Thermal air data (TAD) system

Patent metadata

Field	Value
Publication number	US-10073921-B1
Application number	US-201715646054-A
Country	US
Kind code	B1
Filing date	Jul 10, 2017
Priority date	Nov 21, 2014
Publication date	Sep 11, 2018
Grant date	Sep 11, 2018

Abstract

A thermal air data (TAD) sensor comprising a heat dissipating plate including a first surface and a second surface, the heat dissipating plate having a temperature maintained at the constant temperature. The heat dissipating plate is configured to be located at a first location with the first surface flush with an exterior surface of a vehicle. A temperature controller is provided to control the temperature of the heat dissipating plate to maintain the constant temperature during flight of the vehicle and is configured to calculate a value of power to maintain the heat dissipating plate at the constant temperature. An ambient air temperature sensor is to be located at a second location flush with the exterior surface of the vehicle and being paired with the first location.

First claim

I claim:

1. A thermal air data (TAD) sensor comprising:
a heat dissipating plate including a first surface and a second surface, the heat dissipating plate having a temperature maintained at the constant temperature and configured to be located at a first location with the first surface flush with an exterior surface of a vehicle;
a temperature controller configured to control the temperature of the heat dissipating plate to maintain the constant temperature during flight of the vehicle and configured to calculate a value of power to maintain the heat dissipating plate at the constant temperature; and
an ambient air temperature sensor configured to be located at a second location flush with the exterior surface of the vehicle and being paired with the first location.

2. The TAD sensor of claim 1 , further comprising:
a heater coupled to the heat dissipating plate, the heater configured to heat the heat dissipating plate to the constant temperature during the flight of the vehicle; and
a plate temperature sensor coupled to the heat dissipating plate wherein the temperature controller is coupled to the heater and the plate temperature sensor for controlling the temperature of the heat dissipating plate.

3. The TAD sensor of claim 2 , wherein the heater is a resistive heater and being in surface to surface contact with the second surface of the heat dissipating plate.

4. The TAD sensor of claim 2 , wherein the heat dissipating plate is made of a material having a thermal conductivity above 24 Btu/(hr. ° F. ft.).

5. The TAD sensor of claim 1 , further comprising a coating on the heat dissipating plate, wherein the coating is made of a material with low observability (LO) properties.

6. The TAD sensor of claim 1 , wherein the first surface is configured to reduce drag as air flows over the first surface.

7. The TAD sensor of claim 2 , wherein the first surface comprises an area; and
further comprising a plurality of plate temperature sensors wherein an average temperature is determined for the area of the first surface.

8. The TAD sensor of claim 1 , further comprising a look up table (LUT), the LUT includes columns for local air velocity of the vehicle correlated to a conjugate heat transfer coefficient as a function of one or more MACH numbers for the TAD sensor wherein the local air velocity is calculated at the TAD sensor during the flight of the vehicle.

9. The TAD sensor of claim 1 , further comprising:
calculating, by the temperature controller, a local air velocity as a function of a pairwise difference in temperature between the first location and the second location and relies on dissipated heat at the first location transferred to ambient air during the flight of the vehicle.

10. The TAD sensor of claim 9 , wherein the ambient air temperature sensor is configured to be mounted to the vehicle body at the second location wherein the first location is upstream the second location on the vehicle body.

11. A method comprising:
providing a thermal air data (TAD) sensor comprising a heat dissipating plate including a first surface and a second surface, the heat dissipating plate having a temperature maintained at a constant temperature and configured to be located at a first location with the first surface flush with an exterior surface of a vehicle, a temperature controller and an ambient air temperature sensor;
sensing ambient air temperature, by the ambient air temperature sensor, at a second location different from the first location and paired with the first location;
controlling, by the temperature controller, the temperature of the heat dissipating plate to the constant temperature; and
calculating, by the temperature controller, a value of power to maintain the heat dissipating plate at the constant temperature during flight of the vehicle.

12. The method of claim 11 , further comprising:
heating, by a heater coupled to the heat dissipating plate, the heat dissipating plate to the constant temperature during the flight of the vehicle; and
sensing, by a plate temperature sensor coupled to the heat dissipating plate, a plate temperature wherein the temperature controller is coupled to the heater and the plate temperature sensor.

13. The method of claim 12 , wherein the heater is a resistive heater and being in surface to surface contact with the second surface of the heat dissipating plate.

14. The method of claim 11 , wherein the providing of the heat dissipating plate comprises providing the heat dissipating plate made of a material having a thermal conductivity above 24 Btu/(hr. ° F. ft.).

15. The method of claim 11 , wherein the providing of the heat dissipating plate includes providing the heat dissipating plate with a coating made of a material with low observability (LO) properties.

16. The method of claim 11 , wherein the first surface is configured to reduce drag as air flows over the first surface; and
further comprising reducing drag as the air flows over the first surface.

17. The method of claim 11 , further comprising providing a look up table (LUT), the LUT includes columns for local velocity of the vehicle correlated to a conjugate heat transfer coefficient as a function of one or more MACH numbers for the TAD sensor wherein the local velocity is calculated at the TAD sensor during the flight of the vehicle.

18. The method of claim 11 , further comprising:
calculating, by the temperature controller, a local air velocity as a function of a pairwise difference in temperature between the first location and the second location and relies on dissipated heat at the first location transferred to ambient air during the flight of the vehicle.

19. The method of claim 18 , wherein the ambient air temperature sensor is configured to be mounted to the vehicle body at the second location wherein the first location is upstream the second location on the vehicle body.

Assignees

• Lockheed Corp

Inventors

• Richardson Nathan R

Classifications

• G06F17/3089 Primary

  Physics · mapped topic

• G06N5/022

  Knowledge engineering; Knowledge acquisition · CPC title

• G01P13/025 Primary

  indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw · CPC title

• B64D43/02

  for indicating aircraft speed or stalling conditions · CPC title

• G01P5/10

  by measuring thermal variables · CPC title