Abstract: A method of determining the concentration of an exhaust component in a gas turbine engine includes measuring the concentration of the selected component at a single location, and using the measured concentration in a simple equation which yields a calculation of concentration in the engine exhaust. Use of this method requires that a measurement be taken for only one of multiple combustors in an engine, but the result is valid for the entire engine. Thus, the method can reduce the cost of design and development of new combustors for gas turbine engines, since it does not require that multiple combustors be built before the engine is tested. The sampling of the component of interest is done at a point sufficiently downstream that the concentration of the component has become relatively stable. The invention also includes an engine having one or more combustors modified to include a probe, and its associate analyzer, at an optimum location.

Abstract: A hollow, airfoil shaped stator vane 10 is provided in its trailing edge portion with staggered rows of pin fins 20, 22 and 24 and with longitudinal ribs 26 which provide the required stiffness for the thin wall design of the vane, the ribs being provided with protuberances 36 in those locations where the turbulence inducing pin fins are displaced by the presence of the ribs.