Improved combustor heat shield and method of cooling

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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F23R 3/42 (2006.01) F01D 25/14 (2006.01)

Patent

CA 2579084

A heat shield (80) for a gas turbine engine combustor (16) includes an apparatus (92, 94) for providing a spiral flow to improve at least the cooling of the heat shield.

Bouclier thermique (80) pour une chambre de combustion (16) de moteur à turbine de gaz comprenant un appareil (92, 94) permettant d~obtenir un flux en spirale pour améliorer au moins le refroidissement du bouclier thermique.

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