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:
Nov. 12, 2019

Filed:

May. 17, 2017
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Ilja Waigl, Hamburg, DE;

Matias Mail, Hamburg, DE;

Thorsten Knijnenburg, Hamburg, DE;

Assignee:

AIRBUS OPERATIONS GMBH, Hamburg, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 45/00 (2006.01); B64C 25/00 (2006.01); B64C 25/34 (2006.01); B64D 13/02 (2006.01); G01L 13/00 (2006.01); G01L 19/00 (2006.01); B64D 13/04 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B64C 25/001 (2013.01); B64C 25/34 (2013.01); B64D 13/02 (2013.01); B64D 13/04 (2013.01); G01L 13/00 (2013.01); G01L 19/0007 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A differential pressure sensor system for use in an aircraft comprises a differential pressure sensor for determining a differential pressure between a pressurizable aircraft cabin and an aircraft environment, the differential pressure sensor having a first port connectable to the pressurizable aircraft cabin via a first line and a second port connectable to the aircraft environment via a second line. A shut-off device of the differential pressure sensor system is arranged in the second line which is switchable between an open position in which it opens the second line, such that a pressure prevailing in the aircraft environment acts on the second port of the differential pressure sensor, and a shut-off position in which it closes the second line, such that the second port of the differential pressure sensor is shut off from the pressure prevailing in the aircraft environment.


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