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:
Aug. 16, 2016

Filed:

May. 11, 2015
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Nicolas Certain, Aix en Provence, FR;

Olivier Delecroix, Eguilles, FR;

Assignee:

Airbus Helicopters, Marignane Cedex, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 43/02 (2006.01); G01P 5/26 (2006.01); G01P 5/00 (2006.01); G01P 13/02 (2006.01);
U.S. Cl.
CPC ...
B64D 43/02 (2013.01); G01P 5/00 (2013.01); G01P 5/26 (2013.01); G01P 13/025 (2013.01);
Abstract

A method of calculating and displaying the true airspeed of a rotorcraft. At least one omnidirectional airspeed sensor is installed at the top of a tail fin of the rotorcraft. The true airspeed of the rotorcraft flying at speeds that are lower than or equal to at least one airspeed threshold of the rotorcraft is calculated by correcting the measurements supplied by the airspeed sensor installed at the top of the tail fin as a function of the effects produced by the air stream generated by rotation of the main rotor of the rotorcraft on the characteristics of the speed of the air stream measured by the tail fin airspeed sensor. For this purpose, a correction rule calibrated in test flight is advantageously applied to correct the measurements supplied by the airspeed sensor installed at the top of the tail fin.


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