RU93020025A - GAS TURBINE INSTALLATION - Google Patents

GAS TURBINE INSTALLATION

Info

Publication number
RU93020025A
RU93020025A RU93020025/06A RU93020025A RU93020025A RU 93020025 A RU93020025 A RU 93020025A RU 93020025/06 A RU93020025/06 A RU 93020025/06A RU 93020025 A RU93020025 A RU 93020025A RU 93020025 A RU93020025 A RU 93020025A
Authority
RU
Russia
Prior art keywords
gas turbine
compressor
turbine installation
turbomachine
steam
Prior art date
Application number
RU93020025/06A
Other languages
Russian (ru)
Other versions
RU2053399C1 (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 RU93020025A priority Critical patent/RU2053399C1/en
Priority claimed from RU93020025A external-priority patent/RU2053399C1/en
Publication of RU93020025A publication Critical patent/RU93020025A/en
Application granted granted Critical
Publication of RU2053399C1 publication Critical patent/RU2053399C1/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, рабочие лопатки турбомашины выполнены полыми с отверстиями, сообщенными с межлопаточными пространствами компрессора, рабочие лопатки турбомашины имеют каналы системы охлаждения, подключенные с помощью полого вала к рабочим лопаткам компрессора, а полость вала подключена к конденсатору воды. Установка дополнительно имеет системы подготовки, газификации твердого топлива и золоудаления, пароводяной контур, включающий парогенератор, паровую турбину, конденсатор, насос питательной воды, подогреватель питательной воды.Gas turbine installation is used in gas turbine construction. The inventive gas turbine installation 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 nozzle turbomachine blades, the turbomachine vanes are hollow with holes communicated with the interscapular spaces of the compressor, the turbomachine vanes have system channels cooling, connected via a hollow shaft to the compressor blades, and the shaft cavity is connected to a water condenser. The plant additionally has systems for preparation, gasification of solid fuel and ash removal, a steam-water circuit including a steam generator, a steam turbine, a condenser, a feedwater pump, a feedwater heater.
RU93020025A 1993-04-16 1993-04-16 Gas turbine plant RU2053399C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93020025A RU2053399C1 (en) 1993-04-16 1993-04-16 Gas turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93020025A RU2053399C1 (en) 1993-04-16 1993-04-16 Gas turbine plant

Publications (2)

Publication Number Publication Date
RU93020025A true RU93020025A (en) 1995-10-27
RU2053399C1 RU2053399C1 (en) 1996-01-27

Family

ID=20140523

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93020025A RU2053399C1 (en) 1993-04-16 1993-04-16 Gas turbine plant

Country Status (1)

Country Link
RU (1) RU2053399C1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914365B1 (en) * 2007-03-28 2012-05-18 Airbus France SYSTEM FOR COOLING AND REGULATING EQUIPMENT TEMPERATURE OF A PROPELLANT AIRCRAFT ASSEMBLY.
RU2529289C1 (en) * 2013-03-12 2014-09-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Казанский государственный энергетический университет" (ФГБОУ ВПО "КГЭУ") Method to improve efficiency of axial multistage compressor operation
FR3072908B1 (en) 2017-10-26 2021-02-26 Safran Nacelles AIRCRAFT PROPULSION KIT

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