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. 06, 2019

Filed:

Mar. 23, 2018
Applicant:

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

Inventor:

Lisa Graham, Prior Lake, MN (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 17/08 (2006.01); F23N 5/02 (2006.01); G01P 13/02 (2006.01); G01P 5/14 (2006.01); F23R 3/46 (2006.01); F23N 5/24 (2006.01); G01L 19/06 (2006.01);
U.S. Cl.
CPC ...
F01D 17/085 (2013.01); F23N 5/022 (2013.01); F23N 5/24 (2013.01); F23R 3/46 (2013.01); G01P 5/14 (2013.01); G01P 13/025 (2013.01); F23N 2025/04 (2013.01); F23N 2025/21 (2013.01); F23N 2041/20 (2013.01); G01L 19/0681 (2013.01);
Abstract

A pressure and temperature probe includes a probe head, a probe tip extending from the probe head and ending with a sensor face, a pressure channel extending into the probe tip through the sensor face, and a temperature channel extending into the probe tip through the sensor face. A pressure sensor is in fluid communication with a pressure channel and a temperature sensor in fluid communication with the temperature channel. The temperature channel extends parallel to the pressure channel, and the temperature channel is fluidly separate from the pressure channel. The sensor face can be configured to minimally intrude the flowpath of a working fluid, thereby minimizing disruption of the flowpath. The probe can be configured on a gas turbine engine.


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