Description:

Liner features provided, combustion chamber engine section location, consists of liner assembly; cap assembly; tube; cooling skirt; spacer .

Special Features:

Consists of liner assembly; cap assembly; tube; cooling skirt; spacer and rod

Properties:

The portion of a engine, gas turbine, nonaircraft 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.