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 5985-01-513-6814
NSN 2925-01-595-4345
NSN 5996-01-525-7628
NSN 2925-00-805-6481
NSN 6220-00-361-8338
NSN 6135-01-100-3593
NSN 6130-00-146-6482
NSN 5965-01-384-1953
NSN 6220-00-900-5302
NSN 6685-00-705-6071
NSN 6650-01-542-7154
NSN 6620-01-622-4980