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:
Dec. 13, 2011

Filed:

May. 05, 2008
Applicants:

Daniel E. Mazuk, Marion, IA (US);

Peter J. Morgan, Glenelg, MD (US);

David A. Miller, Swisher, IA (US);

Nicholas H. Bloom, Cedar Rapids, IA (US);

Mark A. Kovalan, Cedar Rapids, IA (US);

Inventors:

Daniel E. Mazuk, Marion, IA (US);

Peter J. Morgan, Glenelg, MD (US);

David A. Miller, Swisher, IA (US);

Nicholas H. Bloom, Cedar Rapids, IA (US);

Mark A. Kovalan, Cedar Rapids, IA (US);

Assignee:

Rockwell Collins, Inc., Cedar Rapids, IA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
H04B 10/20 (2006.01);
U.S. Cl.
CPC ...
Abstract

The present disclosure is directed to a passive optical avionics network system and method. A passive avionics network may comprise: (a) an optical line terminal (OLT); (b) at least one optical network unit (ONU); (c) a fiber optic bus operably coupling the OLT and the ONU; and (d) an avionics module operably coupled to the ONU. An integrated modular avionics (IMA) system may comprise: (a) a line-replaceable unit (LRU), the LRU comprising: (i) a processing unit; and (ii) an optical line terminal (OLT); (b) at least one optical network unit (ONU); (c) a fiber optic bus operably coupling the LRU and the ONU; and (d) an avionics module operably coupled to the ONU. A method for avionics network communication may comprise: (a) providing avionics data; (b) transmitting the avionics data via a fiber optic network; (c) receiving the avionics data; and (d) controlling functionality of an avionics module according to the avionics data.


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