FIELD: refrigerating engineering. SUBSTANCE: turbocooler has compressor 6 and turbine 7 whose blades are mounted on common disk 5 and is provided with heat exchanger 8. Disk 5 is provided with circular projection over periphery received by chamber of heat exchanger 8. EFFECT: enhanced efficiency. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
COOLING TURBINE | 1998 |
|
RU2144647C1 |
COOLING TURBINE | 2004 |
|
RU2263858C1 |
COOLED BLADE FOR A TURBINE | 0 |
|
SU565991A1 |
COOLING SYSTEM FOR INTERNAL COMBUSTION ENGINE | 0 |
|
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COOLED PERFORATED TURBINE BLADE | 2013 |
|
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COOLED PERFORATED BLADE OF TURBOMACHINE WITH HEAT BARRIER COATING | 2004 |
|
RU2286463C2 |
COOLED BLADE | 1984 |
|
SU1275957A1 |
DEVICE FOR MEASURING HEAT EXCHANGE CHARACTERISTICS IN ROTATING CHANNELS | 1988 |
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TWO-LOOP GAS-TURBINE FAN ENGINE | 2006 |
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RU2320885C2 |
ROTARY MACHINE | 1992 |
|
RU2056533C1 |
Authors
Dates
1995-05-27—Published
1992-04-23—Filed