WATER RESISTANT AIRCRAFT PITOT DEVICE

• US 20140290383A1
• Filed: 08/16/2012
• Published: 10/02/2014
• Est. Priority Date: 08/19/2011
• Status: Active Grant

• Current Assignee: Aerovironment
• Original Assignee: Aerovironment
• Inventors: Ashton, Charles F.
• Granted Patent: US 9,080,903 B2
• Time in Patent Office: Days
• US Class Current: 73/861.65
• CPC Class Codes: G01F 1/46 Pitot tubes
• CPC Class Codes: G01P 5/165 Arrangements or constructions of Pitot tubes
• CPC Class Codes: Y10T 29/49764 with testing or indicating

Abstract

A pitot tube system having a pitot tube containing a porous hydrophobic fabric that blocks water and contaminants from reaching a pressure sensor. The distance in the pitot tube between the fabric and a front orifice of the tube is less than 2.4 times the height of the orifice, and preferably less than or equal to 0.38 times the height. The section of the tube through which the fabric extends defines an opening characterized by a minimum dimension greater than 0.15 inches, and preferably being at least 0.21 inches. The tube is a removable structure that attaches to a mount that forms a passage for communicating the pressure in the tube. That passage contains a second porous hydrophobic fabric that also blocks water and contaminants from reaching a pressure sensor.

Claims

1. A pitot device for use in an airflow, comprising:

a pitot housing forming a cavity having a housing external orifice characterized by a housing external-orifice height;

an air-permeable fabric extending across a section of the cavity and defining an internal chamber; and

a pressure sensor configured to sense information regarding the pressure within the internal chamber;

wherein the distance within the cavity between the air-permeable fabric and the housing external orifice is less than 2.4 times the housing external-orifice height.

2. The pitot device of claim 1, and further comprising:

a static port; and

an airspeed calculation system configured to provide an airspeed indication based on the gather information when the external orifice faces into the airflow and the static port is normal to the airflow;

wherein the pressure sensor is part of a pressure measurement system configured to gather information indicative of the difference between the pressure within the internal chamber and the pressure at the static port.

3. An aircraft control system, comprising an autopilot and the pitot device of claim 2, wherein the autopilot is configured to provide flight control information based on the airspeed indication provided by the airspeed calculation system.

4. The pitot device of claim 1, wherein the distance within the cavity between the air-permeable fabric and the housing external orifice is no more than 0.38 times the housing external-orifice height.

5. The pitot device of claim 1, wherein the distance within the cavity between the air-permeable fabric and the housing external orifice is greater than 0.00 times the housing external-orifice height.

6. The pitot device of claim 1, wherein the section of the cavity through which the fabric extends defines an opening to the internal chamber, and wherein the opening to the internal chamber is characterized by a minimum opening-size dimension greater than 0.15 inches.

7. The pitot device of claim 6, wherein the minimum opening-size dimension is at least 0.21 inches.

8. The pitot device of claim 7, wherein the minimum opening-size dimension is at least 0.25 inches.

9. The pitot device of claim 1, and further comprising a second air-permeable fabric covering the static port.

10. The pitot device of claim 9, wherein the pressure measurement system includes a single pressure sensor configured to measure the pressure differential between the pressure in the internal chamber and the pressure at the static port.

11. The pitot device of claim 1, wherein the housing does not form a drain hole.

12. The pitot device of claim 1, wherein the air-permeable fabric is hydrophobic.

13. The pitot device of claim 1, and further comprising a second air-permeable fabric covering the static port, wherein:

the pressure measurement system includes a single pressure sensor configured to measure the pressure differential between the pressure in the internal chamber and the pressure at the static port;

the distance within the cavity between the air-permeable fabric and the housing external orifice is approximately 0.38 times the housing external-orifice height; and

the section of the cavity through which the fabric extends defines an opening to the internal chamber, and the opening to the internal chamber is characterized by a minimum opening-size dimension greater than 0.15 inches.

14. The pitot device of claim 13, wherein the minimum opening-size dimension is at least 0.21 inches.

15. The pitot device of claim 13, wherein the minimum opening-size dimension is at least 0.25 inches.

16. The pitot device of claim 13, wherein the housing does not form a drain hole.

17. The pitot device of claim 13, wherein the air-permeable fabric is hydrophobic.

18. A pitot device for use in an airflow, comprising:

a housing forming a cavity having a housing external orifice characterized by a housing external-orifice height;

an air-permeable fabric extending across a section of the cavity and defining an internal chamber;

a static port;

a pressure measurement system configured to gather information indicative of the difference between the pressure within the internal chamber and the pressure at the static port, the pressure measurement system including a pressure sensor configured to sense information regarding the pressure within the internal chamber; and

an airspeed calculation system configured to provide an airspeed indication based on the gather information when the external orifice faces into the airflow and the static port is normal to the airflow;

wherein the section of the cavity through which the fabric extends defines an opening to the internal chamber, and wherein the opening to the internal chamber is characterized by a minimum opening-size dimension greater than 0.15 inches.

19. The pitot device of claim 18, wherein the minimum opening-size dimension is at least 0.21 inches.

20. The pitot device of claim 19, wherein the minimum opening-size dimension is at least 0.25 inches.

21. The pitot device of claim 19, wherein the pressure measurement system includes a single pressure sensor configured to measure the pressure differential between the pressure in the internal chamber and the pressure at the static port.

22. The pitot device of claim 18, and further comprising a second air-permeable fabric covering the static port.

23. The pitot device of claim 18, wherein the housing does not form a drain hole.

24. The pitot device of claim 18, wherein the air-permeable fabric is hydrophobic.

25. A method of designing a pitot device for use in an airflow over a range of airspeeds, the pitot device including a housing forming a cavity having a housing external orifice characterized by a housing external-orifice height, an air-permeable fabric configured to extend across a section of the cavity and define an internal chamber, a static port structure, a pressure measurement system configured to gather information indicative of the difference between the pressure within the internal chamber and the pressure at the static port, the pressure measurement system including a pressure sensor configured to sense information regarding the pressure within the internal chamber over the range of airspeeds, and an airspeed calculation system configured to provide an airspeed indication based on the gather information when the external orifice faces into the airflow and the static port is normal to the airflow, comprising the steps of:

(a) configuring the housing with a tubular portion extending from the air-permeable fabric to the housing external orifice;

(b) moisture testing the housing over the range of airspeeds to see if the tubing is subject to failure from flooding; and

(c) if tubing is subject to failure from flooding, then reducing the ratio of the distance within the cavity between the air-permeable fabric and the housing external orifice, over the housing external-orifice height, and repeating steps (a) to (c).