IP Library › Granted Patent US 10,928,416
Granted Patent B2
US 10,928,416 · App. 15/975,378 · Granted Feb 23, 2021

Dual heated ramp for ice and water management in angle of attack sensors

Inventors: Alexander N. Reid (St. Louis Park, MN); Richard Alan Schwartz (Fairbault, MN)
Assignee: Rosemount Aerospace Inc.
G01P13/025B64D15/00G01P13/004G01P13/02
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Quick Facts
Patent No.
US 10,928,416
App. No.
15/975,378
Granted
Feb 23, 2021
Kind
B2
Abstract

An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a mounting plate having an opening and a heated chassis positioned adjacent the mounting plate and having a ring portion extending through the opening, the ring portion defining a ring-shaped deflector that surrounds the vane assembly and extends beyond an exterior surface of the mounting plate.

Claims (69)

1. An angle of attack sensor comprising:

a vane assembly; and

a multi-piece faceplate adjacent the vane assembly, the faceplate including:

a mounting plate having an opening; and

a heated chassis positioned adjacent the mounting plate and having a ring portion extending through the opening, the ring portion defining a ring-shaped deflector that surrounds the vane assembly and extends beyond an exterior surface of the mounting plate; wherein the deflector includes:

a fore ramp at an upstream portion of the deflector; and

an aft ramp at a downstream portion of the deflector, the aft ramp including an inclined inner surface with an incline in an aft direction.

2. The angle of attack sensor of claim 1 , wherein:

the fore ramp includes:

an inclined outer surface with an incline in an aft direction; and

a vertical inner surface substantially perpendicular to the exterior surface of the mounting plate; and

the aft ramp includes:

a vertical outer surface substantially perpendicular to the exterior surface of the mounting plate.

3. The angle of attack sensor of claim 2 , wherein the inclined outer surface is continuous with the inclined inner surface.

4. The angle of attack sensor of claim 1 , wherein the deflector is configured to redirect impinging ice or water away from exterior surface of mounting plate.

5. The angle of attack sensor of claim 1 , wherein the deflector is heated.

6. The angle of attack sensor of claim 1 , wherein the angle of attack sensor further includes a heater thermally coupled to the deflector and positioned on the heated chassis.

7. An angle of attack sensor comprising:

a vane assembly; and

a multi-piece faceplate adjacent the vane assembly, the faceplate including:

a mounting plate having an opening; and

a heated chassis positioned adjacent the mounting plate and having a ring portion extending through the opening, the ring portion defining a ring-shaped deflector that surrounds the vane assembly and extends beyond an exterior surface of the mounting plate; wherein the deflector includes:

a fore ramp at an upstream portion of the deflector, the fore ramp including:

tapered end sections; and

a center section between tapered end sections; and

an aft ramp at a downstream portion of the deflector.

8. The angle of attack sensor of claim 7 , wherein the center section of the fore ramp extends beyond the exterior surface of the mounting plate.

9. The angle of attack sensor of claim 7 , wherein the center section of the fore ramp is configured to be substantially normal to oncoming airflow when the angle of attack sensor is installed on an aircraft.

10. An angle of attack sensor comprising:

a vane assembly; and

a multi-piece faceplate adjacent the vane assembly, the faceplate including:

a mounting plate having an opening; and

a heated chassis positioned adjacent the mounting plate and having a ring portion extending through the opening, the ring portion defining a ring-shaped deflector that surrounds the vane assembly and extends beyond an exterior surface of the mounting plate; wherein the deflector includes:

a fore ramp at an upstream portion of the deflector; and

an aft ramp at a downstream portion of the deflector, the aft ramp including:

tapered end sections; and

a center section between tapered end sections.

11. The angle of attack sensor of claim 10 , wherein the center section of the aft ramp extends beyond the exterior surface of the mounting plate.

12. The angle of attack sensor of claim 10 , wherein the center section of the aft ramp is configured to be substantially normal to oncoming airflow when the angle of attack sensor is installed on an aircraft.

13. A method for preventing significant ice accumulation on a faceplate adjacent a vane assembly, the faceplate including a heated chassis adjacent a mounting plate, the method comprising:

re-routing fluid and particles away from an exterior surface of the mounting plate with a fore ramp of a deflector defined by the heated chassis, the fore ramp at an upstream portion of the deflector; and

re-routing fluid away from the exterior surface of the mounting plate with an aft ramp of the deflector, the aft ramp at a downstream portion of the deflector and including an inclined inner surface with an incline in an aft direction.

14. A method for preventing significant ice accumulation on a faceplate adjacent a vane assembly, the faceplate including a heated chassis adjacent a mounting plate, the method comprising:

re-routing fluid and particles away from an exterior surface of the mounting plate with a fore ramp of a deflector defined by the heated chassis; and

re-routing fluid away from the exterior surface of the mounting plate with an aft ramp of the deflector; wherein re-routing fluid away from the exterior surface of the mounting plate with an aft ramp of the deflector includes capturing the fluid and releasing the fluid into oncoming airflow.

15. A heated chassis for use in an angle of attack sensor having a vane assembly and a multi-piece faceplate including a mounting plate with an opening, the heated chassis positioned adjacent the mounting plate and comprising:

a pocket within which a portion of the vane assembly is positioned; and

a ring portion extending through the opening of the mounting plate and defining a heated ring-shaped deflector that surrounds the vane assembly and extends beyond an exterior surface of the mounting plate, wherein the deflector includes:

a fore ramp at an upstream portion of the deflector; and

an aft ramp at a downstream portion of the deflector, the aft ramp including an inclined inner surface with an incline in an aft direction.

16. The heated chassis of claim 15 , wherein:

the fore ramp at the upstream portion of the deflector is forward of the vane; and

the aft ramp at the downstream portion of the deflector is rearward of the vane.

17. The heat chassis of claim 15 , wherein:

the fore ramp includes:

an inclined outer surface with an incline in an aft direction; and

a vertical inner surface substantially perpendicular to the exterior surface of the mounting plate; and

the aft ramp includes:

a vertical outer surface substantially perpendicular to the exterior surface of the mounting plate.

18. The heated chassis sensor of claim 17 , wherein the inclined outer surface is continuous with the inclined inner surface.

19. A heated chassis for use in an angle of attack sensor having a vane assembly and a multi-piece faceplate including a mounting plate with an opening, the heated chassis positioned adjacent the mounting plate and comprising:

a pocket within which a portion of the vane assembly is positioned; and

a ring portion extending through the opening of the mounting plate and defining a heated ring-shaped deflector that surrounds the vane assembly and extends beyond an exterior surface of the mounting plate, wherein the deflector includes:

a fore ramp at an upstream portion of the deflector, the fore ramp including:

tapered end sections; and

a center section between tapered end sections; and

an aft ramp at a downstream portion of the deflector, the aft ramp including:

tapered end sections; and

a center section between tapered end sections.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 9, 2018
From: REID, ALEXANDER N.; SCHWARTZ, RICHARD ALAN
To: ROSEMOUNT AEROSPACE INC.
Reel/Frame 045756/0748 →
Continuity (1)
Related Publication 20190346478A1 · Nov 14, 2019
Cited By (3)
US 12,339,294 US 12,345,731 US 12,360,134