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 5905-01-373-9885
NSN 6320-01-585-8468
NSN 5905-00-050-1458
NSN 6145-00-419-0550
NSN 5975-00-102-2778
NSN 6110-01-536-8454
NSN 5990-01-227-6526
NSN 6645-00-634-9317
NSN 5975-01-433-9999
NSN 5910-01-302-4846
NSN 6320-01-564-0893
NSN 2925-00-284-1534