RU2014125271A - GAS-TURBINE ENGINE WITH SCREW COMPRESSOR - Google Patents

GAS-TURBINE ENGINE WITH SCREW COMPRESSOR Download PDF

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Publication number
RU2014125271A
RU2014125271A RU2014125271/06A RU2014125271A RU2014125271A RU 2014125271 A RU2014125271 A RU 2014125271A RU 2014125271/06 A RU2014125271/06 A RU 2014125271/06A RU 2014125271 A RU2014125271 A RU 2014125271A RU 2014125271 A RU2014125271 A RU 2014125271A
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RU
Russia
Prior art keywords
turbine engine
compressor
screw compressor
gas
gas turbine
Prior art date
Application number
RU2014125271/06A
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Russian (ru)
Inventor
Александр Владимирович Плетнёв
Original Assignee
Александр Владимирович Плетнёв
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Publication date
Application filed by Александр Владимирович Плетнёв filed Critical Александр Владимирович Плетнёв
Priority to RU2014125271/06A priority Critical patent/RU2014125271A/en
Publication of RU2014125271A publication Critical patent/RU2014125271A/en

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Abstract

1. Газотурбинный двигатель, содержащий компрессор для выработки и подачи сжатого воздуха в камеру сгорания, отличающийся тем, что в качестве компрессора используют винтовой компрессор.2. Газотурбинный двигатель по п. 1, отличающийся тем, что на входе в камеру сгорания содержит рекуператор, через который проходят газообразные продукты сгорания топлива.1. A gas turbine engine containing a compressor for generating and supplying compressed air to the combustion chamber, characterized in that a screw compressor is used as a compressor. A gas turbine engine according to claim 1, characterized in that at the entrance to the combustion chamber contains a recuperator through which the gaseous products of combustion of fuel pass.

Claims (2)

1. Газотурбинный двигатель, содержащий компрессор для выработки и подачи сжатого воздуха в камеру сгорания, отличающийся тем, что в качестве компрессора используют винтовой компрессор.1. A gas turbine engine containing a compressor for generating and supplying compressed air to a combustion chamber, characterized in that a screw compressor is used as a compressor. 2. Газотурбинный двигатель по п. 1, отличающийся тем, что на входе в камеру сгорания содержит рекуператор, через который проходят газообразные продукты сгорания топлива. 2. A gas turbine engine according to claim 1, characterized in that at the entrance to the combustion chamber contains a recuperator through which the gaseous products of combustion of fuel pass.
RU2014125271/06A 2014-06-20 2014-06-20 GAS-TURBINE ENGINE WITH SCREW COMPRESSOR RU2014125271A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2014125271/06A RU2014125271A (en) 2014-06-20 2014-06-20 GAS-TURBINE ENGINE WITH SCREW COMPRESSOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014125271/06A RU2014125271A (en) 2014-06-20 2014-06-20 GAS-TURBINE ENGINE WITH SCREW COMPRESSOR

Publications (1)

Publication Number Publication Date
RU2014125271A true RU2014125271A (en) 2014-10-27

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014125271/06A RU2014125271A (en) 2014-06-20 2014-06-20 GAS-TURBINE ENGINE WITH SCREW COMPRESSOR

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RU (1) RU2014125271A (en)

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