RU2003134402A - METHOD FOR STARTING A GAS TURBINE ENGINE - Google Patents

METHOD FOR STARTING A GAS TURBINE ENGINE Download PDF

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Publication number
RU2003134402A
RU2003134402A RU2003134402/06A RU2003134402A RU2003134402A RU 2003134402 A RU2003134402 A RU 2003134402A RU 2003134402/06 A RU2003134402/06 A RU 2003134402/06A RU 2003134402 A RU2003134402 A RU 2003134402A RU 2003134402 A RU2003134402 A RU 2003134402A
Authority
RU
Russia
Prior art keywords
starting
turbine engine
gas turbine
auxiliary power
gas
Prior art date
Application number
RU2003134402/06A
Other languages
Russian (ru)
Other versions
RU2260134C1 (en
Inventor
Валентин Васильевич Быстров (RU)
Валентин Васильевич Быстров
Михаил Михайлович Гойхенберг (RU)
Михаил Михайлович Гойхенберг
Юрий Александрович Канахин (RU)
Юрий Александрович Канахин
Евгений Ювенальевич Марчуков (RU)
Евгений Ювенальевич Марчуков
Original Assignee
Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") (RU)
Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн")
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 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") (RU), Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") filed Critical Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") (RU)
Priority to RU2003134402/06A priority Critical patent/RU2260134C1/en
Publication of RU2003134402A publication Critical patent/RU2003134402A/en
Application granted granted Critical
Publication of RU2260134C1 publication Critical patent/RU2260134C1/en

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Claims (2)

1. Способ запуска газотурбинного двигателя, включающий подачу рабочего тела от вспомогательной силовой установки на воздушную турбину пускового устройства и последующую раскрутку ротора двигателя пусковым устройством, отличающийся тем, что в качестве рабочего тела используют газ из камеры сгорания вспомогательной силовой установки.1. A method of starting a gas turbine engine, comprising supplying a working fluid from the auxiliary power unit to the air turbine of the starting device and subsequent spinning of the engine rotor by the starting device, characterized in that gas is used as the working medium from the combustion chamber of the auxiliary power unit. 2. Способ по п.1, отличающийся тем, что к газу из камеры сгорания вспомогательной силовой установки перед подачей его на воздушную турбину пускового устройства подмешивают воздух от компрессора вспомогательной силовой установки.2. The method according to claim 1, characterized in that the air from the auxiliary power compressor is mixed with gas from the combustion chamber of the auxiliary power unit before it is fed to the air turbine of the starting device.
RU2003134402/06A 2003-11-28 2003-11-28 Gas-turbine engine starting method RU2260134C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2003134402/06A RU2260134C1 (en) 2003-11-28 2003-11-28 Gas-turbine engine starting method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2003134402/06A RU2260134C1 (en) 2003-11-28 2003-11-28 Gas-turbine engine starting method

Publications (2)

Publication Number Publication Date
RU2003134402A true RU2003134402A (en) 2005-08-10
RU2260134C1 RU2260134C1 (en) 2005-09-10

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ID=35844228

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2003134402/06A RU2260134C1 (en) 2003-11-28 2003-11-28 Gas-turbine engine starting method

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RU (1) RU2260134C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2472958C2 (en) * 2011-04-05 2013-01-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Method of starting aircraft gas turbine

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Publication number Publication date
RU2260134C1 (en) 2005-09-10

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20141129