公开(公告)号：US20180186469A1

公开(公告)日：2018-07-05

申请号：US15398812

申请日：2017-01-05

Applicant: Delta Air Lines, Inc.

Inventor： Michael Gregory ,  Eric Holstein ,  Michael Linzbach ,  Richard Shideler

IPC: B64D45/00 ,  G01K7/16 ,  G01L19/00 ,  B64F5/60 ,  G07C5/00

CPC classification number: B64D45/00 ,  B64D13/08 ,  B64D2013/0603 ,  B64D2013/064 ,  B64F5/60 ,  G01K1/026 ,  G01K2201/00 ,  G01L19/0092 ,  G07C5/008

Abstract: A health monitoring system of an aircraft includes a plurality of sensors and interfaces that are non-invasively installed in a system of the aircraft. Further, the health monitoring system includes a data concentrator unit that is coupled to the plurality of sensor and interfaces. The data concentrator unit receives data associated with various components of the aircraft system from the plurality of sensor and interfaces. Responsively, the data concentrator unit processes the received data to generate a single output data stream that is transmitted to a configurable data receiver unit of the aircraft. The configurable data receiver unit transmits the received single output data stream to a ground server and an on-board display to monitor and determine a health and/or performance of the aircraft system.

公开(公告)号：US10220955B2

公开(公告)日：2019-03-05

申请号：US15398812

申请日：2017-01-05

Applicant: Delta Air Lines, Inc.

Inventor： Michael Gregory ,  Eric Holstein ,  Michael Linzbach ,  Richard Shideler

IPC: B64D45/00 ,  B64D13/08 ,  B64F5/60 ,  G01K7/16 ,  G01L19/00 ,  G07C5/00 ,  B64D13/06

Abstract: A health monitoring system of an aircraft includes a plurality of sensors and interfaces that are non-invasively installed in a system of the aircraft. Further, the health monitoring system includes a data concentrator unit that is coupled to the plurality of sensor and interfaces. The data concentrator unit receives data associated with various components of the aircraft system from the plurality of sensor and interfaces. Responsively, the data concentrator unit processes the received data to generate a single output data stream that is transmitted to a configurable data receiver unit of the aircraft. The configurable data receiver unit transmits the received single output data stream to a ground server and an on-board display to monitor and determine a health and/or performance of the aircraft system.