F02C3/00

System and method for limiting movement of a retainer ring of a gas turbine engine
10215099 · 2019-02-26 · ·

A method of installing a retaining ring assembly in a turbine case is provided. The method may include installing a blade outer air seal into a case before installation of a retaining ring assembly. The method may further include installing a key system on a retaining ring to create the retaining ring assembly. The method may also include installing the retaining ring assembly in a case. The method may further include rotating the retaining ring assembly in the case until key system is aligned with a case slot. The method may also include tightening the key system to the retaining ring and cause key system to engage the case slot.

Multi-axial brush seal
10208674 · 2019-02-19 · ·

A seal assembly, includes a first brush supported between first and second plates, a second brush supported on the first and second plates transverse to the first brush seal, and a third plate attached to the second brush.

Multi-axial brush seal
10208674 · 2019-02-19 · ·

A seal assembly, includes a first brush supported between first and second plates, a second brush supported on the first and second plates transverse to the first brush seal, and a third plate attached to the second brush.

Communicating signal between rotating antenna and plurality of stationary antennae based on displacement

Methods and systems for communicating a signal between a rotating antenna and a plurality of stationary antennae based on an axial displacement of the rotating antenna are provided. In one example, the method can include obtaining one or more measurements of an axial displacement of the rotating antenna from one or more axial displacement sensors. The method can further include determining a selected stationary antenna from the plurality of stationary antennae based at least in part on the measurements of an axial displacement of the rotating antenna. The method can further include activating the selected stationary antenna to communicate a signal with the rotating antenna. The method can further include communicating a signal between the rotating antenna and the selected stationary antenna.

Communicating signal between rotating antenna and plurality of stationary antennae based on displacement

Methods and systems for communicating a signal between a rotating antenna and a plurality of stationary antennae based on an axial displacement of the rotating antenna are provided. In one example, the method can include obtaining one or more measurements of an axial displacement of the rotating antenna from one or more axial displacement sensors. The method can further include determining a selected stationary antenna from the plurality of stationary antennae based at least in part on the measurements of an axial displacement of the rotating antenna. The method can further include activating the selected stationary antenna to communicate a signal with the rotating antenna. The method can further include communicating a signal between the rotating antenna and the selected stationary antenna.

TURBINE ANALYSIS DEVICE, TURBINE ANALYSIS METHOD, AND PROGRAM
20180328290 · 2018-11-15 ·

A turbine analysis device according to the present application includes a state quantity acquiring unit configured to acquire a state quantity of a turbine, the state quantity including a temperature of the turbine. A load specifying unit specifies a history of a load of the turbine, based on the state quantity. A load and time calculating unit calculates a relationship between the load of the turbine and an operable time when the turbine is operated at the load, based on a designed service life of the turbine and on a history of the load that has been specified by the load specifying unit.

Dual integrated PSA for simultaneous power plant emission control and enhanced hydrocarbon recovery

Systems and methods are provided for combined cycle power generation and enhanced hydrocarbon production where emission gases during power generation are separated by adsorption and applied to facilitate extraction of hydrocarbons from a reservoir. A power generation plant passes exhaust gas to a first swing adsorption reactor. The first swing adsorption reactor adsorbs the CO.sub.2 from the exhaust gas. An adsorption cycle of the first swing adsorption reactor is variable. An injection well injects the CO.sub.2 adsorbed by the first swing adsorption reactor in a hydrocarbon reservoir. A production well that is in communication with the injection well produces a mixture of hydrocarbons and CO.sub.2. A second swing adsorption reactor purifies the produced hydrocarbons by adsorbing the produced CO.sub.2 from the production well.

Dual integrated PSA for simultaneous power plant emission control and enhanced hydrocarbon recovery

Systems and methods are provided for combined cycle power generation and enhanced hydrocarbon production where emission gases during power generation are separated by adsorption and applied to facilitate extraction of hydrocarbons from a reservoir. A power generation plant passes exhaust gas to a first swing adsorption reactor. The first swing adsorption reactor adsorbs the CO.sub.2 from the exhaust gas. An adsorption cycle of the first swing adsorption reactor is variable. An injection well injects the CO.sub.2 adsorbed by the first swing adsorption reactor in a hydrocarbon reservoir. A production well that is in communication with the injection well produces a mixture of hydrocarbons and CO.sub.2. A second swing adsorption reactor purifies the produced hydrocarbons by adsorbing the produced CO.sub.2 from the production well.

FLOW GUIDING DEVICE AND METHOD FOR FORMING A FLOW GUIDING DEVICE
20180320631 · 2018-11-08 ·

A flow guiding appliance of a turbomachine, in particular of an aircraft engine, for a partial exit flow of an outlet guide vane of a compressor, wherein, a flow guiding element delimits an annular channel about a shaft of the turbomachine. A frictional engagement connecting surface at the circumference of the flow guiding element connects the flow guiding element to another structural component of the turbomachine. The frictional engagement connecting surface with a closed enveloping surface can be inserted in a deformed state into the structural component with a circular cylindrical sealing surface with at least two opposite points. The at least two points of the closed enveloping surface are arranged in at least two opposite frictionally engaged contact areas of the circular cylindrical sealing surface following deformation. The invention also relates to a method for creating a flow guiding element.

Moisture separator and air cycle system with the same
10118116 · 2018-11-06 ·

The present invention provides a moisture separator separating condensed water mist in compressed air, and an air cycle system provided with the same. The moisture separator includes a coalescer filter and a wire mesh pad demister. The coalescer filter is provided with a filter media formed of a fiber layer through which compressed air is passed, primarily condensing moisture mist in the compressed air, and filtering foreign particles and a housing supporting the filter media. The wire mesh pad demister is provided at a downstream of the coalescer filter to receive the compressed air passed through the coalescer filter and secondarily condenses moisture mist in the compressed air to separate moisture using gravity.