RU2015143945A - TWO-GAS TURBINE ENGINE - Google Patents

TWO-GAS TURBINE ENGINE Download PDF

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Publication number
RU2015143945A
RU2015143945A RU2015143945A RU2015143945A RU2015143945A RU 2015143945 A RU2015143945 A RU 2015143945A RU 2015143945 A RU2015143945 A RU 2015143945A RU 2015143945 A RU2015143945 A RU 2015143945A RU 2015143945 A RU2015143945 A RU 2015143945A
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RU
Russia
Prior art keywords
gas turbine
turbine engine
shaft
turbine
centrifugal
Prior art date
Application number
RU2015143945A
Other languages
Russian (ru)
Inventor
Виктор Серафимович Бахирев
Original Assignee
Виктор Серафимович Бахирев
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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Publication date
Application filed by Виктор Серафимович Бахирев filed Critical Виктор Серафимович Бахирев
Priority to RU2015143945A priority Critical patent/RU2015143945A/en
Publication of RU2015143945A publication Critical patent/RU2015143945A/en

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Claims (1)

Двухвальный газотурбинный двигатель, содержащий входное устройство с воздухоочистителем, статор с рубашкой охлаждения, ротор центробежного компрессора с турбиной и опорами, ротор турбокомпрессора выполнен центробежным с одной ступицей на одном диске, силовая турбина выполнена центробежной многоступенчатой, статор по окружности имеет сопловые окна в количестве равном числу камер сгорания, отличающийся тем, что корпус двухвального газотурбинного двигателя выполнен из двух частей, в первой его половине имеется входное устройство, вал с компрессором, газотурбинный двигатель с камерами сгорания, диском с окнами входа и выхода перед турбиной, чередующая глухой частью и ее лопатками, за ними находится направляющий аппарат, далее в другой части корпуса расположен второй вал с тяговой турбиной, а за ней по окружности прилегает сборник отработанных продуктов сгорания с выхлопными патрубками.A twin-shaft gas turbine engine containing an inlet device with an air purifier, a stator with a cooling jacket, a rotor of a centrifugal compressor with a turbine and bearings, a rotor of a turbocompressor is made centrifugal with one hub on one disk, a power turbine is made of a centrifugal multistage, the stator around the circumference has nozzle windows equal to the number of combustion chambers, characterized in that the casing of a twin-shaft gas turbine engine is made of two parts, in its first half there is an input device, a shaft a compressor, a gas turbine engine with combustion chambers, a disk with entry and exit windows in front of the turbine, alternating between the blind part and its blades, there is a guide apparatus behind them, then in the other part of the housing there is a second shaft with a traction turbine, and behind it lies a collection of waste combustion products with exhaust pipes.
RU2015143945A 2015-10-13 2015-10-13 TWO-GAS TURBINE ENGINE RU2015143945A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015143945A RU2015143945A (en) 2015-10-13 2015-10-13 TWO-GAS TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015143945A RU2015143945A (en) 2015-10-13 2015-10-13 TWO-GAS TURBINE ENGINE

Publications (1)

Publication Number Publication Date
RU2015143945A true RU2015143945A (en) 2017-04-19

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ID=58641846

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015143945A RU2015143945A (en) 2015-10-13 2015-10-13 TWO-GAS TURBINE ENGINE

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RU (1) RU2015143945A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2685170C1 (en) * 2018-05-17 2019-04-16 Виктор Серафимович Бахирев Two-wheel gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2685170C1 (en) * 2018-05-17 2019-04-16 Виктор Серафимович Бахирев Two-wheel gas turbine engine

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Legal Events

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

Effective date: 20170803