RU2001133953A - The device for ventilation of the drive compartment of the gas turbine engine of the gas pumping unit of the main gas pipeline - Google Patents

The device for ventilation of the drive compartment of the gas turbine engine of the gas pumping unit of the main gas pipeline

Info

Publication number
RU2001133953A
RU2001133953A RU2001133953/06A RU2001133953A RU2001133953A RU 2001133953 A RU2001133953 A RU 2001133953A RU 2001133953/06 A RU2001133953/06 A RU 2001133953/06A RU 2001133953 A RU2001133953 A RU 2001133953A RU 2001133953 A RU2001133953 A RU 2001133953A
Authority
RU
Russia
Prior art keywords
turbine engine
gas turbine
gas
compartment
pumping unit
Prior art date
Application number
RU2001133953/06A
Other languages
Russian (ru)
Other versions
RU2246017C2 (en
Inventor
Борис Сергеевич Окромешко
Анатолий Алексеевич Сандимиров
Original Assignee
ЗАО "Эверест-Турбосервис"
Filing date
Publication date
Application filed by ЗАО "Эверест-Турбосервис" filed Critical ЗАО "Эверест-Турбосервис"
Priority to RU2001133953/06A priority Critical patent/RU2246017C2/en
Priority claimed from RU2001133953/06A external-priority patent/RU2246017C2/en
Publication of RU2001133953A publication Critical patent/RU2001133953A/en
Application granted granted Critical
Publication of RU2246017C2 publication Critical patent/RU2246017C2/en

Links

Claims (1)

Устройство вентиляции отсека приводного газотурбинного двигателя газоперекачивающего агрегата магистрального газопровода, содержащее отсек с центробежным вытяжным вентилятором воздуха, приводной газотурбинный двигатель с внутренней и внешней оболочками, образующими канал с горячим воздухом, технологические люки по диаметру внешней оболочки и компрессор высокого давления, отличающееся тем, что, с целью снижения температуры в отсеке приводного газотурбинного двигателя, приводной газотурбинный двигатель дополнительно снабжен воздуховодом для отвода горячего воздуха непосредственно в атмосферу через один из его открытых технологических люков, используя при этом в качестве эжектора активный воздух, нагнетаемый в воздуховод по отдельной трубе из компрессора высокого давления.A ventilation device for a compartment of a driving gas turbine engine of a gas pumping unit of a main gas pipeline, comprising a compartment with a centrifugal exhaust fan of air, a driving gas turbine engine with inner and outer shells forming a channel with hot air, technological hatches by the diameter of the outer shell and a high pressure compressor, characterized in that, in order to reduce the temperature in the compartment of the driving gas turbine engine, the driving gas turbine engine is additionally provided with air channeling systems for discharging hot air directly into the atmosphere via one of its access doors open, using as an active ejector air injected into a duct through a separate pipe from the high pressure compressor.
RU2001133953/06A 2001-12-13 2001-12-13 Ventilation device of compartment of drive gas-turbine engine of gas main line gas-transfer set RU2246017C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001133953/06A RU2246017C2 (en) 2001-12-13 2001-12-13 Ventilation device of compartment of drive gas-turbine engine of gas main line gas-transfer set

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001133953/06A RU2246017C2 (en) 2001-12-13 2001-12-13 Ventilation device of compartment of drive gas-turbine engine of gas main line gas-transfer set

Publications (2)

Publication Number Publication Date
RU2001133953A true RU2001133953A (en) 2003-09-10
RU2246017C2 RU2246017C2 (en) 2005-02-10

Family

ID=35209015

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001133953/06A RU2246017C2 (en) 2001-12-13 2001-12-13 Ventilation device of compartment of drive gas-turbine engine of gas main line gas-transfer set

Country Status (1)

Country Link
RU (1) RU2246017C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU182721U1 (en) * 2017-12-25 2018-08-29 Акционерное общество "ОДК-Газовые Турбины" GAS-TURBINE ENGINE AIR COOLING SYSTEM

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