The portion of an engine, gas turbine, aircraft in which fuel is burned. it may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5915-00-553-3650
NSN 5920-01-546-4749
NSN 5930-00-690-4603
NSN 6150-01-634-0575
NSN 5998-00-039-5092
NSN 5975-00-841-1284
NSN 6130-00-839-1176
NSN 6110-01-288-0517
NSN 5998-00-823-8488
NSN 5945-01-190-1295
NSN 5975-00-456-0627
NSN 7035-01-585-5888