Real Time Touch



new TOP 200 Companies filing patents this week

new Companies with the Most Patent Filings (2010+)




Real Time Touch

Ge Aviation Systems Limited patents


Recent patent applications related to Ge Aviation Systems Limited. Ge Aviation Systems Limited is listed as an Agent/Assignee. Note: Ge Aviation Systems Limited may have other listings under different names/spellings. We're not affiliated with Ge Aviation Systems Limited, we're just tracking patents.

ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "G" | Ge Aviation Systems Limited-related inventors


Aircraft high current switch module

A switch module includes a first single-throw switch having a first input terminal 20 switchable to a common terminal. A second single-throw switch has a second input terminal switchable to the common terminal. ... Ge Aviation Systems Limited

Fuel cell emergency power system

A method and system (60) for generating emergency power includes a hydrogen storage system (62) configured to supply hydrogen gas, an air delivery system (64) configured to supply air at a predetermined temperature, and a fuel cell system (66) coupled with the hydrogen storage system and the air delivery system and configured to generate power at a power output from a chemical reaction involving the hydrogen gas and the air at the predetermined temperature.. . ... Ge Aviation Systems Limited

Power distribution system including a commutation device

There is provided a power distribution system for power delivery to a load. The power distribution system includes a commutation device disposed between the load and a power source. ... Ge Aviation Systems Limited

Method and apparatus for operating a power system architecture

A method and apparatus for operating a power system architecture including an electrical power storage system, a power distribution bus selectively connected with the electrical power storage device, a hydraulic pump selectively connected with the electrical power storage device and a controller module communicatively connected with the electrical power storage system and the hydraulic pump.. . ... Ge Aviation Systems Limited

A passive leakage management circuit for a switch leakage current

A passive leakage management circuit (401) for a switch leakage current includes a switch (44) having operable in a first operating mode, wherein the switch output supplies an output current having a first predetermined voltage, and a second operating mode, wherein the switch output supplies a leakage current having a second voltage, a first current path, and a leakage current path.. . ... Ge Aviation Systems Limited

System and method for protecting a solid-state power controller

An electrical power distribution system can distribute electricity from a source to a load, and can comprise at least one solid state power controller (sspc) having an input coupled to the source and an output coupled to the load. The sspc can include an open shunt switch connecting the input to ground. ... Ge Aviation Systems Limited

Auxiliary power unit with solid oxide fuel cell for an aircraft

An auxiliary power unit and a method for providing electricity to an aircraft with the auxiliary power unit where the auxiliary power unit includes a turbine with a compressor and an output shaft. A combustor coupled to the turbine and to a fuel source, and a solid oxide fuel cell coupled to the combustor, the compressor and to the fuel source.. ... Ge Aviation Systems Limited

Power system for more electric aircraft

Systems and methods for providing power to one or more loads on an aircraft are provided. A power system for an aircraft can include a first fuel cell configured to provide base power to one or more loads on the aircraft. ... Ge Aviation Systems Limited

System and method for power distribution

A system for aircraft power distribution (100) includes a source of energy (112) to deliver an input power; a bus contactor (122); a set of switches (130) connected between the bus contactor and a set of essential and non-essential devices (132); a current analysis component (315) to determine a power level drawn from the source of current by the set of essential and non-essential devices (132); a variation reduction component (317) to determine an energization schedule of the set of essential and non-essential devices (132) based on reducing temporal variation in the input power drawn from the source of energy (112) to the bus contactor (122); and a switch control component (319) configured to adjust the set of switches (130) according to the energization schedule. If too much power is drawn, the set of switches (130) will be configured such as not to exceed the maximum power rating of the source (112).. ... Ge Aviation Systems Limited

Taxi vehicle for moving an aircraft

In one aspect, there is disclosed a taxi vehicle comprising a chassis having a coupler to connect to a coupling location of a craft and a set of wheels with at least one electric motor coupled to the set of wheels. The taxi vehicle can include a fuel cell coupled to the at least one electric motor and a battery coupled to the fuel cell. ... Ge Aviation Systems Limited

Systems, methods, and devices for bipolar high voltage direct current ground fault detection

Systems, methods, and devices for aircraft power distribution include a bipolar high voltage direct current source component; an electrical loading component capable of drawing electrical power from the bipolar high voltage direct current source component; a set of switching components configured to selectively couple power from the bipolar high voltage dc source component to the electrical loading and a ground fault interruption component coupled to the set of switching components. The ground fault interruption component is configured to detect a ground fault based on a sensed difference between a current flowing out of the set of switching components and back from the electrical loading component.. ... Ge Aviation Systems Limited

Power source for an aircraft

A power source for an aircraft including a solid oxide fuel cell and a solid oxide fuel cell along with a solid oxide fuel cell multi-power source. At least one battery is electrically coupled to the solid oxide fuel cell, the solid oxide fuel cell, and an aircraft distribution network to supply electricity to the aircraft and also for becoming recharged by the solid oxide fuel cell and the solid oxide fuel cell.. ... Ge Aviation Systems Limited

Power distribution rack assembly

An apparatus for distributing power from a power source to a set of power outputs using a power distribution rack includes a manifold having a set of bus bar channels in a wall, a set of electronic cards, and a set of bus bars received in the set of bus bar channels and coupling a power source to the electronic cards, wherein the electronic cards route the power from the power source to the power outputs.. . ... Ge Aviation Systems Limited

Display of intensity profile discs

According to an example, coordinates in a coordinate space of a display device at which a line is to be displayed may be determined. A first set of intensity profile discs corresponding to the determined coordinates and a second set of intensity profile discs having inverted intensity profiles from the first set of intensity profile discs may be identified. ... Ge Aviation Systems Limited

01/11/18 / #20180011481

Prognostic rules for predicting a part failure

A device may receive equipment information, associated with a first equipment, including information associated with anomalies identified based on operational information collected during operation of the first equipment, and messages generated during the operation of the first equipment. The device may receive maintenance information, associated with the first equipment, that identifies one or more part failures associated with one or more equipment parts. ... Ge Aviation Systems Limited

12/28/17 / #20170372723

Natural travel mode description system

Systems and methods for providing natural language annunciations are provided. In one embodiment, a method can include receiving a set of data indicative of a user input associated with one or more travel modes. ... Ge Aviation Systems Limited

12/21/17 / #20170364207

Correction of vibration-induced error for touch screen display in an aircraft

Systems and methods for correcting a vibration-induced error on a touch screen display device on an aircraft are provided. A method can include providing a user interface for display on a touch screen display device. ... Ge Aviation Systems Limited

11/30/17 / #20170341773

Aircraft component monitoring system

Systems and methods for determining aircraft component phase position are provided. In one embodiment, a method can include receiving a set of data from a data acquisition system associated with a component. ... Ge Aviation Systems Limited

11/23/17 / #20170337030

Displaying data by a display system

Systems and methods of displaying data are provided. For instance, a display system associated with a vehicle can include a first display implemented within a display housing, a transparent cover disposed over the first display device, and a second display device implemented within the display housing. ... Ge Aviation Systems Limited

08/17/17 / #20170234921

Locating electrical faults in a circuit

The present embodiments are directed to locating electrical faults in an electrical circuit, in particular electrical faults in transmission wires of an electrical circuit. Examples of the present embodiments provide a method and apparatus for opening a switch in the electrical circuit to cause an open circuit or discontinuity at the fault; transmitting a signal to be reflected from the open circuit or discontinuity and receiving the signal reflected from the open circuit or discontinuity to determine the location of the fault. ... Ge Aviation Systems Limited

08/10/17 / #20170230043

A passive leakage management circuit for a switch leakage current

A passive leakage management circuit for a switch leakage current includes a switch being operable in a first operating mode, wherein the switch output supplies an output current having a first predetermined voltage. In a second operating mode, the switch output supplies a leakage current having a second voltage, a first current path, and a leakage current path.. ... Ge Aviation Systems Limited

08/03/17 / #20170217565

Propeller blades having icephobic coating

A propeller blade for rotation about a hub assembly is provided, wherein the propeller blade defines a radial direction along its length from a blade root to a blade tip, the propeller blade including a radially inner region, a radially outer region located between the blade root and the blade tip at a position where rotational forces on the blade are sufficient, in use, to remove ice from an uncoated blade, a coating disposed at least along a leading edge of the propeller blade, the coating including an icephobic material, wherein the coating extends along the propeller blade from the radially inner region to the radially outer region.. . ... Ge Aviation Systems Limited

06/15/17 / #20170170583

Distributing wiring board connections

The present embodiments relate to providing electrical connectivity to electric-powered components mounted in parallel on a wiring board. An electrical apparatus is provided in which electricity is conducted from an electrically conductive member onto first and second electrically conductive pathways, of a wiring board through the use of first and second resiliently-deformable electrically conductive connectors. ... Ge Aviation Systems Limited

06/15/17 / #20170169632

Method for detecting a bleed air system fault

A method of detecting a fault in a bleed air system of an aircraft having multiple engines is disclosed. The method includes transmitting a bleed air flow rate from multiple engines, determining a difference between the transmitted bleed air flow rates to define a difference value, and determining, by a controller, a fault condition with the bleed air system based on the difference value.. ... Ge Aviation Systems Limited

06/15/17 / #20170166324

Power distribution connector

A power distribution connector is provided, which includes an electrically conductive bus bar configured to conduct electricity between a power-supplying node and an opposing power-consuming node, and has a set of surfaces between the opposing nodes and a thermally conductive polymer having a first surface abutting at least a portion of a subset of the bus bar surfaces and a second surface spaced from the first surface.. . ... Ge Aviation Systems Limited

06/08/17 / #20170161963

Method of identifying anomalies

A method of identifying anomalies in a monitored system includes acquiring input data from a plurality of sensors in the monitored system. Preprocessing the acquired data to prepare it for modeling leaves a first data subset that feeds into a normal gaussian mixture model built using normal operating conditions of the monitored system. ... Ge Aviation Systems Limited

02/23/17 / #20170054438

Systems, methods, and devices for bipolar high voltage direct current electrical power distribution

Systems, methods and devices for aircraft power distribution include a bipolar high voltage direct current source component; an electrical loading component capable of drawing electrical power from the bipolar high voltage direct current source component; a set of switching components configured to selectively couple power from the bipolar high voltage dc source component to the electrical loading; and a transient suppression component. The transient suppression component is configured to limit current flowing through the first or the second subset of the set of switching components when the first and the second subsets are not in the same state.. ... Ge Aviation Systems Limited








ARCHIVE: New 2018 2017 2016 2015 2014 2013 2012 2011 2010 2009



###

This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. Freshpatents.com is not affiliated or associated with Ge Aviation Systems Limited in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for Ge Aviation Systems Limited with additional patents listed. Browse our Agent directory for other possible listings. Page by FreshPatents.com

###