Air impingement cooling system
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Jul 19, 2001
app pub date -
Dec 28, 2000
filing date -
Jan 18, 2000
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
Where gas turbine engine structure eg combustion equipment, is to be air impingement cooled, the surface which receives the air jets is so shaped as to produce boundary layer separation zones 34, 38 and 44 in the cooling air, as it spreads across the surface. Mixing of the boundary layer with the remainder of the air flow results, followed by the reestablishment of the boundary layer. The new boundary layer is cooler than the original layer and so provides more effective cooling.
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