Checking and angle-of-attack sensor vane assembly

Patent metadata

Field	Value
Publication number	US-11906541-B2
Application number	US-202016894714-A
Country	US
Kind code	B2
Filing date	Jun 5, 2020
Priority date	Jun 6, 2019
Publication date	Feb 20, 2024
Grant date	Feb 20, 2024

Abstract

Methods and devices for checking the geometry of an angle-of-attack sensor belonging to an aircraft are provided. The device includes one or more stages, a stage comprising a slot the geometric dimensions of which are specifically configured to accept a portion of the said angle-of-attack sensor. The device allows a visual inspection but can also be instrumented (photoelectric cell, laser, camera) in order to verify the geometry of the sensor in detail. Developments notably describe the use of signal indicators, motorized stages, one or more image sensors, specific materials, communications with computers, or placement by drone and/or robotic arm. Software aspects are described.

First claim

The invention claimed is:

1. An assembly comprising:
an angle of attack sensor of an aircraft, the angle of attack sensor comprising a body and a vane assembly mounted on said body, the vane assembly comprising a vane and a base, the base of the vane assembly being pivotable relative to the body and the vane; and
a device comprising several levels, each level comprising a notch whose geometric dimensions are specifically configured to receive and embrace a portion of the vane of the angle of attack sensor when the device is placed against the vane of the vane assembly directly on the aircraft.

2. The assembly according to claim 1 , wherein the several levels of said device comprises only two levels.

3. The assembly according to claim 1 , wherein the several levels of said device comprises only three levels.

4. The assembly according to claim 1 , wherein the several levels of said device comprises more than three levels.

5. The assembly according to claim 1 , wherein said device comprises a photoelectric cell and a laser, which are arranged in such a way as to check the straightness of the vane of the vane assembly.

6. The assembly according to claim 1 , wherein at least one level comprises one or more image sensors.

7. The assembly according to claim 1 , wherein at least one level is motorized.

8. The assembly according to claim 1 , wherein said device is obtained at least partially by additive printing.

9. The assembly according to claim 1 , wherein one or more parts of the device are made from materials the hardness properties of which are inferior to that of the external surface material of the vane of the angle of attack sensor.

10. The assembly according to claim 1 , further comprising a signal light to avoid or reduce the risk of being left behind on the aircraft.

11. The assembly according to claim 1 , said device configured for being connected to a mobile telephone or to a remote server, the device comprising a communication module including at least one of Bluetooth, Wifi, 3G, 4G, LTE, and 5G.

12. The assembly according to claim 1 , further comprising a slide and lock mechanism for retaining said device when it is positioned against the vane assembly.

13. A method for checking the geometry of a vane of an angle of attack sensor directly on an aircraft, comprising the steps of:
using the assembly of claim 1 to place the device against the vane of the angle of attack sensor to be directly controlled on the aircraft; and
verifying the geometry of the vane of the angle of attack sensor with respect to a predefined geometry by measuring one or more geometric points of the device placed against the vane of the angle of attack sensor.

14. The method according to claim 13 , wherein the device is placed against the angle of attack sensor by a drone and/or by a robotic arm.

15. The method according to claim 13 , further comprising a step of emitting a message and/or a light signal and/or an audio signal and/or a vibration depending on the step of verifying the geometry of the vane of the angle of attack sensor.

Assignees

• Thales Sa

Inventors

• Hemelsdael Cécile
• Damiens Tessier Stéphane

Classifications

• G01P21/00 Primary

  Testing or calibrating of apparatus or devices covered by the preceding groups · CPC title

• G01B3/38

  Gauges with an open yoke and opposed faces, i.e. calipers, in which the internal distance between the faces is fixed, although it may be preadjustable · 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

• G01P21/025

  for measuring speed of fluids; for measuring speed of bodies relative to fluids (for measuring volume flow G01F25/10) · CPC title