Angle of attack sensor with thermal enhancement

Patent metadata

Field	Value
Publication number	US-11768219-B2
Application number	US-202117506382-A
Country	US
Kind code	B2
Filing date	Oct 20, 2021
Priority date	Aug 17, 2017
Publication date	Sep 26, 2023
Grant date	Sep 26, 2023

Abstract

An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.

First claim

The invention claimed is:

1. An angle of attack sensor comprising:
a vane assembly; and
a multi-piece faceplate adjacent the vane assembly, the faceplate including:
a heated chassis defining a pocket; and
a mounting plate positioned on the heated chassis and having a first opening;

wherein the vane assembly has a vane base that is positioned in the pocket of the heated chassis and connected to a vane shaft, and the heated chassis includes a protrusion that extends into a second opening in the mounting plate, the second opening extending from an interior surface of the mounting plate to an exterior surface of the mounting plate and the protrusion extending into the second opening toward the exterior surface of the mounting plate.

2. The angle of attack sensor of claim 1 , wherein the heated chassis is made of thermally conductive metal or metal alloys, and the mounting plate is made of a material selected from the group consisting of: polymers, composites, and metals.

3. The angle of attack sensor of claim 1 , further including a heater positioned on the heated chassis.

4. The angle of attack sensor of claim 3 , further including a fastener connected to the heated chassis and the mounting plate.

5. The angle of attack sensor of claim 4 , wherein the heated chassis defines the pocket at a central portion of the heated chassis.

6. The angle of attack sensor of claim 5 , further including an air gap between the heated chassis and the mounting plate.

7. The angle of attack sensor of claim 1 , further including a standoff positioned between the heated chassis and the mounting plate, wherein the standoff is configured to be a thermal break between the heated chassis and the mounting plate.

8. The angle of attack sensor of claim 7 , wherein the standoff is comprised of a material selected from the group consisting of: stainless steel, plastic, polymers, and composites.

9. The angle of attack sensor of claim 8 , further including an air gap between the heated chassis and the mounting plate.

10. The angle of attack sensor of claim 9 , wherein the heated chassis includes an annular space extending into the heated chassis from an exterior surface of the heated chassis.

11. The angle of attack sensor of claim 1 , wherein the protrusion and the second opening are positioned downstream of the vane assembly.

12. The angle of attack sensor of claim 1 , wherein the heated chassis includes a second protrusion that extends into a third opening in the mounting plate.

13. A faceplate for an angle of attack sensor comprising:
a heated chassis defining a pocket at a central portion of the heated chassis, the pocket being configured to receive a vane base of a vane assembly connected to a vane shaft; and
a mounting plate positioned on the heated chassis and having a first opening and a second opening, the first opening and the second opening each extending from an interior surface of the mounting plate to an exterior surface of the mounting plate;
wherein the heated chassis includes a protrusion that extends into the second opening in the mounting plate toward the exterior surface of the mounting plate.

14. The faceplate of claim 13 , wherein the heated chassis is made of thermally conductive metal or metal alloys, and the mounting plate is thermally isolated from the heated chassis.

15. The faceplate of claim 14 , wherein the heated chassis includes a ring portion that extends into the first opening of the mounting plate.

16. The faceplate of claim 13 , wherein the heated chassis includes an annular space extending into the heated chassis from an exterior surface of the heated chassis.

17. The faceplate of claim 16 , further including a standoff positioned between the heated chassis and the mounting plate, wherein the standoff is configured to be a thermal break between the heated chassis and the mounting plate.

18. The faceplate of claim 17 , further including an air gap located between the mounting plate and the heated chassis.

19. The faceplate of claim 18 , wherein the heated chassis includes a second protrusion that extends into a third opening in the mounting plate.

20. The faceplate of claim 19 , further including a heater positioned on the heated chassis and a fastener connected to the heated chassis and the mounting plate.

Assignees

• Rosemount Aerospace Inc

Inventors

• Reid Alexander N
• Schwartz Richard Alan
• Krueger William B
• Deangelo Timothy
• Freeman Kenneth

Classifications

• G01P13/025 Primary

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

• B64D43/00

  Arrangements or adaptations of instruments · CPC title

• B64D45/0005

  Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear · CPC title

• B64D15/14

  controlled cyclically along length of surface · CPC title