| 1. A gas turbine variable geometry combustor, comprising: a combustor liner defining a plurality of dilution ports for providing
air to a dilution zone of the gas turbine combustor; and
a plurality of valves, each valve being positioned adjacent a respective one of the dilution ports for controlling the flow
of air through the dilution ports, each valve being settable to maintain one of a plurality of different open configurations,
each valve being arranged for reciprocating movement and said combustor further comprising control means for variably controlling
the setting of the valves wherein the control means comprises a rotatable actuating ring, the actuating ring has a plurality
of camming surfaces and each valve has a cam follower arranged to rest on a respective one of the plurality of camming surfaces.
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