Total air temperature probes for reducing deicing heater error

Patent metadata

Field	Value
Publication number	US-9658117-B2
Application number	US-201313964693-A
Country	US
Kind code	B2
Filing date	Aug 12, 2013
Priority date	Aug 18, 2012
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

A total air temperature probe includes a probe head having an airflow inlet, a main airflow outlet, a main probe head wall extending from the airflow inlet to the main airflow outlet, and a flow separation bend wall positioned between the airflow inlet and the main airflow outlet. The flow separation bend wall is opposite the main probe head wall across a primary flow passage defined through the probe head from the airflow inlet to the main airflow outlet. A flow separation trip feature is defined on an interior surface of the main probe head wall for tripping a boundary layer flow separation in flow in the primary flow passage, e.g., for reduction of deicing heater error.

First claim

What is claimed is:

1. A total air temperature probe comprising:
a probe head having an airflow inlet, a main airflow outlet, a main probe head wall extending from the airflow inlet to the main airflow outlet, and a flow separation bend wall positioned between the airflow inlet and the main airflow outlet, the flow separation bend wall being opposite the main probe head wall across a primary flow passage defined through the probe head from the airflow inlet to the main airflow outlet;
opposed sidewalls, each sidewall connecting between the main probe head wall and the flow separation bend wall; and
a flow separation trip feature defined on an interior surface of the main probe head wall for tripping a boundary layer flow separation in flow in the primary flow passage, wherein the flow separation trip feature spans the main probe head wall from one of the opposed sidewalls to the other, and, wherein the flow separation trip feature has a leading notch edge spaced inward from the airflow inlet.

2. A total air temperature probe as recited in claim 1 , further comprising:
a sensor passage connected to the primary flow passage and oriented at an angle relative to a flow axis defined from the airflow inlet to the main airflow outlet, wherein a temperature sensor is mounted within the sensor passage for total air temperature measurements; and
a deicing heater operatively connected to heat the probe head and to form a heated boundary layer within the primary flow passage with a portion of the heated boundary layer passing from the primary flow passage into the sensor passage, wherein the temperature sensor and the flow separation trip feature are positioned so the portion of the heated boundary layer passing into the sensor passage substantially avoids the sensor for reduction of deicing heater error.

3. A total air temperature probe as recited in claim 2 , wherein the sensor passage includes a sensor passage wall, and wherein a thermal shield is included in the sensor passage between the sensor and the sensor passage wall, wherein the flow separation trip feature and thermal shield are positioned so the portion of the heated boundary layer passing into the sensor passage substantially avoids spilling into the thermal shield.

4. A total air temperature probe as recited in claim 1 , wherein the flow separation trip feature includes a notch set in from the interior surface of the main probe head wall.

5. A total air temperature probe as recited in claim 4 , wherein the notch has a leading notch edge spaced inward from the airflow inlet by 0.8 inches (2.032 cm).

6. A total air temperature probe as recited in claim 4 , wherein the notch has a depth relative to the interior surface of the main probe head wall of 0.008 inches (0.0203 cm).

7. A total air temperature probe as recited in claim 1 , wherein the flow separation trip feature includes a protrusion set out from the interior surface of the main probe head wall.

8. A total air temperature probe as recited in claim 7 , wherein the protrusion has a leading edge spaced inward from the airflow inlet by 0.8 inches (2.032 cm).

9. A total air temperature probe as recited in claim 7 , wherein the protrusion protrudes from the interior surface of the main probe head wall by 0.008 inches (0.0203 cm).

Assignees

• Rosemount Aerospace Inc

Inventors

• Herman Chad James
• Larson Howard Earl

Classifications

• G01K13/028 Primary

  for use in total air temperature [TAT] probes · CPC title

• G01K13/024

  of moving gases · CPC title

• G01K1/20 Primary

  Compensating for effects of temperature changes other than those to be measured, e.g. changes in ambient temperature · CPC title