IMPROVING THE DESIGN OF THE SEAL GAPS IN THE FLOW OF THE PUMPING UNIT GTK-10-4.
Abstract and keywords
Abstract (English):
Describes the methods of modernization seal the radial clearance of the gas turbine by using the honeycomb structure at the periphery of the wheel. Discusses the gas-dynamic and thermal engineering problems using honeycomb seals in turbomachinery.

Keywords:
honeycomb seal, hydraulic resistance, heat transfer, cooling air.
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References

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