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:

Sep. 15, 2016
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Patrick Bowles, Glastonbury, CT (US);

ByungYoung Min, Glastonbury, CT (US);

Barbara Brenda Botros, Vernon, CT (US);

Brian E. Wake, South Glastonbury, CT (US);

Claude G. Matalanis, Longmeadow, MA (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 7/00 (2006.01); B64C 21/04 (2006.01); B64C 27/10 (2006.01); B64C 27/82 (2006.01); B64C 27/32 (2006.01);
U.S. Cl.
CPC ...
B64C 7/00 (2013.01); B64C 21/04 (2013.01); B64C 27/10 (2013.01); B64C 27/32 (2013.01); B64C 27/82 (2013.01); B64C 2027/8236 (2013.01); B64C 2027/8272 (2013.01); B64C 2027/8281 (2013.01);
Abstract

A rotary wing aircraft includes a fuselage having a plurality of surfaces, at least one engine mounted in the fuselage, and a rotor assembly including a rotor shaft and plurality of rotor blades operatively connected to the rotor shaft. The rotor assembly includes a plurality of surface portions. A rotor shaft fairing extends between the fuselage and the rotor assembly and about at least a portion of the rotor shaft. The rotor shaft fairing includes an outer surface. A plate member is mounted to and projects proudly of the at least a portion of the rotor shaft fairing. The plate member is configured and disposed to increase an aspect ratio of and reduce induced drag on the rotor shaft fairing as well as reduce rotor hub wake size.


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