IP Library Granted Patent US 12,339,294
Granted Patent B2
US 12,339,294 · App. 17/799,863 · Granted Jun 24, 2025

Angle of attack sensor vane geometry

Inventors: Armando Valdes Chavez (Lakeville, MN); Luke Anderson (Plymouth, MN); Kaleb Anderson (Goodhue, MN)
Assignee: Rosemount Aerospace Inc.
G01P13/025B64D43/02G01C21/10
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Quick Facts
Patent No.
US 12,339,294
App. No.
17/799,863
Granted
Jun 24, 2025
Kind
B2
Abstract

An angle of attack sensor includes a housing and a faceplate. A vane assembly extends through a central opening of the faceplate and includes a vane. The vane comprises a root, a tip, a leading edge, a trailing edge, a first lateral face, and a second lateral face. The first lateral face and the second lateral face are symmetric about a chord of the vane and each have a forward section with an outer surface profile that is nonlinear and geometrically convex from the leading edge to a transition point at a tangent to the widest point of the geometrically convex outer surface profile and each have an aft section with an outer surface profile that extends out to form a diverging wedge shape from the transition point to the trailing edge.

Claims (56)

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;

a vane assembly extending through the central opening of the faceplate, the vane assembly comprising:

a vane hub positioned in the central opening of the faceplate; and

a vane connected to the vane hub, the vane comprising:

a root connected to the vane hub;

a tip opposite the root;

a leading edge extending from the root to the tip;

a trailing edge extending from the root to the tip opposite the leading edge;

a first lateral face extending from the leading edge to the trailing edge; and

a second lateral face opposite the first lateral face and extending from the leading edge to the trailing edge;

wherein the first lateral face and the second lateral face are symmetric about a chord of the vane and each have a forward section with an outer surface profile that is nonlinear and geometrically convex from the leading edge to a transition point at a tangent to the widest point of the geometrically convex outer surface profile and each have an aft section with an outer surface profile that extends out to form a diverging wedge shape from the transition point to the trailing edge.

2. The angle of attack sensor of claim 1 , further comprising a vane heating element disposed within the vane between the first lateral face and the second lateral face proximate the leading edge.

3. The angle of attack sensor of claim 2 , wherein the vane heating element has a forward end disposed at a distance from the leading edge of the vane that is less than ten percent of a length of the chord of the vane.

4. The angle of attack sensor of claim 2 , further comprising a plurality of vane heating elements disposed within the vane between the first lateral face and the second lateral face proximate the leading edge.

5. The angle of attack sensor of claim 4 , wherein each of the plurality of vane heating elements has a forward end disposed at a distance from the leading edge of the vane that is less than ten percent of a length of the chord of the vane.

6. The angle of attack sensor of claim 2 , wherein the vane heating elements are self-regulating heating elements.

7. The angle of attack sensor of claim 1 , wherein the first lateral face and the second lateral face are shaped to decrease an amount of heat dissipation from the vane.

8. The angle of attack sensor of claim 1 , further comprising a faceplate heater positioned on an inner surface of the faceplate and extending around the vane assembly.

9. The angle of attack sensor of claim 8 , wherein the faceplate heater comprises a plurality of heating elements mounted on the faceplate.

10. The angle of attack sensor of claim 9 , wherein the plurality of heating elements are arranged to provide a higher concentration of heat to the faceplate upstream of the vane assembly.

11. The angle of attack sensor of claim 1 , further comprising:

a vane shaft that extends into the housing and is connected to the vane assembly; and

a rotational position sensor connected to the vane shaft.

12. The angle of attack sensor of claim 1 , wherein the diverging wedge shape has an angle of up to 45 degrees.

13. 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;

a vane assembly extending through the central opening of the faceplate, the vane assembly comprising:

a vane hub positioned in the central opening of the faceplate; and

a vane connected to the vane hub, the vane comprising:

a root connected to the vane hub;

a tip opposite the root;

a leading edge extending from the root to the tip;

a trailing edge extending from the root to the tip opposite the leading edge;

a first lateral face extending from the leading edge to the trailing edge; and

a second lateral face opposite the first lateral face and extending from the leading edge to the trailing edge;

wherein the first lateral face and the second lateral face are symmetric about a chord of the vane and form a truncated symmetrical NACA profile extending downstream from the leading edge to a wedge-like profile extending from the truncated NACA profile to the trailing edge.

14. The angle of attack sensor of claim 13 , wherein the truncated NACA profile and the wedge-like profile meet at a transition point at a tangent to the widest point of the NACA profile.

15. The angle of attack sensor of claim 13 , wherein the truncated NACA profile and the wedge-like profile meet at a transition point at a point of maximum thickness of the truncated NACA profile.

16. The angle of attack sensor of claim 13 , further comprising a vane heating element disposed within the vane between the first lateral face and the second lateral face proximate the leading edge.

17. The angle of attack sensor of claim 16 , wherein the vane heating element has a forward end disposed at a distance from the leading edge of the vane that is less than ten percent of a length of the chord of the vane.

18. The angle of attack sensor of claim 13 , further comprising a plurality of vane heating elements disposed within the vane between the first lateral face and the second lateral face proximate the leading edge, wherein each of the plurality of vane heating elements has a forward end disposed at a distance from the leading edge of the vane that is less than ten percent of a length of the chord of the vane.

19. The angle of attack sensor of claim 13 , wherein the first lateral face and the second lateral face are shaped to decrease an amount of heat dissipation from the vane.

20. The angle of attack sensor of claim 13 , further comprising a faceplate heater positioned on an inner surface of the faceplate and extending around the vane assembly, wherein the faceplate heater comprises a plurality of heating elements mounted on the faceplate and arranged to provide a higher concentration of heat to the faceplate upstream of the vane assembly.

21. The angle of attack sensor of claim 13 , further comprising:

a vane shaft that extends into the housing and is connected to the vane assembly; and

a rotational position sensor connected to the vane shaft.

22. The angle of attack sensor of claim 13 , wherein the first lateral face and the second lateral face of the wedge-like profile form an angle equal to or between 0 degrees and 45 degrees.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 15, 2022
From: VALDES CHAVEZ, ARMANDO; ANDERSON, KALEB; ANDERSON, LUKE
To: ROSEMOUNT AEROSPACE INC.
Reel/Frame 060810/0878 →
Continuity (2)
Provisional Application 62981256 · Feb 25, 2020
Related Publication 20230073522A1 · Mar 9, 2023
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