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RU2011128427A - GAS TURBINE ENGINE - Google Patents

GAS TURBINE ENGINE Download PDF

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Publication number
RU2011128427A
RU2011128427A RU2011128427/06A RU2011128427A RU2011128427A RU 2011128427 A RU2011128427 A RU 2011128427A RU 2011128427/06 A RU2011128427/06 A RU 2011128427/06A RU 2011128427 A RU2011128427 A RU 2011128427A RU 2011128427 A RU2011128427 A RU 2011128427A
Authority
RU
Russia
Prior art keywords
gas turbine
turbine engine
engine
compressor
combustion chamber
Prior art date
Application number
RU2011128427/06A
Other languages
Russian (ru)
Inventor
Олег Владимирович Савченко
Сергей Алексеевич Ялдин
Original Assignee
Олег Владимирович Савченко
Сергей Алексеевич Ялдин
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 Олег Владимирович Савченко, Сергей Алексеевич Ялдин filed Critical Олег Владимирович Савченко
Priority to RU2011128427/06A priority Critical patent/RU2011128427A/en
Publication of RU2011128427A publication Critical patent/RU2011128427A/en

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Abstract

Газотурбинный двигатель, включающий компрессор, камеру сгорания и турбину, отличающийся тем, что, с целью повышения экономичности газотурбинного двигателя, в тракте двигателя на выходе из турбины установлен теплообменник-испаритель теплового насоса, а теплообменник-конденсатор теплового насоса установлен в тракте двигателя между компрессором и камерой сгорания.A gas turbine engine including a compressor, a combustion chamber and a turbine, characterized in that, in order to increase the efficiency of the gas turbine engine, a heat pump-heat exchanger-evaporator is installed in the engine path at the outlet of the turbine, and a heat pump-heat exchanger-condenser is installed in the engine path between the compressor and combustion chamber.

Claims (1)

Газотурбинный двигатель, включающий компрессор, камеру сгорания и турбину, отличающийся тем, что, с целью повышения экономичности газотурбинного двигателя, в тракте двигателя на выходе из турбины установлен теплообменник-испаритель теплового насоса, а теплообменник-конденсатор теплового насоса установлен в тракте двигателя между компрессором и камерой сгорания. A gas turbine engine including a compressor, a combustion chamber and a turbine, characterized in that, in order to increase the efficiency of the gas turbine engine, a heat pump-heat exchanger-evaporator is installed in the engine path at the outlet of the turbine, and a heat pump-heat exchanger-condenser is installed in the engine path between the compressor and combustion chamber.
RU2011128427/06A 2011-07-08 2011-07-08 GAS TURBINE ENGINE RU2011128427A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011128427/06A RU2011128427A (en) 2011-07-08 2011-07-08 GAS TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011128427/06A RU2011128427A (en) 2011-07-08 2011-07-08 GAS TURBINE ENGINE

Publications (1)

Publication Number Publication Date
RU2011128427A true RU2011128427A (en) 2013-01-20

Family

ID=48805006

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011128427/06A RU2011128427A (en) 2011-07-08 2011-07-08 GAS TURBINE ENGINE

Country Status (1)

Country Link
RU (1) RU2011128427A (en)

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20130110