Ducted fan air data system

• US 7,841,563 B2
• Filed: 03/13/2007
• Issued: 11/30/2010
• Est. Priority Date: 03/27/2006
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Fleming, Jonathan Lee, Goossen, Emray R.
• Primary Examiner(s): Dinh; Tien
• Assistant Examiner(s): Green; Richard R
• Application Number:
  US11/685,532
• Publication Number:
  US 20070221790A1
• Time in Patent Office: 1,358 Days
• Field of Search: 244/76.B, 244/73.R, 244/62, 244/1.R, 244/17.13, 244/194, 244/195, 244/53.B, 244/73.B, 244/73.C, 244/12.2, 244/23.C, 244/23.R, 244/23.A, 244/7.B, 244/34.A, 244/12.1, 244/175, 731/700.2, 731/701.4, 731/80, 731/700.8, 731/700.9, 731/79, 738/616.6, 731/83, 731/78.H, 731/700.7, 735/02, 415/118, 602/261, 137/152.2, 137/15.1, D12/330
• US Class Current: 244/175
• CPC Class Codes: G01P 13/025 indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
• CPC Class Codes: G01P 5/14 by measuring differences of pressure in the fluid
• CPC Class Codes: G01P 5/16 using Pitot tubes , e.g. Machmeter

Abstract

An air data system and method for a ducted fan air-vehicle is described. The air data system includes a plurality of air pressure sensors placed around a lip of an air duct of the ducted fan air-vehicle. The air data system calculates the speed and direction of airflow surrounding the ducted fan air-vehicle based on pressure data measured across the lip of the air duct. Additionally, the air data system may estimate forces generated by airflow surrounding the air-vehicle.

Claims

1. A system for an air-vehicle, the system comprising:

an air duct comprising a lip;

a fan located within the air duct;

a plurality of air pressure sensors placed around and within the lip of the air duct operable to measure air pressure data; and

a processor that receives the air pressure data from the plurality of air pressure sensors and calculates speed and direction of airflow surrounding the air-vehicle based on a plurality of pressure differentials across the lip of the air duct determined from the air pressure data measured by the plurality of air pressure sensors.

2. The system of claim 1, wherein the plurality of air pressure sensors are flush mounted sensors.

3. The system of claim 2, wherein the flush mounted sensors are mounted at a high velocity, low pressure region at the lip of the air duct.

4. The system of claim 1, wherein the plurality of air pressure sensors placed around the lip of the air duct are mounted within a duct lip port.

5. The system of claim 1, wherein the plurality of air pressure sensors includes at least one pair of pressure sensors placed around the lip substantially 180 degrees apart, wherein the processor receives pressure inputs from each of the pressure sensors.

6. The system of claim 1, wherein the processor is operable to estimate the air-vehicle velocity based on the speed and direction of the airflow surrounding the air-vehicle.

7. The system of claim 1, wherein the processor is operable to estimate forces acting on the air-vehicle generated by airflow surrounding the air-vehicle.

8. The system of claim 7, further comprising an avionics system that receives an estimate of at least one force of the forces acting on the air-vehicle and adjusts an attitude of the air vehicle based on the estimate.

9. The system of claim 1, further comprising a plurality of vanes placed at an exit section of the air duct.

10. The system of claim 1, wherein each air pressure sensor of the plurality of air pressure sensors is mounted to the lip at a respective position internal to the air duct.

11. A method of measuring air data for a ducted fan air-vehicle, the method comprising:

placing a plurality of air pressure sensors within a lip of an air duct of the air-vehicle such that the plurality of air pressure sensors includes at least one pair of air pressure sensors comprising a first air pressure sensor that measures pressure at a first point on the lip of the air duct and a second air pressure sensor that measures pressure at a second point on the lip of the air duct substantially 180 degrees away from the first point; and

connecting a processor to the plurality of air pressure sensors, wherein the processor calculates speed and direction of airflow surrounding the air-vehicle based on a differential between pressure inputs received from each of the first and second air pressure sensors of the at least one pair of air pressure sensors.

12. The method of claim 11, wherein placing a plurality of air pressure sensors on the lip of the air duct of the air-vehicle includes flush mounting the plurality of air pressure sensors to the lip of the air duct.

13. The method of claim 12, wherein flush mounting the plurality of air pressure sensors to the lip of the air duct includes mounting the plurality of air pressure sensors at a high velocity low pressure region at the lip of the air duct of the air-vehicle.

14. The method of claim 11, wherein the processor is operable to estimate forces acting on the air-vehicle generated by the airflow surrounding the air-vehicle.

15. The method of claim 11, wherein the processor is operable to estimate air-vehicle velocity based on the speed and direction of airflow surrounding the air-vehicle.

16. The method of claim 11, wherein the processor operable to calculate speed and direction of airflow calculates direction of airflow by:

calculating a plurality of pressure differentials between the first point on the lip of the air duct and the second point on the lip of the air duct substantially 180 degrees apart from the first point;

calculating a plurality of vectors from the plurality of pressure differentials;

summing the plurality of vectors; and

calculating the direction of the airflow based on the sum of the plurality of vectors.

17. The method of claim 11, wherein a fan is located within the air duct and placing the plurality of air pressure sensors within the lip of the air duct comprises placing the plurality of air pressure sensors within the lip of a leading edge of the air duct.

18. A method for calculating speed and direction of airflow surrounding a ducted fan air-vehicle, the method comprising:

obtaining a plurality of pressure measurements within a lip of an air duct of the air-vehicle via a plurality of air pressure sensors;

compensating the plurality of pressure measurements for vehicle attitude;

determining a plurality of pressure differentials across the lip of the air duct via a plurality of pairs of the air pressure sensors, wherein at least one pair of air pressure sensors comprises a first air pressure sensor that measures pressure at a first point on the lip of the air duct and a second air pressure sensor that measures pressure at a second point on the lip of the air duct substantially 180 degrees away from the first point;

compensating the plurality of pressure differentials for a fan speed of the fan of the air-vehicle and air density to arrive at a plurality of compensated pressure differentials;

applying a linear velocity curve lit for the compensated pressure differentials;

generating a plurality of individual velocity vectors across the lip of the air duct based on the linear velocity curve fit for the compensated pressure differentials; and

generating a total velocity vector of the airflow based on the plurality of individual velocity vectors across the lip of the air duct.

19. The method of claim 18, wherein compensating the plurality of pressure measurements for vehicle attitude includes compensating for the ducted fan air-vehicle pitch attitude.

20. The method of claim 18, wherein compensating the plurality of pressure measurements for vehicle attitude includes compensating for the ducted fan air-vehicle roll attitude.