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:
May. 07, 2019

Filed:

Aug. 10, 2016
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Daniel Bryan Robertson, Fort Worth, TX (US);

Dudley Smith, Fort Worth, TX (US);

Mark Dreier, Fort Worth, TX (US);

Steve Ray Ivans, Fort Worth, TX (US);

Kirk Landon Groninga, Fort Worth, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/82 (2006.01); B64C 27/06 (2006.01); B64C 11/00 (2006.01); B64C 39/00 (2006.01); F04D 17/04 (2006.01); F04D 29/36 (2006.01);
U.S. Cl.
CPC ...
B64C 27/82 (2013.01); B64C 11/006 (2013.01); B64C 27/06 (2013.01); B64C 39/008 (2013.01); F04D 17/04 (2013.01); F04D 29/362 (2013.01); B64C 2027/8245 (2013.01); B64C 2027/8254 (2013.01); F05D 2220/90 (2013.01);
Abstract

In some embodiments, a rotorcraft includes a fuselage, a tailboom, a drive system and a variable thrust cross-flow fan system. The cross-flow fan system includes a cross-flow fan assembly that is mechanically coupled to a drive shaft and operable to rotate with the drive shaft about a longitudinal axis. The cross-flow fan assembly includes first and second driver plates having a plurality of blades rotatably mounted therebetween. The blades are disposed radially outwardly from the longitudinal axis and have a generally circular path of travel when the cross-flow fan assembly rotates about the longitudinal axis. The blades are moveable between a plurality of pitch angle configurations. A control assembly is coupled to the blades. The control assembly is operable to change the pitch angle configuration of the blades to generate variable thrust at a substantially constant rotational speed of the cross-flow fan assembly.


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