RU92014115A - GAS TURBINE INSTALLATION - Google Patents

GAS TURBINE INSTALLATION

Info

Publication number
RU92014115A
RU92014115A RU92014115/06A RU92014115A RU92014115A RU 92014115 A RU92014115 A RU 92014115A RU 92014115/06 A RU92014115/06 A RU 92014115/06A RU 92014115 A RU92014115 A RU 92014115A RU 92014115 A RU92014115 A RU 92014115A
Authority
RU
Russia
Prior art keywords
gas turbine
turbomachine
compressor
blades
installation
Prior art date
Application number
RU92014115/06A
Other languages
Russian (ru)
Other versions
RU2044145C1 (en
Inventor
Л.К. Хохлов
М.А. Пикин
А.Л. Хохлов
Original Assignee
Л.К. Хохлов
М.А. Пикин
А.Л. Хохлов
Filing date
Publication date
Application filed by Л.К. Хохлов, М.А. Пикин, А.Л. Хохлов filed Critical Л.К. Хохлов
Priority to RU92014115A priority Critical patent/RU2044145C1/en
Priority claimed from RU92014115A external-priority patent/RU2044145C1/en
Publication of RU92014115A publication Critical patent/RU92014115A/en
Application granted granted Critical
Publication of RU2044145C1 publication Critical patent/RU2044145C1/en

Links

Claims (1)

Газотурбинная установка используется в газотурбостроении. Сущность изобретения: газотурбинная установка снабжена конденсатором воды из выхлопных газов, насосом, системой очистки, воздуховодами, соединяющими соответствующие по давлению ступени компрессора с сопловыми лопатками турбомашины; полые рабочие лопатки турбомашины снабжены отверстиями, сообщающимися с межлопаточными пространствами компрессора, полый вал, в рабочих лопатках турбомашины расположены системы охлаждения, подключенные с помощью полого вала к рабочим лопаткам компрессора, а полость вала сообщается с конденсатором воды. Установка дополнительно оборудована системой подготовки, газификации твердого топлива и золоудаления.Gas turbine installation is used in gas turbine construction. The essence of the invention: the gas turbine plant is equipped with a water condenser from the exhaust gases, a pump, a cleaning system, air ducts connecting the pressure stages of the compressor with the nozzle vanes of the turbomachine; the hollow blades of the turbomachine are provided with holes communicating with the interscapular spaces of the compressor, the hollow shaft, in the blades of the turbomachine are cooling systems connected via the hollow shaft to the blades of the compressor, and the shaft cavity communicates with the water condenser. The installation is additionally equipped with a system for preparation, gasification of solid fuel and ash removal.
RU92014115A 1992-12-23 1992-12-23 Gas-turbine plant RU2044145C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU92014115A RU2044145C1 (en) 1992-12-23 1992-12-23 Gas-turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU92014115A RU2044145C1 (en) 1992-12-23 1992-12-23 Gas-turbine plant

Publications (2)

Publication Number Publication Date
RU92014115A true RU92014115A (en) 1995-08-20
RU2044145C1 RU2044145C1 (en) 1995-09-20

Family

ID=20134148

Family Applications (1)

Application Number Title Priority Date Filing Date
RU92014115A RU2044145C1 (en) 1992-12-23 1992-12-23 Gas-turbine plant

Country Status (1)

Country Link
RU (1) RU2044145C1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2474718C2 (en) * 2011-01-25 2013-02-10 Николай Евгеньевич Староверов Method of turbojet afterburning and engine to this end (versions)
RU2474708C1 (en) * 2011-07-29 2013-02-10 Михаил Аркадьевич Верткин Gas turbine engine with two combustion chambers
RU2473817C1 (en) * 2011-08-02 2013-01-27 Михаил Аркадьевич Верткин Steam and gas plant with combustion chambers of two pressures
US9376931B2 (en) * 2012-01-27 2016-06-28 General Electric Company Turbomachine passage cleaning system
RU2545113C2 (en) * 2013-04-24 2015-03-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного мотростроения им. П.И. Баранова" Solid fuel gas-turbine plant
RU2568031C2 (en) * 2014-01-17 2015-11-10 Николай Евгеньевич Староверов Turbojet afterburning process 2

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