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:
Mar. 19, 2019

Filed:

Feb. 23, 2017
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Patrick Manoukian, Saint-Laurent, CA;

Sarah Theriault, Montreal, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60R 22/00 (2006.01); E05F 15/00 (2015.01); G05D 1/00 (2006.01); G05D 3/00 (2006.01); G06F 7/00 (2006.01); G06F 17/00 (2006.01); B64D 41/00 (2006.01); F01D 17/24 (2006.01); F02C 9/00 (2006.01); B64C 1/14 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64D 41/00 (2013.01); F01D 17/24 (2013.01); B64D 2033/0213 (2013.01); F05D 2220/50 (2013.01); F05D 2270/306 (2013.01);
Abstract

There is provided a method and a system for controlling an inlet door of an auxiliary power unit provided on an aircraft. Input data indicative of whether the aircraft is on ground or airborne is received. If the aircraft is on ground, a first control signal comprising instructions to command the inlet door to a fully open position is output. If the aircraft is airborne, a second control signal comprising instructions to command the inlet door to a partially open position. When a current value of a rotational speed of the auxiliary power unit reaches a predetermined threshold indicative of an end of a start sequence of the auxiliary power unit, a third control signal comprising instructions to transition the inlet door from the partially open position to the fully open position is output.


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