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:
Jun. 02, 2020

Filed:

Oct. 20, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Joseph M. DiRusso, Snohomish, WA (US);

Keith D. Parsons, Renton, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/06 (2006.01); G06Q 10/06 (2012.01); B64C 13/18 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0661 (2013.01); B64C 13/18 (2013.01); B64D 31/06 (2013.01); G06Q 10/06315 (2013.01);
Abstract

An example method includes: receiving information indicative of a desired aircraft cruise insertion point comprising achieving a desired cruise altitude for an aircraft within: a predetermined period of time from departure, or within a predetermined distance from departure; receiving information indicative of an estimated weight of the aircraft upon the aircraft reaching the desired cruise altitude; determining a desired airspeed for the aircraft based on the information indicative of the estimated weight of the aircraft; prior to a flight of the aircraft, determining, based on the desired airspeed and the desired aircraft cruise insertion point, a climb trajectory for the aircraft; and during a climb flight phase of the aircraft, varying climb thrust of an engine of the aircraft to follow the climb trajectory and achieve the desired aircraft cruise insertion point.


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