.)
GYOERGY JENDRASSIK
Original Assignee
GYOERGY JENDRASSIK
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 GYOERGY JENDRASSIK filed Critical GYOERGY JENDRASSIK
Publication of GB471887A publication Critical patent/GB471887A/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

Abstract

471,887. Gas turbine plant. JENDRASSIK, G. Dec. 9, 1935, No. 34106. Convention date, April 1. [Class 110 (iii)] The gas for a gas turbine plant is compressed by a multi-stage compressor to not more than eight times its initial pressure following which it is heated to at least 70 per cent of the highest temperature of the working cycle in a periodically operating heat exchange device heated by exhaust gases whereupon it is passed to the turbine in which fuel is burnt upon admission and/or during expansion. The Figure shows a turbine 1 and a triple section heat-exchanger 24<1>. Air is supplied by a rotary compressor to a pipe 23. from which it passes under the control of valves 26<1>, 31<1> through one of the sections of the heat-storer to the inlet pipe 25 of the turbine. The exhaust of the turbine passes through the other sections of the heatstorer to pipe 30 and to atmosphere. Periodically the valves, which are driven by an electric motor, are actuated so that the compressed air is passed to a section which has just been heated, and exhaust gas is diverted to the previously used section. Fuel is supplied to intermediate stages of the turbine by a pipe 11 and may be also at the point of admission. Additional air may be admitted from a pipe 12. In a modification, the exhaust gases are returned to the compressor and extra air is introduced.
GB34106/35A 1935-04-01 1935-12-09 Working process and apparatus for gas turbines Expired GB471887A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
HU471887X 1935-04-01

Publications (1)

Publication Number Publication Date
GB471887A true GB471887A (en) 1937-09-09

Family

ID=10979278

Family Applications (1)

Application Number Title Priority Date Filing Date
GB34106/35A Expired GB471887A (en) 1935-04-01 1935-12-09 Working process and apparatus for gas turbines

Country Status (2)

Country Link
ES (1) ES141849A1 (en)
GB (1) GB471887A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2557131A (en) * 1948-02-20 1951-06-19 Charles H Miller Gas turbine and cycle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2557131A (en) * 1948-02-20 1951-06-19 Charles H Miller Gas turbine and cycle

Also Published As

Publication number Publication date
ES141849A1 (en) 1936-09-16

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