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:
May. 21, 2019

Filed:

Jan. 31, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Federico Papa, Ellington, CT (US);

Bradley C Farnum, Tolland, CT (US);

Kristin Kopp-Vaughan, East Hartford, CT (US);

Nathan Roe, Newington, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); B64D 13/02 (2006.01); B64D 13/08 (2006.01); F02C 6/08 (2006.01); B64D 13/00 (2006.01); B64D 15/04 (2006.01); F02C 7/047 (2006.01); F02C 7/18 (2006.01); B64D 13/06 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); B64D 13/006 (2013.01); B64D 13/02 (2013.01); B64D 13/08 (2013.01); B64D 15/04 (2013.01); F02C 6/08 (2013.01); F02C 7/047 (2013.01); F02C 7/185 (2013.01); B64C 2230/04 (2013.01); B64C 2230/06 (2013.01); B64D 2013/0618 (2013.01); B64D 2033/0233 (2013.01); Y02T 50/675 (2013.01);
Abstract

A method of controlling an aircraft bleed may include the steps of monitoring a temperature of a precooled airflow exiting a precooler, and determining a status of a wing anti-ice system of an aircraft. The wing anti-ice system may be configured to receive the precooled airflow from the precooler. The method may further comprise the steps of determining whether an engine operating condition of the aircraft is within an icing envelope, selecting a temperature set point for the precooled airflow based on the status of the wing anti-ice system and whether the aircraft is within an icing envelope, and modulating a fan airflow from a fan to the precooler to adjust the temperature of the precooled airflow to the temperature set point.


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