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 6240-00-275-1950
NSN 6240-01-242-0150
NSN 6105-00-287-0989
NSN 6220-00-230-4705
NSN 5950-00-259-3063
NSN 5920-00-702-6694
NSN 2925-01-157-9204
NSN 5999-01-235-7867
NSN 6130-01-254-3934
NSN 5915-00-107-6828
NSN 6240-01-260-8149
NSN 5835-01-087-9515