Gas turbine combustion chamber with air scoops

Details Gas turbine combustion chamber with air scoops Gas turbine combustion chamber with air scoops

F - Mech Eng,Light,Heat,Weapons

23

R

60/164

F23R 3/06 (2006.01) F23R 3/04 (2006.01)

Patent

CA 1315994

-13- W.E. 54,803 Abstract A gas turbine combustion chamber with an inlet and outlet has apertures in the combustion chamber wall and air scoops provided in the apertures, the air scoops having an outer tubular member and coaxially spaced inner tubular member. The spaced tubular members have inner cylindrical portions and outwardly extending flanges, with spacers disposed between and secured to the flanges with cooling air passing therebetween and through the annular air flow passage into the combustion chamber. Preferably, a radially outwardly extending arcuate section on the inner tubular member has a radius at least about one-third of the inner diameter of the inner cylindrical portion thereof.

612174

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