The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 22, 2021

Filed:

Dec. 24, 2018
Applicant:

Panasonic Avionics Corporation, Lake Forest, CA (US);

Inventors:

Philip Watson, Lake Forest, CA (US);

Steven Bates, Mission Viejo, CA (US);

Samuel Jester, Lake Forest, CA (US);

Grant Edward Burrows, Irvine, CA (US);

Assignee:

PANASONIC AVIONICS CORPORATION, Lake Forest, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H04L 12/26 (2006.01); H04L 29/08 (2006.01); B64D 11/00 (2006.01); G07C 5/00 (2006.01); H04L 29/06 (2006.01);
U.S. Cl.
CPC ...
H04L 43/028 (2013.01); B64D 11/0015 (2013.01); G07C 5/008 (2013.01); H04L 63/0263 (2013.01); H04L 67/025 (2013.01); H04L 67/12 (2013.01);
Abstract

An in-flight entertainment and communications (IFEC) system configured to stream vehicle operational parameters from avionics systems connected thereto. An avionics interface defines a node of an avionics bus, and the avionics systems are connectible to the avionics interface over the avionics bus to transmit aircraft operational parameters thereto as a raw stream of chronologically sequenced data elements. A data processor is connected to the avionics interface and a network interface, and is receptive to the aircraft operational parameters from the avionics interface. The data processor applies a variable filter that selectively passes a filtered data stream of aircraft operational parameters derived from the raw stream to a data storage device. The variable filter is defined by one or more filter parameters dynamically adjustable in response to changing conditions derived from the aircraft operational parameters. The filtered data stream is transmitted to the remote monitoring station.


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