Article | REF: BM4567 V1

Gas turbine cooling. Combustion chamber

Author: Bruno FACCHINI

Publication date: July 10, 2006 | Lire en français

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    1. Heat flow in the combustion chamber

    The evaluation of heat flows on the wall of a combustion chamber can be carried out in a similar way to that of the blades (cf. ).

    Figure 1 shows the heat flows acting on the chamber wall. Those entering are due to radiation R 1 and hot gas convection C 1 , while the outer side of the wall yields heat flow to the convective cooling system C 2 , by radiation R 2 towards the envelope due to the large surfaces involved and the low value of the outer wall temperatures. Heat exchange between the two faces of the wall K 1 – 2 ...

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