Gas turbine combustor air inlet

Details Gas turbine combustor air inlet Gas turbine combustor air inlet

F - Mech Eng,Light,Heat,Weapons

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C

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F02C 3/14 (2006.01) F23R 3/04 (2006.01)

Patent

CA 1108874

GAS TURBINE COMBUSTOR AIR INLET ABSTRACT OF THE DISCLOSURE A covered air scoop for a gas turbine combustor comprising a tubular member radially extending through the combustor shell to define an air inlet. A symmetrical cap member is disposed in spaced, overhanging relationship over the inlet. To enter the combustor, the air must flow into the cap member, thereby causing all air to enter the tube in a substantially uniform manner so that the air flow through all similarly constructed air tubes at a common axial loca- tion of the combustor is substantially equal at all times.

307937

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