Abstract: In the embodiment shown, the device comprises a pair of turbine wheels, rotatively journaled, each having a peripheral, concave channel. The wheels are journaled to close onto each other, in close proximity, to define of their channels a circular aperture. A conduit is directed to impel rounds of shot into the aperture, so that rotary torque power will be derived from the turbine wheels. A supply of pressured steam accelerates the rounds through the conduit to the aperture, and a feed wheel singly and successively introduces the shot into the conduit. A drive belt fixed around a hub on the feed wheel and a hub on one of the turbine wheels imparts rotation to the feed wheel, and the spent-missile end of the conduit opens onto the feed wheel to cause the latter to store and advance shot.

Abstract: In the embodiments shown, the device comprises a turbine wheel, rotatively journaled, having a peripheral, grooved surface onto which rounds of shot are impelled, under steam pressure, to rotate the wheel so that torque power might be derived therefrom. The turbine wheel, in turn, rotates a pulley -- by means of a drive belt -- which operates a sluice-type gating device. The latter device cyclically opens and closes off the pressured steam supply, and feeds a missile -- a round of shot -- to a conduit which terminates in adjacency to the turbine wheel, in order that the round, the missile, will be impelled through the conduit to impact upon the grooved surface of the turbine wheel and deliver a frictional, glancing, energy-transferring blow to the turbine wheel. The turbine wheel is rotatively carried on a support which is pivotally mounted, so that the turbine wheel can be moved into and out of proximity with the missile-impelling conduit in order to optimize missile impact.