RU96104986A - METHOD OF WORK OF GAS-TURBINE INSTALLATION - Google Patents

METHOD OF WORK OF GAS-TURBINE INSTALLATION

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Publication number
RU96104986A
RU96104986A RU96104986/06A RU96104986A RU96104986A RU 96104986 A RU96104986 A RU 96104986A RU 96104986/06 A RU96104986/06 A RU 96104986/06A RU 96104986 A RU96104986 A RU 96104986A RU 96104986 A RU96104986 A RU 96104986A
Authority
RU
Russia
Prior art keywords
heat
stage
turbine installation
gas
work
Prior art date
Application number
RU96104986/06A
Other languages
Russian (ru)
Other versions
RU2138660C1 (en
Inventor
Б.Х. Перельштейн
Original Assignee
Б.Х. Перельштейн
Filing date
Publication date
Application filed by Б.Х. Перельштейн filed Critical Б.Х. Перельштейн
Priority to RU96104986A priority Critical patent/RU2138660C1/en
Priority claimed from RU96104986A external-priority patent/RU2138660C1/en
Publication of RU96104986A publication Critical patent/RU96104986A/en
Application granted granted Critical
Publication of RU2138660C1 publication Critical patent/RU2138660C1/en

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Claims (1)

Способ работы газотурбинной установки, включающий в первом рабочем контуре процессы сжатия в компрессоре, ступенчатый подвод тепла в камерах сгорания, расширения на турбинах, ступенчаты отвод тепла во второй контур в теплообменниках, отличающийся тем, что по крайней мере один раз в первом рабочем контуре последовательно осуществляют первую ступень подвода тепла и первую ступень отвода тепла до начала процесса сжатия, рабочее тело первого рабочего контура частично срабатывают на турбинах, охлаждают в последующей ступени отвода тепла и расширяют на турбине низкого давления и подают во внешнюю среду.The method of operation of a gas turbine installation, including compression processes in the compressor in the first working circuit, stepwise heat supply in the combustion chambers, expansion on the turbines, heat transfer to the second circuit in heat exchangers is stepped, characterized in that at least once in the first working circuit they are sequentially carried out the first stage of heat supply and the first stage of heat removal before the start of the compression process, the working fluid of the first working circuit is partially activated on the turbines, cooled in the next stage of heat removal and expands it to the low pressure turbine and supplied to the external environment.
RU96104986A 1996-03-14 1996-03-14 Gas turbine plant operation method RU2138660C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96104986A RU2138660C1 (en) 1996-03-14 1996-03-14 Gas turbine plant operation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96104986A RU2138660C1 (en) 1996-03-14 1996-03-14 Gas turbine plant operation method

Publications (2)

Publication Number Publication Date
RU96104986A true RU96104986A (en) 1998-06-20
RU2138660C1 RU2138660C1 (en) 1999-09-27

Family

ID=20178069

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96104986A RU2138660C1 (en) 1996-03-14 1996-03-14 Gas turbine plant operation method

Country Status (1)

Country Link
RU (1) RU2138660C1 (en)

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