Angle of attack sensor with sloped faceplate

Patent metadata

Field	Value
Publication number	US-12360134-B2
Application number	US-202117799855-A
Country	US
Kind code	B2
Filing date	Feb 25, 2021
Priority date	Feb 25, 2020
Publication date	Jul 15, 2025
Grant date	Jul 15, 2025

Abstract

An angle of attack sensor includes a housing having an open end and a closed end, a faceplate positioned on the open end of the housing, the faceplate comprising a periphery at an outer edge of the faceplate, a central opening, and an exterior surface extending from the periphery to the central opening, and a vane assembly extending through the central opening of the faceplate. The exterior surface of the faceplate has a sloped profile from the periphery to the central opening.

First claim

The invention claimed is:

1. An angle of attack sensor comprising:
a housing having an open end and a closed end;
a faceplate positioned on the open end of the housing, the faceplate comprising:
a periphery at an outer edge of the faceplate;
a central opening; and
an exterior surface extending from the periphery to the central opening; and

a vane assembly extending through the central opening of the faceplate;
wherein the exterior surface of the faceplate has a sloped profile from the periphery to the central opening;
wherein the exterior surface of the faceplate has a slope equal to or between 6 degrees and 30 degrees.

2. The angle of attack sensor of claim 1 , wherein the sloped profile of the faceplate has an axis and is axisymmetric, the axis of the sloped profile of the faceplate being the same as an axis of the vane assembly.

3. The angle of attack sensor of claim 1 , wherein the faceplate has a frustoconical exterior surface.

4. The angle of attack sensor of claim 1 , further including a heater configured to provide heat to the faceplate.

5. The angle of attack sensor of claim 1 , wherein the exterior surface of the faceplate has a sloped profile from the periphery to the central opening at the upstream portion of the faceplate.

6. The angle of attack sensor of claim 1 , wherein the vane assembly includes a vane hub positioned in the central opening of the faceplate and a vane connected to the vane hub, an exterior surface of the vane hub and the vane being above the skin of the aircraft.

7. The angle of attack sensor of claim 6 , wherein the exterior surface of the faceplate has a slope equal to or between 6 degrees and 12 degrees and a distance from a tip of the vane and a skin of an aircraft is between 3.1 and 3.2 inches.

8. The angle of attack sensor of claim 6 , wherein the vane has a vane height of 71 mm and a vane sweep angle of 38 degrees and the faceplate has a slope of 8 degrees.

9. The angle of attack sensor of claim 1 , wherein the faceplate has a sloped profile from the periphery to the central opening to create a shadowing effect aft of the vane assembly.

10. The angle of attack sensor of claim 1 , wherein a height of the faceplate at the central opening is greater than a height of the faceplate at the periphery.

11. An angle of attack sensor comprising:
a housing having an open end and a closed end;
a faceplate positioned on the open end of the housing, the faceplate comprising:
a periphery at an outer edge of the faceplate;
a central opening; and
an exterior surface extending from the periphery to the central opening; and

a vane assembly extending through the central opening of the faceplate;
wherein the exterior surface of the faceplate has a continuous incline from the periphery to the central opening; and
wherein the exterior surface of the faceplate has a continuous incline with a slope equal to or between 6 degrees and 30 degrees.

12. The angle of attack sensor of claim 11 , wherein the faceplate has a frustoconical exterior surface.

13. The angle of attack sensor of claim 11 , further including a heater configured to provide heat to the faceplate.

14. The angle of attack sensor of claim 11 , wherein the exterior surface of the faceplate continuously inclines from the periphery to the central opening at the upstream portion of the faceplate.

15. The angle of attack sensor of claim 11 , wherein the vane assembly includes a vane hub positioned in the central opening of the faceplate and a vane connected to the vane hub, an exterior surface of the vane hub and the vane being above the skin of the aircraft.

16. The angle of attack sensor of claim 15 , wherein the exterior surface of the faceplate has a continuous incline with a slope equal to or between 6 degrees and 12 degrees and a distance from a tip of the vane and a skin of an aircraft is between 3.1 and 3.2 inches.

17. The angle of attack sensor of claim 15 , wherein the vane has a vane height of 71 mm and a vane sweep angle of 38 degrees and the faceplate has a continuous incline with a slope of 8 degrees.

18. An angle of attack sensor comprising:
a housing having an open end and a closed end;
a faceplate positioned on the open end of the housing, the faceplate comprising:
a periphery at an outer edge of the faceplate;
a central opening; and
an exterior surface extending from the periphery to the central opening; and

a vane assembly extending through the central opening of the faceplate;
wherein the exterior surface of the faceplate slopes downward and outward from the central opening to the periphery; and
wherein the exterior surface of the faceplate has a slope equal to or between 6 degrees and 30 degrees.

19. The angle of attack sensor of claim 18 , wherein the faceplate has a frustoconical exterior surface.

20. The angle of attack sensor of claim 18 , wherein the vane assembly includes a vane hub positioned in the central opening of the faceplate and a vane connected to the vane hub, an exterior surface of the vane hub and the vane being above the skin of the aircraft.

21. The angle of attack sensor of claim 20 , wherein the exterior surface of the faceplate has a slope equal to or between 6 degrees and 12 degrees and the distance from a tip of the vane and a skin of an aircraft is between 3.1 and 3.2 inches.

22. The angle of attack sensor of claim 20 , wherein the vane has a height of 71 mm and a vane sweep angle of 38 degrees and the faceplate has a slope of 8 degrees.

23. The angle of attack sensor of claim 18 , wherein the faceplate slopes downward and outward from the central opening to the periphery at the upstream portion of the faceplate.

Assignees

• Rosemount Aerospace Inc

Inventors

• Whalen Mackenzie
• Cusher Aaron A
• Valdes Chavez Armando
• Hanson Daniel
• Schwartz Richard Alan
• Johnson Wallace
• Krueger William B
• Anderson Kaleb

Classifications

• G01C21/10 Primary

  by using measurements of speed or acceleration (G01C21/24, G01C21/26 take precedence) · CPC title

• B64D43/02

  for indicating aircraft speed or stalling conditions · 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