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 5999-01-577-7689
NSN 5996-00-887-0595
NSN 5996-00-373-9001
NSN 5950-01-160-8176
NSN 5905-01-588-0610
NSN 5975-00-894-9639
NSN 6145-00-347-1171
NSN 5950-01-010-3887
NSN 6650-01-317-2101
NSN 5855-01-045-9728
NSN 5915-00-240-7349
NSN 6650-01-151-6450