Gas turbine combustion chambers

Power plants – Combustion products used as motive fluid – External-combustion engine type

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Details

60 3971, 60 3974R, 60 3972R, 431 10, 431352, F02C 722

Patent

active

040528448

ABSTRACT:
Combustion chamber comprising a first combustion zone opening into a wider second combustion zone into which the combustion air is admitted through a practically frontal air entry comprising obstacles which impart a coefficient of blocking of about 60% to 80% to it. The first zone is supplied with air and fuel in substantially stoichiometric proportion in idling. At the other running rates, a supplementary fuel flow is injected into the chamber and burns in the second zone in the wake of the obstacles.

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Yaffee, M. L., "NASA Seeks Clean Combustors", Aviation Wk. and Space Tech., ug. 26, 1974, pp. 56-59.

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