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:
Dec. 29, 2015

Filed:

May. 23, 2013
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventors:

Kevin J Conner, Kent, WA (US);

Yasuo Ishihara, Kirkland, WA (US);

Thea L. Feyereisen, Hudson, WI (US);

John Allan Morgan, Peoria, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08B 23/00 (2006.01); B64D 45/00 (2006.01); G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); G01C 23/005 (2013.01);
Abstract

A vehicle system is provided. The system includes a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude. The system further includes a display device configured to receive the display signals and operable to selectively render an image including roll angle alert symbology. The roll angle alert symbology includes a first curved arrow.


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Conner, Kevin. (2015). Aircraft systems and methods for attitude recovery (U.S. Patent No. 9221552). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9221552

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

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