Abstract: The disclosure provides engines or pumps that includes a rotatable shaft defining a central axis A, the shaft having a first end and a second end. The shaft can have an elongate first island disposed thereon. The first island can have a body with a volume generally defined between front and rear surfaces that are spaced apart. The front and rear surfaces can lie in a plane parallel to a radial axis R. The perimeters of the front and rear surfaces can define a curved perimeter surface therebetween. The engine or pump can further include a front side plate disposed adjacent to the front surface of the first island, and a rear side plate disposed adjacent to the rear surface of the first island. The engine or pump also includes a first contour assembly disposed between the front side plate and the rear side plate.

Abstract: A rotary compressor or expander include a cylindrical housing chamber, a rotatable cylindrical rotor mounted eccentrically with respect to housing chamber center, a cylindrical rotor liner free to move around the rotor, and a pivoting generally circular arc vane hinged to the rotor liner. Cavity or buckets engraved to the outer surface of the rotor liner together with corresponding inlet nozzle flow provide additional momentum impulse transfer from working fluid to expander eccentric rotor. The inlet of the rotary expander is equipped with a rotating valve synchronous to the eccentric rotor, regulating the admission time and duration of the entering working fluid. The exhaust of the rotary compressor is equipped with either a check valve or a rotating valve synchronizing the fluid discharge time and duration.

Abstract: A component for a gas turbine engine having an engine axis includes a rotor disk and a plurality of airfoils. The rotor disk comprises a web and a rim. The web has a first outer surface at least partially defining a plurality of holes and a plurality of slots. Each of the plurality of slots extends from a corresponding one of the plurality of holes and forms a first angle with the engine axis at the point of intersection with the corresponding one of the plurality of holes. The rim has a second outer surface also at least partially defining the plurality of slots. Each of the plurality of slots forms a second angle with the engine axis at the second outer surface, the second angle being different from the first angle. Each of the plurality of airfoils extends from the second outer surface.

Abstract: The invention relates to a vane machine (500) for the expansion or compression of gaseous media, for example, air, exhaust gases of an internal combustion engine, vaporous media, or a mixture thereof, comprising a housing (505) with a cylindrical space and an inlet opening (510) and an outlet opening (520) into the cylindrical space, with a parallel offset or eccentrically disposed shaft (101) relative to the center axis (501) of the housing, at least one first and one second circular disc (102, 103; 401, 402) disposed on the shaft (101) offset in a parallel fashion relative to each other. The invention further comprises sliders (104 to 115) that are guided by the circular discs and can be displaced in the direction of the inner wall of the housing (505), wherein a vane is formed by two neighboring sliders (108, 109/109, 110; . . .

Abstract: A turbine fuel pump including a cylindrical casing, an electric motor accommodated in the casing, a pump housing mounted into the casing, and an impeller disposed within the pump housing and driven around an axis in a rotational direction by the electric motor. The impeller includes a plurality of vanes each formed into a generally rectangular plate including a tip end face that extends circumferentially to define an outer peripheral surface of the impeller, and front and rear faces respectively located on forward and rearward sides in the rotational direction of the impeller. The front face is curved such that a tip end portion thereof is positioned forwardly in the rotational direction of the impeller relative to a root portion thereof. A chamfer portion is disposed between the tip end face and a tip end portion of the front face.

Abstract: A pump for pumping a liquid containing solids comprises a housing having a first end and second end and an interior pump chamber. An inlet pipe leads to the pump chamber through the first end, and an outlet pipe leads from the pump chamber at the second end. A core having a vane extending therefrom rotates within the chamber. The core has hollow portions permitting material to move from the inlet pipe to the pump chamber and from the pump chamber to the outlet pipe. The vane extends from the core outwardly, seals against the housing, and works in cooperation with a pair of moving blades to draw material from the inlet pipe and expel the material through the outlet pipe. The blades, which are arcuate in shape and have curved ends, are operated by pneumatic cylinders and move from a retracted position in which they are positioned out of the pump chamber to a deployed position in which the curved end sealably engages the core.

Abstract: A rotary internal combustion engine including a plurality of variable compression ratio rotating combustion chambers or alternatively stationary combustion chambers, a multi-piston movable assembly or alternatively a multi-sector movable assembly, a multi-sector stationary assembly or alternatively multi-piston stationary assembly with means for effecting ignition or alternatively for injecting fuel into the combustion chambers. The combustion chambers are formed by the multi-sector stationary assembly and the multi-piston movable assembly such that each of the pistons is located radially of the engine's pre-definable center axis. The stationary assembly, the movable assembly and the pistons of the movable assembly are cooperatively associated one with another so that the movable assembly is capable of being made to undergo rotating motion about the engine's center axis in a circular path about the stationary assembly.

Abstract: A rotary air motor has a stator with a cylindrical inner surface defining a chamber and a cylindrical rotor mounted by hub structure for eccentric rotation within the chamber and end plates closing the opposite ends of the chamber and spaced from the adjacent ends of the rotor by end clearance spaces. The rotor has a plurality of arcuate slots therein extending the length thereof and respectively slidably receiving arcuate vanes arranged so that when the rotor is rotated the outermost edges of the vanes are centrifugally urged into sliding engagement with the inner surface of the stator.

Abstract: In a rotary engine comprising a casing defining an oval working chamber and a rotor mounted in the chamber, the rotor is mounted for simple rotation about the chamber axis and resilient sealing means are provided in the rotor to cooperate with the curved chamber wall to provide suction through an inlet port in the casing, compression and expansion, and exhaustion through an outlet port in the casing during rotation of the rotor.

Abstract: A rotary device of the type having an oblong chamber and a rotating rotor therein. Arcuate vanes are slidably mounted in the rotor so as to rotate therewith and concurrently slide relative thereto such that the ends of the vanes constantly engage the walls of the oblong chamber. The chamber walls, viewed axially in cross-section, comprise a pair of straight sides and a pair of curved ends. The curvature of these ends is derived mathematically from a square, the sides of which square form the said straight sides of the chamber walls.