IP Library Granted Patent US 12,442,831
Granted Patent B2
US 12,442,831 · App. 18/338,067 · Granted Oct 14, 2025

Pitot tube sensing apparatus

Inventor: Anmol Dhandhania (Bristol, GB)
Assignee: AIRBUS (SAS)
G01P5/165B64D15/20G01F1/46
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Quick Facts
Patent No.
US 12,442,831
App. No.
18/338,067
Granted
Oct 14, 2025
Kind
B2
Abstract

A pitot tube sensing apparatus and method are disclosed for determining the presence or absence of a foreign object within the pitot tube sensing apparatus, and including a pitot tube having a channel, a pressure sensor coupled to the channel, a capacitor and a system. The capacitor includes two electrodes on opposing sides of the channel. The system measures a parameter indicative of a capacitance between the two electrodes and determines the presence or absence of a foreign object within the channel based on the parameter.

Claims (34)

1. A pitot tube sensing apparatus comprising:

a pitot tube comprising a channel;

a pressure sensor coupled to the channel;

a capacitor comprising two electrodes on opposing sides of the channel, wherein the two electrodes conform to a shape of an inner surface of the channel; and

a system configured to:

measure a capacitance between the two electrodes; and determine the presence or absence of a foreign object within the channel based on the capacitance.

2. The pitot tube sensing apparatus of claim 1 , further comprising electrical shielding between the capacitor and the pitot tube.

3. The pitot tube sensing apparatus of claim 1 , wherein measuring the capacitance comprises measuring a voltage between the two electrodes.

4. The pitot tube sensing apparatus of claim 1 , wherein the system is configured to measure the capacitance by applying current across the capacitor.

5. The pitot tube sensing apparatus of claim 1 , wherein the determination of the presence or absence of a foreign object is based on a comparison of the capacitance to a detection threshold.

6. The pitot tube sensing apparatus of claim 1 , wherein the system is further configured to calculate a rate of change in the capacitance, wherein the determination of the presence or absence of a foreign object is based on a comparison of the rate of change in the capacitance to a detection threshold.

7. The pitot tube sensing apparatus of claim 1 , wherein the inner surface of the channel and an inner surface of each electrode have a curved shape in a plane perpendicular to a length of the channel.

8. The pitot tube sensing apparatus of claim 1 , wherein the channel is in the shape of a cylinder, and each electrode is in the shape of a cylindrical arc.

9. The pitot tube sensing apparatus of claim 1 , wherein the pitot tube sensing apparatus further comprises a trap, the capacitor is between an opening of the channel and the trap, and the trap is arranged to block foreign objects from reaching the pressure sensor.

10. The pitot tube sensing apparatus of claim 1 , wherein the pitot tube sensing apparatus is further configured to generate an alert upon determining the presence of a foreign object within the channel.

11. The pitot tube sensing apparatus of claim 1 , wherein the pitot tube sensing apparatus is configured to determine a fluid speed based on an output of the pressure sensor.

12. The pitot tube sensing apparatus of claim 1 , wherein the electrodes are positioned in the channel between an opening of the channel and the pressure sensor.

13. The pitot tube sensing apparatus of claim 1 , wherein the pressure sensor is configured to measure a total pressure in the channel; the pitot tube sensing apparatus further comprises a static pressure sensor configured to measure a static pressure; and the pitot tube sensing apparatus is further configured to calculate a fluid speed based on a difference between the total pressure and the static pressure.

14. An aircraft comprising the pitot tube sensing apparatus of claim 1 .

15. An aircraft according to claim 14 , wherein the pitot tube sensing apparatus is configured to determine an air speed of the aircraft based on an output of the pressure sensor.

16. A method of determining the presence or absence of a foreign object within a pitot tube sensing apparatus, wherein the pitot tube sensing apparatus comprises:

a pitot tube comprising a channel with an opening;

a pressure sensor coupled to the channel; and

a capacitor comprising two electrodes on opposing sides of the channel,

the method comprising:

measuring a capacitance between the two electrodes; and

determining the presence or absence of a foreign object within the channel based on the capacitance.

17. The method of claim 16 , wherein determining the presence or absence of a foreign object is based on a comparison of the capacitance to a detection threshold.

18. The method of claim 16 , further comprising calculating a rate of change in the capacitance, wherein the determination of the presence or absence of a foreign object is based on a comparison of the rate of change in the capacitance to a detection threshold.

19. The method of claim 16 , further comprising generating an alert upon determining the presence of a foreign object within the channel.

20. A pitot tube sensing apparatus comprising: a pitot tube comprising a channel; a pressure sensor coupled to the channel; a capacitor comprising two electrodes on opposing sides of the channel; and a system configured to:

measure a capacitance between the two electrodes;

determine the presence or absence of a foreign object within the channel based on the capacitance; and

calculate a rate of change in the capacitance, wherein the determination of the presence or absence of a foreign object is based on a comparison of the rate of change in the capacitance to a detection threshold.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 20, 2023
From: DHANDHANIA, ANMOL
To: AIRBUS (SAS)
Reel/Frame 064000/0517 →
Priority Claims (1)
IN 202211035631 · Jun 21, 2022 · national
Continuity (1)
Related Publication 20230408720A1 · Dec 21, 2023
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