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. 03, 2020

Filed:

Jan. 23, 2017
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Lazar Mitrovic, Longueuil, CA;

Eric Durocher, Vercheres, CA;

Keith Morgan, Westmount, CA;

Assignee:

Pratt & Whitney Canada Corp., Longueuil, Quebec, CA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/02 (2006.01); B64D 35/08 (2006.01); F02C 7/32 (2006.01); F02C 7/26 (2006.01); B64C 27/12 (2006.01); B64D 27/10 (2006.01); B64D 31/06 (2006.01); F02C 7/22 (2006.01); F02C 7/262 (2006.01); F02C 7/275 (2006.01); F02C 7/36 (2006.01); F16D 48/02 (2006.01);
U.S. Cl.
CPC ...
B64D 35/08 (2013.01); B64C 27/12 (2013.01); B64D 27/10 (2013.01); B64D 31/06 (2013.01); F02C 6/02 (2013.01); F02C 7/22 (2013.01); F02C 7/26 (2013.01); F02C 7/262 (2013.01); F02C 7/275 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F16D 48/02 (2013.01); F05D 2220/323 (2013.01); F05D 2220/329 (2013.01); F05D 2260/404 (2013.01); F05D 2260/4023 (2013.01); F05D 2260/85 (2013.01); F05D 2260/902 (2013.01); F05D 2260/903 (2013.01); Y02T 50/671 (2013.01); Y10T 477/753 (2015.01);
Abstract

A method of operating a twin engine helicopter power plant, the power plant comprising: two turboshaft engines each having an engine shaft with a turbine at a distal end and a one-way clutch at a proximal end; a gear box having an input driven by the one way clutch of each engine and an output driving a helicopter rotor; a bypass clutch disposed between the proximal end of each engine shaft and the input of the gear box; and power plant management system controls for activating the bypass clutch; the method comprising: detecting when a rotary speed of an associated engine shaft is less than a rotary speed of the gear box input; activating the bypass clutch to drive the associated engine shaft using the rotation of the gear box input; and starting an associated engine by injecting fuel when the bypass clutch is activated.


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