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 5935-01-271-1287
NSN 5835-01-576-9013
NSN 5945-00-686-6066
NSN 5920-01-474-7536
NSN 6135-01-428-6069
NSN 6620-01-344-9355
NSN 6105-01-513-9330
NSN 6105-01-278-9830
NSN 5990-01-548-5979
NSN 5945-01-643-2649
NSN 5915-01-300-6279
NSN 6320-00-925-0558