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 6610-01-328-3400
NSN 6220-01-436-3850
NSN 2925-01-303-5266
NSN 5950-01-562-1374
NSN 5960-00-243-5025
NSN 6145-00-764-4338
NSN 4140-01-624-1218
NSN 2925-01-359-4027
NSN 5945-01-550-8910
NSN 5990-01-632-0969
NSN 6110-01-224-6409
NSN 5998-01-335-2648