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 6620-01-554-8169
NSN 5895-00-708-2116
NSN 5985-01-634-0635
NSN 5960-01-505-2426
NSN 6110-00-363-3974
NSN 5990-01-498-0641
NSN 6135-00-097-8162
NSN 6320-00-270-8222
NSN 6645-01-163-9930
NSN 5930-01-027-1080
NSN 5945-01-575-0755
NSN 5990-00-990-8940