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:
Aug. 20, 2019

Filed:

Feb. 15, 2017
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Aric Charles Liberman, Yuma, AZ (US);

Barbara Holder, Seattle, WA (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01C 23/00 (2006.01); B64D 43/00 (2006.01); G08G 5/02 (2006.01); B64D 45/08 (2006.01); G09G 5/36 (2006.01); G09G 5/38 (2006.01); B64D 45/04 (2006.01); G08G 5/00 (2006.01);
U.S. Cl.
CPC ...
G08G 5/025 (2013.01); B64D 45/04 (2013.01); B64D 45/08 (2013.01); G01C 23/00 (2013.01); G08G 5/0021 (2013.01); G09G 5/363 (2013.01); G09G 5/38 (2013.01); G09G 2340/0464 (2013.01); G09G 2380/12 (2013.01);
Abstract

Cockpit display systems and methods are provided for generating energy management symbology on cockpit displays, which aid pilot decision-making when evaluating and executing direct approaches. In an embodiment, the cockpit display system includes a cockpit display device on which a first cockpit display, such as a vertical situation display or a horizontal navigation display, is generated. A controller is operably coupled to the cockpit display device and configured to: (i) identify a direct approach (DA) path to a configuration point located over a destination airfield; (ii) calculate a first DA energy estimate for the aircraft to fly the DA path under engine idle conditions and arrive at the configuration point with an airspeed less than a configuration airspeed; and (iii) generate symbology on the first cockpit display indicative of the first DA energy estimate.


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