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. 22, 2023

Filed:

Aug. 21, 2020
Applicant:

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

Inventors:

Saravanakumar Gurusamy, Bangalore, IN;

Kantha Chikkegowda, Bangalore, IN;

Ivan Wyatt, Scottsdale, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/06 (2006.01); G08G 5/00 (2006.01); G01C 23/00 (2006.01); G05D 1/10 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0661 (2013.01); B64D 31/06 (2013.01); G01C 23/00 (2013.01); G05D 1/106 (2019.05); G08G 5/0065 (2013.01);
Abstract

Methods and systems for generating a vertical situation display for a noise abatement departure procedure (NADP). Other NADP relevant displays are also disclosed including display of NADP parameters on altitude tape and primary flight displays, an NADP bug on an engine display and NADP status annunciations. The methods and systems include receiving NADP parameters entered into a flight management system (FMS) on a user interface of the aircraft system. The NADP parameters include: an initial altitude at which take-off thrust should be reduced to NADP thrust, an acceleration altitude at which the aircraft should begin accelerating to a final take-off speed whilst maintaining the NADP thrust, a climb excitement altitude at which a speed target is changed to the final take-off speed whilst maintaining the NADP thrust, and an end altitude at which the NADP should be exited. The methods and systems include generating a vertical situation display for a display device of the aircraft system indicating the NADP parameters on a flight path indication.


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