GB387264A - Improvements in and relating to the regulation of the performance of gas turbines - Google Patents

Improvements in and relating to the regulation of the performance of gas turbines

Info

Publication number
GB387264A
GB387264A GB23885/32A GB2388532A GB387264A GB 387264 A GB387264 A GB 387264A GB 23885/32 A GB23885/32 A GB 23885/32A GB 2388532 A GB2388532 A GB 2388532A GB 387264 A GB387264 A GB 387264A
Authority
GB
United Kingdom
Prior art keywords
turbine
regulation
performance
gas turbines
precompressor
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
GB23885/32A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB387264A publication Critical patent/GB387264A/en
Expired legal-status Critical Current

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Abstract

387,264. Gas turbines. WALTER, H., 26, Sturmvogelstrasse, Johannisthal, Berlin. Aug. 26, 1932, No. 23885. Convention date, Aug. 26, 1931. [Class 110 (iii).] In a gas-turbine plant working under vacuum and comprising an air precompressor A, a combustion chamber B, a load turbine T1 and a turbine T2 driving a compressor C which draws the exhaust through a cooler K up to atmospheric pressure, the useful turbine performance is regulated by regulating the precompressor A. Regulation may be effected by providing a cut-off valve or a throttle valve, or by varying the speed. The compressors A, C need not be on the same shaft.
GB23885/32A 1931-08-26 1932-08-26 Improvements in and relating to the regulation of the performance of gas turbines Expired GB387264A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE387264X 1931-08-26

Publications (1)

Publication Number Publication Date
GB387264A true GB387264A (en) 1933-02-02

Family

ID=6371102

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23885/32A Expired GB387264A (en) 1931-08-26 1932-08-26 Improvements in and relating to the regulation of the performance of gas turbines

Country Status (1)

Country Link
GB (1) GB387264A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623357A (en) * 1945-09-06 1952-12-30 Birmann Rudolph Gas turbine power plant having means to cool and means to compress combustion products passing through the turbine
DE1009434B (en) * 1954-02-05 1957-05-29 Associated British Oil Engines Gas turbine with piston propellant gas generator
US2898731A (en) * 1953-09-11 1959-08-11 Power Jets Res & Dev Ltd Power producing equipment incorporating gas turbine plant
US2977753A (en) * 1954-02-13 1961-04-04 Rech Etudes Prod Improvements in continuous flow gas engines

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2623357A (en) * 1945-09-06 1952-12-30 Birmann Rudolph Gas turbine power plant having means to cool and means to compress combustion products passing through the turbine
US2898731A (en) * 1953-09-11 1959-08-11 Power Jets Res & Dev Ltd Power producing equipment incorporating gas turbine plant
DE1009434B (en) * 1954-02-05 1957-05-29 Associated British Oil Engines Gas turbine with piston propellant gas generator
US2977753A (en) * 1954-02-13 1961-04-04 Rech Etudes Prod Improvements in continuous flow gas engines

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