Abstract: An attachment for the air intake of a gas turbine engine includes a plurality of particle separators. The particle separators cooperate to define an attachment axis and are spaced circumferentially about the attachment axis. Each particle separator includes a housing defining a separator axis, a first flow passage having at least a portion that is annular, an annular opening, and an annular second flow passage. The first and second flow passages are configured so that inertia of particles entrained in a stream of air flowing through the annular portion of the first flow passage tends to cause the particles to flow from the annular portion through the opening into the second flow passage to allow the stream of air to enter the engine flow passage free of the particles removed therefrom. The separator axes are parallel to and spaced apart from the attachment axis.

Abstract: A particle separator for a gas turbine engine includes a housing defining an annular first flow passage, an annular first opening, and an annular second flow passage positioned in fluid communication with the first flow passage through the first opening. The particle separator also includes a plurality of first vanes coupled to the housing in the first flow passage and a plurality of blades positioned in the first flow passage for rotation about an axis of the particle separator in response to a stream of air flowing past the blades downstream of the first vanes to allow the blades to deflect particles entrained in the stream of air from the first flow passage into the second flow passage through the first opening.

Abstract: A wave rotor apparatus and method of using the transient gas dynamic processes within the wave rotor to accomplish an engine topping cycle. In one form of the present invention the wave rotor is a five port device. Working fluid from the highest pressure outlet port is routed to a port adjacent to and preceding an inlet port admitting air from the compressor. In a preferred form of the present invention there are two port sequences disposed along the circumference of the wave rotor apparatus.

Abstract: A wave rotor apparatus and method of using the transient gas dynamic processes within the wave rotor to accomplish an engine topping cycle. In one form of the present invention the wave rotor is a five port device. Working fluid from the highest pressure outlet port is routed to a port adjacent to and preceding an inlet port admitting air from the compressor. In a preferred form of the present invention there are two port sequences disposed along the circumference of the wave rotor apparatus.

Abstract: A wave rotor apparatus and method of using the transient gas dynamic processes within the wave rotor to accomplish an engine topping cycle. In one form of the present invention the wave rotor is a five port device. Working fluid from the highest pressure outlet port is routed to a port adjacent to and preceding an inlet port admitting air from the compressor. In a preferred form of the present invention there are two port sequences disposed along the circumference of the wave rotor apparatus.