Axial flow gas turbines
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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-
Dec 7, 1993
Grant Date -
N/A
app pub date -
Jan 18, 1984
filing date -
Feb 26, 1983
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
An axial flow gas turbine is provided with a shroud ring which is defined by two axially adjacent heat pipes. The radially inner face of the shroud ring has a plurality of axially extending cooling air passages located adjacent to it. Cooling air, which in operation is directed through the passages serves to provide cooling of the shroud ring and the substantial elimination of any radial heat flux in the shroud ring.
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