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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

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... 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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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. Information indicative of the one or more travel modes can be provided for display on a... Ge Aviation Systems Limited

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. The user interface can include one or more virtual elements associated with functions to be... Ge Aviation Systems Limited

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. The method can include identifying a plurality of phase reference points based, at least in part, on the... Ge Aviation Systems Limited

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. The second display device... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... Ge Aviation Systems Limited

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... 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. 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