RU2001103576A - GAS DISCHARGE DEVICE FOR GAS-TURBINE INSTALLATION - Google Patents

GAS DISCHARGE DEVICE FOR GAS-TURBINE INSTALLATION

Info

Publication number
RU2001103576A
RU2001103576A RU2001103576/06A RU2001103576A RU2001103576A RU 2001103576 A RU2001103576 A RU 2001103576A RU 2001103576/06 A RU2001103576/06 A RU 2001103576/06A RU 2001103576 A RU2001103576 A RU 2001103576A RU 2001103576 A RU2001103576 A RU 2001103576A
Authority
RU
Russia
Prior art keywords
gas
discharge device
turbine installation
diffuser
gas discharge
Prior art date
Application number
RU2001103576/06A
Other languages
Russian (ru)
Other versions
RU2226610C2 (en
Inventor
Юрий Иванович Кустов
Алевтина Александровна Баянкина
Владимир Иванович Рыженков
Original Assignee
Открытое акционерное общество "Научно-производственное объединение "Искра"
Filing date
Publication date
Application filed by Открытое акционерное общество "Научно-производственное объединение "Искра" filed Critical Открытое акционерное общество "Научно-производственное объединение "Искра"
Priority to RU2001103576/06A priority Critical patent/RU2226610C2/en
Priority claimed from RU2001103576/06A external-priority patent/RU2226610C2/en
Publication of RU2001103576A publication Critical patent/RU2001103576A/en
Application granted granted Critical
Publication of RU2226610C2 publication Critical patent/RU2226610C2/en

Links

Claims (1)

Газоотводное устройство газотурбинной установки, содержащее осерадиальный диффузор, сообщенный с выхлопной трубой, отличающееся тем, что осерадиальный диффузор выполнен с обводами, при которых проточный тракт диффузора в поперечном сечении имеет ω-образный (омегообразный) профиль, при этом он разделен перегородками, установленными эквидистатно обводам наружной стенки диффузора.A gas turbine gas vent device containing an axial radial diffuser in communication with an exhaust pipe, characterized in that the axial radial diffuser is made with bypasses, in which the diffuser flow path in cross section has an ω-shaped (omega-shaped) profile, while it is divided by partitions installed equidistically bypasses outer wall of the diffuser.
RU2001103576/06A 2001-02-07 2001-02-07 Gas-turbine plant gas outlet device RU2226610C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001103576/06A RU2226610C2 (en) 2001-02-07 2001-02-07 Gas-turbine plant gas outlet device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001103576/06A RU2226610C2 (en) 2001-02-07 2001-02-07 Gas-turbine plant gas outlet device

Publications (2)

Publication Number Publication Date
RU2001103576A true RU2001103576A (en) 2003-02-27
RU2226610C2 RU2226610C2 (en) 2004-04-10

Family

ID=32464808

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001103576/06A RU2226610C2 (en) 2001-02-07 2001-02-07 Gas-turbine plant gas outlet device

Country Status (1)

Country Link
RU (1) RU2226610C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2504665C1 (en) * 2012-05-24 2014-01-20 Открытое акционерное общество Конструкторско-производственное предприятие "Авиамотор" Exhaust device of turbomachine
RU2529560C1 (en) * 2013-03-14 2014-09-27 Открытое Акционерное Общество "Российские Железные Дороги" Suppression of effects of self-contained locomotive exhaust gases on trolley line of electrified railways and device to this end

Similar Documents

Publication Publication Date Title
RU2007116857A (en) GAS TURBINE INTERMEDIATE UNIT AND GAS-TURBINE ENGINE CONTAINING THIS ASSEMBLY
EP1865261A3 (en) Inlet flow conditioner for gas turbine engine fuel nozzle
EP1892405A3 (en) Gas turbine engine exhaust duct ventilation
DE60125441D1 (en) Multi-stage, multi-level combustion system for gas turbine
GB2430236A (en) Gas flow enhancer for combustion engines
EP1882883A3 (en) Combustor liner with reverse flow for gas turbine engine
RU2002109453A (en) REDUCED CONTROL SYSTEM FOR SIMPLIFIED CONTROL FOR TURBO-REACTIVE OR TURBO-SCREW ENGINE
WO2006026719A3 (en) Gas generating system
EP1741985A3 (en) Augmentor spray bar mounting
EP2196634A3 (en) Cavity ventilation
IT1309045B1 (en) PROCEDURE FOR CHECKING THE OPERATION OF AN EXHAUST GAS TURBOCHARGER WITH A VARIABLE GEOMETRY TURBINE.
WO2008143023A1 (en) Exhaust pipe for vehicle-mounted engine
DK1573077T3 (en) Rotary tube device for processing molten metal
EP1818521A3 (en) Muffler and vehicle equipped with muffler
KR100769700B1 (en) Apparatus for preventing flowing backward of exhaust gas
FR3099801B1 (en) Set for a turbomachine turbine
RU2001103576A (en) GAS DISCHARGE DEVICE FOR GAS-TURBINE INSTALLATION
JP2009168019A (en) Device for plugging turbine wheel hole
EP1099829A3 (en) Insert for silencer
TW200517587A (en) Scroll compressor and scroll wall arrangement therefor
RU2611544C2 (en) Turbo machine (versions)
WO2004101960A3 (en) Sound-attenuating muffler having reduced back pressure
DK1226339T3 (en) Dimmer
CN203532004U (en) Improved diesel engine silencer
KR102270835B1 (en) Gas Boiler Pipe Structure