Component for a thermal machine, in particular a gas turbine
A technology for gas turbines and components, used in engine components, machines/engines, blade support components, etc., to solve problems such as increased purge air volume, loss of cooling type, and low temperature of mixed hot gas
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[0032] According to the invention, the technique of sinking cooling channels close to the surface is used for cooling corners or edges of gas turbine components (for example rotor blades, guide vanes or heat shields) which are subjected to high thermal loads. in accordance with figure 2 The problem with the configuration of is that the edge 22 is exposed to hot air from two surfaces that abut one another and is thus subjected to a very high thermal load in the corner region 24 .
[0033] according to image 3 Cooling channels 25 with a small inner diameter running parallel to the edge 22 are now provided directly below the surface in the edge region in order to cool the corner effectively and with reduced use of coolant (usually cooling air) Area 24. The inlet 30 and outlet 29 of the cooling channel 25 are in image 3 shown in dotted line.
[0034] The cooling channel 25 (with the inlet 30 ) starts from a plenum filled with cooling air, then runs parallel to the edge 22 t...
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