RU2001130397A - METHOD OF OPERATION OF A GAS TURBO-DETANDER INSTALLATION - Google Patents

METHOD OF OPERATION OF A GAS TURBO-DETANDER INSTALLATION Download PDF

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Publication number
RU2001130397A
RU2001130397A RU2001130397/06A RU2001130397A RU2001130397A RU 2001130397 A RU2001130397 A RU 2001130397A RU 2001130397/06 A RU2001130397/06 A RU 2001130397/06A RU 2001130397 A RU2001130397 A RU 2001130397A RU 2001130397 A RU2001130397 A RU 2001130397A
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RU
Russia
Prior art keywords
installation
detander
gas turbo
gas turbine
turboexpander
Prior art date
Application number
RU2001130397/06A
Other languages
Russian (ru)
Inventor
Валерий Николаевич Веселов
Сергей Георгиевич Валюхов
Виталий Викторович Ходус
Original Assignee
Валерий Николаевич Веселов
Сергей Георгиевич Валюхов
Виталий Викторович Ходус
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.)
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Application filed by Валерий Николаевич Веселов, Сергей Георгиевич Валюхов, Виталий Викторович Ходус filed Critical Валерий Николаевич Веселов
Priority to RU2001130397/06A priority Critical patent/RU2001130397A/en
Publication of RU2001130397A publication Critical patent/RU2001130397A/en

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Claims (1)

Способ работы газотурбодетандерной установки, заключающийся в подогреве природного газа высокого давления выхлопными газами газотурбинного двигателя с последующей подачей в турбодетандер, отличающийся тем, что получаемую мощность турбодетандера передают только компрессору, а нагнетаемый им воздух дополнительно нагревают выхлопными газами газотурбинного двигателя.The method of operation of a gas turbine expander installation, which consists in heating high-pressure natural gas with the exhaust gases of a gas turbine engine and then supplying it to a turboexpander, characterized in that the received power of the turboexpander is transmitted only to the compressor, and the air pumped by it is additionally heated by the exhaust gases of the gas turbine engine.
RU2001130397/06A 2001-11-13 2001-11-13 METHOD OF OPERATION OF A GAS TURBO-DETANDER INSTALLATION RU2001130397A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001130397/06A RU2001130397A (en) 2001-11-13 2001-11-13 METHOD OF OPERATION OF A GAS TURBO-DETANDER INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001130397/06A RU2001130397A (en) 2001-11-13 2001-11-13 METHOD OF OPERATION OF A GAS TURBO-DETANDER INSTALLATION

Publications (1)

Publication Number Publication Date
RU2001130397A true RU2001130397A (en) 2003-06-27

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001130397/06A RU2001130397A (en) 2001-11-13 2001-11-13 METHOD OF OPERATION OF A GAS TURBO-DETANDER INSTALLATION

Country Status (1)

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RU (1) RU2001130397A (en)

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Legal Events

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FA93 Acknowledgement of application withdrawn (no request for examination)

Effective date: 20051110