Honeywell International Inc.

Shaik Shafi Ahamed

Zhenning Liu

Srinivasa Rao Dangeti

Aralakuppe Ramegowda Yogesha

Narasimha Rao Pesala

Sundeep Vanka

Sreenivasulu Reddy Vedicherla

Thappeta Peddaiah

Vedagiribabu Subramanyam

A method is provided for diagnosing an aircraft. The method includes: determining a location of a fault in the aircraft; determining a zone of the aircraft that is associated with the location of the fault; and generating an interactive three-dimensional user interface based on the zone, wherein the interactive three-dimensional user interface provides fault data of at least one of historical faults and current faults associated with the zone.

Diagnostic methods and systems for an aircraft

Hidden or overlapped peaks may occur when using SSTDR technology to determine ware faults. These hidden/overlapped peaks may cause false negative determinations (no fault) when testing a wire for faults. In one method of the present invention, the symmetrical property of the SSTDR wave envelope is used to resolve hidden/overlapped peaks. In another method of the present invention, the calibrated normalized loop back SSTDR wave envelope may be used to resolve hidden/overlapped peaks.

Methods for detecting a hidden peak in wire fault location applications&#x2014;improving the distance range resolution

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Karnataka, India

Shaik Shafi Ahamed