Abstract: An internal gear pump or motor includes inner and outer rotors that mesh together. An internal electric motor or generator may include a stator supported by a support element that passes through bearings of the outer rotor and the inner rotor may act as a rotor of the electric motor or generator. With or without the stator, the support element may support bearings of the inner rotor. The support element may be, for example, an eccentric shaft. Fluids may be supplied via the support element, if present, for cooling, lubrication or to flush a working fluid out of portions of the pump or motor, such as bearings. Flushing may also occur via channels in the housing with or without the presence of the support element. Axial faces of one of a pair of adjacent elements, for example the inner rotor and the outer rotor, may include portions for improved axial sealing and wearing in of the other of the pair. Fluid may enter and exit chambers between the inner and outer rotors by radial ports.

Abstract: A positive displacement gear pump or gear hydraulic motor having at least a first rotor with first rotor teeth and a second rotor with second rotor teeth, the first rotor teeth meshing with the second rotor teeth. First rotor chambers are defined between first rotor teeth and second rotor chambers are defined between the second rotor teeth. As the rotors mesh, the first rotor chambers, second rotor chambers or both become enclosed or substantially enclosed to form what are referred to here as secondary chambers. Pressure variations in a secondary chamber are relieved by internal flow channels in the first rotor, second rotor or both, creating a fluid connection between the first rotor chambers and the second rotor chambers. The first rotor may be an internal gear rotor or both rotors may be external gear rotors.

Abstract: An internal gear pump or motor includes inner and outer rotors that mesh together. An internal electric motor or generator may include a stator supported by a support element that passes through bearings of the outer rotor and the inner rotor may act as a rotor of the electric motor or generator. With or without the stator, the support element may support bearings of the inner rotor. The support element may be, for example, an eccentric shaft. Fluids may be supplied via the support element, if present, for cooling, lubrication or to flush a working fluid out of portions of the pump or motor, such as bearings. Flushing may also occur via channels in the housing with or without the presence of the support element. Axial faces of one of a pair of adjacent elements, for example the inner rotor and the outer rotor, may include portions for improved axial sealing and wearing in of the other of the pair.

Abstract: A method of varying a volume of a chamber defined by a first rotor, a second rotor, and a piston in a housing of a piston machine apparatus involves: causing the first rotor to rotate around a first axis of rotation; causing the second rotor to rotate around a second axis of rotation different from the first axis of rotation; and causing the piston to slide, in response to rotation of the second rotor around the second axis of rotation, along a first linear path relative to a first coupling portion of the first rotor coupled to the piston. Causing the second rotor to rotate around the second axis of rotation involves causing a second coupling portion of the second rotor coupled to the piston to revolve around the second axis of rotation in a path around the first coupling portion. Piston machine apparatuses and uses thereof are also disclosed.

Abstract: A computing device for displaying procedures for an aircraft is provided. The computing device includes a presentation interface, a user input interface, and a processing device coupled to the presentation interface and to the user input interface. The processing device is configured to cause the presentation interface to display an initial procedure display, and in response to a triggering event, cause the presentation interface to display an adjusted procedure display that emphasizes a predetermined portion of a procedure.

Abstract: The different advantageous embodiments provide a system comprising a computer, first program code stored on the computer, and second program code stored on the computer. The computer is configured to run the first program code to retrieve flight status information during a flight and generate four dimensional flight information. The four dimensional flight information includes a comparison of the flight status information to a flight plan for the flight. The computer is configured to run the second program code to depict the four dimensional flight information in a textual format.

Abstract: A liquid-in-gas injector tube in which the diameter of the inner liquid-bearing tube within the gas-transmitting tube is reduced adjacent the outlet end of the injector. Clogging may be further reduced by adding vanes to the outer surface of the inner liquid-bearing tube within the gas-transmitting tube to impart swirling or otherwise focus the flow of gas at the exit of the injector tube.