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. 04, 2018

Filed:

May. 30, 2017
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

James M. McCollough, Arlington, TX (US);

Erik Oltheten, Azle, TX (US);

Nicholas Lappos, Southlake, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08B 21/00 (2006.01); G01C 23/00 (2006.01); B64D 45/00 (2006.01); B64C 27/04 (2006.01); B60C 1/00 (2006.01); B64D 43/00 (2006.01); G01D 7/02 (2006.01); B64C 27/00 (2006.01); B64C 27/52 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2006.01); G01C 21/00 (2006.01); G05D 17/02 (2006.01);
U.S. Cl.
CPC ...
G01C 23/00 (2013.01); B60C 1/00 (2013.01); B64C 27/04 (2013.01); B64D 43/00 (2013.01); B64D 45/00 (2013.01); G01D 7/02 (2013.01); B64C 27/00 (2013.01); B64C 27/006 (2013.01); B64C 27/52 (2013.01); B64C 29/00 (2013.01); B64C 39/024 (2013.01); B64C 2201/108 (2013.01); B64C 2201/121 (2013.01); G01C 21/00 (2013.01); G05D 17/02 (2013.01);
Abstract

A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.


Find Patent Forward Citations

Loading…