An ignition distributor is arranged so that its axis is aligned with the central longitudinal axis of a camshaft. A generally cylindrical cam is attached to an end of the camshaft for driving a rotor of the ignition distributor. A flange on the cam extends transversely to the central
A combustion chamber for gas turbine engines, particularly aircraft turbojet engines, which is constituted of an outer casing, at least one flame tube inserted therein, and incorporating at least one ignition device for the produced, respectively, supplied fuel-air mixture. The ignit
