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:
Oct. 23, 2018

Filed:

Oct. 30, 2015
Applicant:

GE Aviation Systems Llc, Grand Rapids, MI (US);

Inventors:

Nicholas Visser, Grand Rapids, MI (US);

Sridhar Adibhatla, Glendale, OH (US);

David Michael Lax, Grand Rapids, MI (US);

Assignee:

GE Aviation Systems LLC, Grand Rapids, MI (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); F01D 21/00 (2006.01); G01S 13/95 (2006.01); F02C 9/18 (2006.01); F02C 9/00 (2006.01); F02C 9/28 (2006.01); F02C 9/52 (2006.01); G01S 17/95 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); F01D 21/003 (2013.01); F02C 9/00 (2013.01); F02C 9/18 (2013.01); F02C 9/28 (2013.01); F02C 9/52 (2013.01); G01S 13/953 (2013.01); G01S 17/95 (2013.01); B64D 2013/0618 (2013.01); F05D 2270/096 (2013.01); F05D 2270/311 (2013.01); F05D 2270/313 (2013.01); F05D 2270/805 (2013.01); Y02A 90/18 (2018.01); Y02A 90/19 (2018.01); Y02T 50/56 (2013.01); Y02T 50/671 (2013.01);
Abstract

Systems and methods for enhancing engine performance based on atmospheric ice particles are provided. For example, a method can include selecting one or more points along a flight path of an aircraft and receiving a reflectivity measurement for each of the one or more points obtained using a device located on the aircraft. The method can further include determining an estimate of ice water content for each of the one or more points based at least in part on the reflectivity measurements; and controlling at least one component of the aircraft engine (e.g., a variable bleed valve) based at least in part on the estimate of ice water content for at least one of the plurality of points.


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