SU282837A1 - TWO-CONTAINED GAS TURBINE INSTALLATION - Google Patents

TWO-CONTAINED GAS TURBINE INSTALLATION

Info

Publication number
SU282837A1
SU282837A1 SU1323374/06A SU1323374A SU282837A1 SU 282837 A1 SU282837 A1 SU 282837A1 SU 1323374/06 A SU1323374/06 A SU 1323374/06A SU 1323374 A SU1323374 A SU 1323374A SU 282837 A1 SU282837 A1 SU 282837A1
Authority
SU
USSR - Soviet Union
Prior art keywords
gas turbine
gas
turbine installation
contained gas
turbine
Prior art date
Application number
SU1323374/06A
Other languages
Russian (ru)
Inventor
А.П. Тунаков
Б.Х. Перельштейн
Original Assignee
Казанский ордена Трудового Красного Знамени авиационный институт
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 Казанский ордена Трудового Красного Знамени авиационный институт filed Critical Казанский ордена Трудового Красного Знамени авиационный институт
Priority to SU1323374/06A priority Critical patent/SU282837A1/en
Application granted granted Critical
Publication of SU282837A1 publication Critical patent/SU282837A1/en

Links

Landscapes

  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

Двухконтурная газотурбинная установка, содержащая во внутреннем контуре непосредственно перед выхлопным патрубком газовый компрессор, турбину для привода последнего и размещенный между ними теплообменник для охлаждения газа перед компрессором воздухом наружного контура, отличающаяся тем, что, с целью повышения экономичности и уменьшения удельного веса, во внешний контур включена дополнительная турбина для привода газового компрессора.A dual-circuit gas turbine installation, containing a gas compressor directly in front of the exhaust pipe, a turbine to drive the latter and a heat exchanger placed between them to cool the gas in front of the compressor with external circuit air, which, in order to increase efficiency and reduce specific gravity included additional turbine to drive a gas compressor.

SU1323374/06A 1969-04-21 1969-04-21 TWO-CONTAINED GAS TURBINE INSTALLATION SU282837A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1323374/06A SU282837A1 (en) 1969-04-21 1969-04-21 TWO-CONTAINED GAS TURBINE INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1323374/06A SU282837A1 (en) 1969-04-21 1969-04-21 TWO-CONTAINED GAS TURBINE INSTALLATION

Publications (1)

Publication Number Publication Date
SU282837A1 true SU282837A1 (en) 2010-06-10

Family

ID=60514370

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1323374/06A SU282837A1 (en) 1969-04-21 1969-04-21 TWO-CONTAINED GAS TURBINE INSTALLATION

Country Status (1)

Country Link
SU (1) SU282837A1 (en)

Similar Documents

Publication Publication Date Title
CA928976A (en) Gas turbine engines with compressor rotor cooling
BE752584A (en) MULTI-STAGE COMPRESSOR TURBINE ENGINE WITH BETWEEN STAGE AIR LEAK SYSTEMS
NO142969C (en) COOLING DEVICE FOR GAS TURBINES.
AU1033770A (en) Cooling of turbine rotors in gas turbine engines
ES382568A1 (en) Cooling tower system
ES408786A1 (en) Compact heat exchanger
ZA703422B (en) Gas turbine provided with rotating heat exchangers
IT1027381B (en) AIR COOLED HEAT EXCHANGER WITH POST CONDENSER
SU282837A1 (en) TWO-CONTAINED GAS TURBINE INSTALLATION
CH510242A (en) Evaporative heat exchanger
GB1366659A (en) Road vehicle powered by a thermal prime mover
JPS5348006A (en) Tuyere for blast furnace
AT307465B (en) High performance air condensation cooling tower with natural draft
ES341702A1 (en) Conditioning unit for heating, refreshing, conditioning and ventilation of environments, with heat exchanger battery and fans of high preponderance. (Machine-translation by Google Translate, not legally binding)
DD49078A1 (en) Sealing of the cooling gas duct in the blading part of gas turbines
JPS51127554A (en) Open cooler of the absorption type
SU402271A1 (en) TERMOBARCAMERA
SU400156A1 (en) Turbo cooler loading device
CA815887A (en) High efficiency regeneratively cooled gas turbine engine
SU266583A1 (en) AIRCRAFT AIRCRAFT
ES175030U (en) Environmental purifier. (Machine-translation by Google Translate, not legally binding)
JPS5378465A (en) Refrigeration device
JPS5384344A (en) Air conditioner
SU349332A1 (en) FRONT DEVICE COMBUSTION CAMERA
SU488466A1 (en) Air bleed system for turbojet compressor