UA87670C2 - Gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow - Google Patents

Gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow

Info

Publication number
UA87670C2
UA87670C2 UAA200606266A UAA200606266A UA87670C2 UA 87670 C2 UA87670 C2 UA 87670C2 UA A200606266 A UAA200606266 A UA A200606266A UA A200606266 A UAA200606266 A UA A200606266A UA 87670 C2 UA87670 C2 UA 87670C2
Authority
UA
Ukraine
Prior art keywords
turbine
power
high pressure
shaft
gas
Prior art date
Application number
UAA200606266A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Сергей Константинович Чернов
Владимир Евгеньевич Спицын
Валентин Никитович Лысенко
Original Assignee
Государственное Предприятие "Научно-Производственный Комплекс Газотурбостроения "Заря"- "Машпроект"
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 Государственное Предприятие "Научно-Производственный Комплекс Газотурбостроения "Заря"- "Машпроект" filed Critical Государственное Предприятие "Научно-Производственный Комплекс Газотурбостроения "Заря"- "Машпроект"
Priority to UAA200606266A priority Critical patent/UA87670C2/en
Publication of UA87670C2 publication Critical patent/UA87670C2/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

A gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow has a front body, low pressure circuit, this consists of low pressure compressor and low pressure turbine rotors of which are installed on bearings placed in bodies, intermediate body, high pressure circuit that consists of high pressure compressor and high pressure turbine, rotors of those are installed on bearings placed in the bodies, combustion chamber and power turbine. According to the invention in the front body on the power takeoff shaft roller bearing is installed, disc elestic clutch and two control rings placed at the ends of the inner ring of roller bearing, combustion chamber is arranged as counter-flow one, and between rotors of compressor and high pressure turbine body of back bearing of high pressure compressor is installed.
UAA200606266A 2006-06-05 2006-06-05 Gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow UA87670C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAA200606266A UA87670C2 (en) 2006-06-05 2006-06-05 Gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAA200606266A UA87670C2 (en) 2006-06-05 2006-06-05 Gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow

Publications (1)

Publication Number Publication Date
UA87670C2 true UA87670C2 (en) 2009-08-10

Family

ID=50633399

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200606266A UA87670C2 (en) 2006-06-05 2006-06-05 Gas-turbine engine with shaft of power takeoff from power turbine in direction opposite to air flow

Country Status (1)

Country Link
UA (1) UA87670C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2562682C2 (en) * 2010-04-28 2015-09-10 Сименс Акциенгезелльшафт Turbine comprising system of sealing air valves

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2562682C2 (en) * 2010-04-28 2015-09-10 Сименс Акциенгезелльшафт Turbine comprising system of sealing air valves

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