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 6620-01-043-1816
NSN 5975-01-317-4372
NSN 5990-00-506-8315
NSN 6130-01-069-9187
NSN 6650-00-826-7396
NSN 5935-00-650-3237
NSN 6650-00-924-3340
NSN 5895-01-004-9847
NSN 4140-00-409-6785
NSN 5965-00-969-5795
NSN 6105-00-253-1654
NSN 5920-01-330-5224