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:
Nov. 26, 2019

Filed:

Sep. 23, 2016
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventor:

Mark R. Alber, Milford, CT (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 3/38 (2006.01); B64C 5/02 (2006.01); B64C 39/04 (2006.01); B64D 35/08 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 3/385 (2013.01); B64C 5/02 (2013.01); B64C 39/04 (2013.01); B64D 35/08 (2013.01);
Abstract

A tiltwing aircraft includes a fuselage, an engine mounted stationary relative to the fuselage, and an opposed pair of wings. The wings are separated from each other with the fuselage therebetween, each wing independently mounted to the fuselage by a respective pivot system for rotation relative to the fuselage. An opposed pair of rotor assemblies is included, each operatively connected to a respective one of the wings for common rotation with the respective wing back and forth between a first position predominantly for lift to a second position predominantly for thrust.


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Quick Actions:

Alber, Mark. (2019). Pivot systems for tiltwing aircraft (U.S. Patent No. 10486806). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10486806

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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