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 5945-01-569-5925
NSN 6135-01-556-7318
NSN 5910-01-176-6476
NSN 5998-01-415-3068
NSN 5925-01-315-6349
NSN 5945-01-425-1749
NSN 5855-00-911-1370
NSN 5910-00-212-5969
NSN 6645-01-307-6815
NSN 6135-01-159-9705
NSN 7035-01-282-7124
NSN 5998-00-943-8965