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. 14, 2016

Filed:

Oct. 03, 2014
Applicant:

Abb Technology Ag, Zürich, CH;

Inventors:

Christian Messinger, Hirschberg, DE;

Pablo Rodriguez Carrion, Ilvesheim, DE;

Georg Gutermuth, Heidelberg, DE;

Jan-Christian Schäfer, Mannheim, DE;

Assignee:

ABB TECHNOLOGY AG, Zurich, CH;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05B 19/418 (2006.01); H04L 12/24 (2006.01); H04L 12/703 (2013.01); H04L 12/26 (2006.01);
U.S. Cl.
CPC ...
H04L 45/28 (2013.01); G05B 19/4185 (2013.01); G05B 19/41885 (2013.01); H04L 41/0659 (2013.01); H04L 41/147 (2013.01); H04L 41/20 (2013.01); H04L 41/22 (2013.01); H04L 43/045 (2013.01);
Abstract

A system analyzer and a method for analyzing an impact of a change in a component of a distributed control system (DCS) are disclosed. The system can collect and store data representing the DCS components and their interconnection as well as signals of the DCS components. The DCS can be graphically modeled with nodes and directed edges, wherein a node represents either a type of DCS component or a signal of a DCS components, and wherein an edge is an 'influence'-edge, or a 'contains'-edge. Information on a change of a DCS components is received, a depth first or breadth first search is performed over the “influence”-edges and “contains”-edges and determine unchanged DCS components which would be affected by a malfunction, a removal or a taking out of operation of the at least one DCS component, and information on the affected DCS components is transmitted to an operator interface.


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