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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.

Patent No.:

US 11059575 B1

PDFFull Text
Date of Patent:
Jul. 13, 2021

Filed:

Apr. 09, 2019

Control system for a stopped rotor aircraft

Applicant:

Kitty Hawk Corporation, Mountain View, CA (US);

Inventors:

Gregory Mainland Horn, Mountain View, CA (US);

Damon Vander Lind, East Palo Alto, CA (US);

Assignee:

Kitty Hawk Corporation, Palo Alto, CA (US);

Attorney:

Van Pelt, Yi & James LLP

Primary Examiner:

Richard G Davis

Int. Cl.
CPC ...
B64C 27/24 (2006.01); G05B 11/42 (2006.01); B64C 27/26 (2006.01); B64C 29/00 (2006.01); B64C 27/82 (2006.01); B64C 27/30 (2006.01); B64C 27/615 (2006.01); B64C 27/467 (2006.01); B64C 27/14 (2006.01);
U.S. Cl.
CPC ...
B64C 27/24 (2013.01); B64C 27/14 (2013.01); B64C 27/26 (2013.01); B64C 27/30 (2013.01); B64C 27/467 (2013.01); B64C 27/615 (2013.01); B64C 27/82 (2013.01); B64C 29/0025 (2013.01); G05B 11/42 (2013.01); B64C 2027/8236 (2013.01);
Abstract

While an aircraft is mid-flight, a braking start point associated with a stoppable rotor is calculated where the stoppable rotor includes a first and second blade and the stoppable rotor is configured to rotate about a substantially vertical axis. A process to stop the stoppable rotor is started, while the aircraft is mid-flight, when the stoppable rotor reaches the braking start point, where the stoppable rotor is stopped with the first blade pointing forward and the second blade pointing backward.

Find Patent Forward Citations

Horn, Gregory. (2021). Control system for a stopped rotor aircraft (U.S. Patent No. 11059575). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11059575

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

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