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. 23, 2023

Filed:

Feb. 28, 2020
Applicant:

Rosemount Aerospace Inc., Burnsville, MN (US);

Inventors:

Andrew Holl, Lakeville, MN (US);

Scott Wigen, Eagan, MN (US);

Robert Edward Sable, Lakeville, MN (US);

Scott D. Isebrand, Minneapolis, MN (US);

Brian Boyd, Burnsville, MN (US);

Assignee:

ROSEMOUNT AEROSPACE INC., Burnsville, MN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 17/08 (2006.01); G01K 13/02 (2021.01); F01D 25/02 (2006.01); G01K 1/14 (2021.01); G01K 1/20 (2006.01); G01L 19/00 (2006.01); G01L 19/14 (2006.01); G01L 19/06 (2006.01);
U.S. Cl.
CPC ...
F01D 17/085 (2013.01); F01D 25/02 (2013.01); G01K 1/14 (2013.01); G01K 1/20 (2013.01); G01K 13/028 (2013.01); F05D 2270/303 (2013.01); F05D 2270/80 (2013.01); G01L 19/0092 (2013.01); G01L 19/0654 (2013.01); G01L 19/14 (2013.01);
Abstract

A sensor includes an airfoil body, a heater element, and a temperature probe. The airfoil body defines a sensor axis, an insulating cavity, and extends between a leading edge and a trailing edge of the airfoil body. The heater element extends axially within the airfoil body and is positioned between the leading edge and the trailing edge of the airfoil body. The temperature probe extends axially within the airfoil body, is positioned between the heater element and the trailing edge of the airfoil body, and is separated from the heater element by the insulating cavity to limit thermal communication between the temperature probe and the heater element. Gas turbine engines, methods of making sensors, and methods of thermally separating temperature probes and heater elements in sensors are also described.


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