Abstract: An aircraft propulsion system utilizes a rotary engine to drive a centrifugal fan providing a thrust vector that is generally orthogonal to an axis of rotation of the rotary engine and the fan. The aircraft propulsion system may be mounted, for example, in the wing of a fixed-wing aircraft with the rotary engine and the centrifugal fan rotating about an axis of rotation that is generally parallel to a yaw axis of the aircraft.

Abstract: An aircraft propulsion system utilizes a rotary engine to drive a centrifugal fan providing a thrust vector that is generally orthogonal to an axis of rotation of the rotary engine and the fan. The aircraft propulsion system may be mounted, for example, in the wing of a fixed-wing aircraft with the rotary engine and the centrifugal fan rotating about an axis of rotation that is generally parallel to a yaw axis of the aircraft.

Abstract: A method of applying realtime effects to at least one lighting channel (15) for a lighting fixture or luminaire (11) is disclosed. The method includes the steps of providing a common control means interface (12) which controls the different realtime effects (13/14) to be applied to the one or more lighting channels. The realtime effects include those selected from amongst the following effects: Intensity, Position, Color, Gobo (Pattern) Beam or other controllable attribute of an automated lighting fixture. The method of applying realtime effects making up the combined effect under realtime control is such that each included effects feature of all fixtures is coordinated by a corresponding effects master controller (13/145) for that effect.

Abstract: A compression-ignition internal combustion engine for aircraft generally comprises a stationary crankshaft, a crankcase adapted to rotate about the stationary crankshaft, and a plurality of cylinders radially extending from the crankcase. Each cylinder includes a piston adapted to reciprocate therein and a connecting rod drivingly coupling the piston to the crankshaft. The engine further comprises a valve assembly for operating an exhaust valve associated with each cylinder and a fuel assembly for supplying fuel to each cylinder. First and second cams mounted on the crankshaft are adapted to operate the valve assembly and fuel assembly in a timed manner as the crankcase rotates about the crankshaft. The engine also includes a propeller synchronizer for adjusting the pitch of a plurality of propellers radially extending from the rotating crankcase.

Abstract: A bow sight includes a sight assembly having a supporting block provided with a transverse bore which slidably receives a spring loaded sighting pin for movement between a sighting position and a nonsighting position. A latch is pivoted on the block for releasable engagement with the sighting pin so that when engaged the pin is held in its nonsighting position, and when disengaged the spring forces the pin to its sighting position. A plurality of such assemblies may be mounted on a base plate in vertically spaced arrangement and the base plate in turn may be mounted on a bow to provide a device for sighting targets at various ranges.