Aircraft wind indicator

• US 6,647,774 B1
• Filed: 06/28/2000
• Issued: 11/18/2003
• Est. Priority Date: 06/28/2000
• Status: Active Grant

• Current Assignee: John S. Youngquist
• Original Assignee: John S. Youngquist
• Inventors: Youngquist, John S.
• Primary Examiner(s): Lefkowitz, Edward
• Assistant Examiner(s): Martir, Lilybett
• Application Number:
  US09/605,631
• Time in Patent Office: 1,238 Days
• Field of Search: 731/700.2, 731/700.1, 340/975, 340/968, 349/58, 701/7, 701/14
• US Class Current: 73/170.02
• CPC Class Codes: G01P 1/08 Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers
• CPC Class Codes: G01P 5/00 Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft application of speed-measuring devices for measuring volume of fluid G01F

Abstract

Wind direction relative to an aircraft, wind speed and left/right wind correction angle data are derived and serially transmitted to an instrument panel indicator which simultaneously displays such data in a graphic visual format. A simple 2-wire interface provides both power and data to the indicator which includes on-board data processing/display driver capability on one side of a PCB with the driven display elements on the other side of the PCB. The entire integrated driver display unit can be made quite small and adhesively mounted in virtually any desired location (e.g., even on a portion of another instrument face) and connected to the power/data source via an almost transparent 2-conductor umbilical connection.

Claims

1. An aircraft wind indicator comprising:

a printed circuit board having first and second surfaces, said first surface being opposed to said second surface;

wind data display elements disposed on said first surface of said printed circuit board; and

wind data processing and display driving circuits disposed on said second surface of said printed circuit board.

2. An aircraft wind indicator as in claim 1 disposed in a housing of about 1.3 inches diameter with an adhesive pad on its back side for affixation to an aircraft instrument panel.

3. An aircraft wind indicator as in claim 2 further comprising a two conductor ribbon cable having a substantially transparent base for simultaneously conducting both power and data to the indicator circuits.

4. An aircraft wind indicator as in claim 1 wherein said display elements are disposed to depict wind speed, wind direction and wind correction angle data.

5. An aircraft wind indicator as in claim 1 wherein said display elements comprise solid state elements.

6. An aircraft wind indicator as in claim 5 wherein said display elements include elements arrayed in:

(i) two concentric circular tracks, and

(ii) a linear track.

7. An aircraft wind indicator as in claim 1 wherein said display elements comprise LCD elements.

8. An aircraft wind indicator as in claim 1 wherein said display elements include both graphic and alpha-numeric digital display elements.

9. An aircraft wind indicator for use on an aircraft, said aircraft wind indicator comprising:

visible digital display elements disposed to display wind speed and wind direction, said visible digital display elements being arranged to form an arcuate bar coded display; and

digital data processing and indicator driving circuits connected to drive said visible digital display elements in accordance with digital data representing wind speed and wind direction when the aircraft is in flight.

10. An aircraft wind indicator as in claim 9 wherein:

said wind speed and direction are displayed by graphical depictions disposed about two respectively associated concentric loci.

11. An aircraft wind indicator as in claim 10 wherein:

said wind correction angle is displayed by graphical depictions disposed to the left and to the right of a reference indicia.

12. An aircraft wind indicator as in claim 9 disposed in a housing of about 1.3 inches diameter with an adhesive pad on its back side for affixation to an aircraft instrument panel.

13. An aircraft wind indicator as in claim 9 further comprising a two conductor cable for simultaneously conducting both power and data to the indicator circuits.

14. An aircraft wind indicator for use on an aircraft, said aircraft wind indicator comprising:

visible digital display elements disposed to display wind speed and wind direction, said visible digital display elements being arranged to form an arcuate bar coded display; and

digital data processing and indicator driving circuits connected to drive said visible digital display elements in accordance with digital data representing wind speed and wind direction when the aircraft is in flight;

wherein said visible digital display elements are also disposed to display a wind correction angle and said digital data processing and indicator driving circuits are also connected to drive said visible digital display elements in accordance with digital data representing a wind correction angle when the aircraft is in flight.

15. An aircraft wind indicator as in claim 14 wherein:

said visible indicators comprise at least one of solid state LED and LCD elements arrayed on one side of a printed circuit board; and

said data processing and indicator driving circuits are disposed on the other side of said printed circuit board.

16. An aircraft wind indicator as in claim 14 wherein:

said wind correction angle is displayed by graphical depictions disposed to the left and to the right of a reference indicia.

17. An aircraft wind indicator as in claim 14 including display elements defining alpha-numeric digits.

18. An aircraft wind indicator comprising:

a housing containing a plurality of digital display elements and driving circuits therefor disposed for selective activation of said elements to represent the speed and direction of wind with respect to a moving airborne aircraft.

19. An aircraft wind indicator as in claim 18 wherein said display elements and driving circuits are configured to also represent a requisite wind correction offset aircraft steering angle for maintaining a predetermined direction of aircraft movement with respect to the ground.

20. An aircraft wind indicator as in claim 19 wherein said display elements are disposed to provide graphic data depiction.

21. An aircraft wind indicator as in claim 19 wherein at least some of said display elements are disposed to provide a display of numeric digits.

22. An aircraft wind indicator as in claim 19 wherein said elements are arrayed:

(i) in two concentric circular tracks to respectively depict the magnitudes of wind speed and direction; and

(ii) in a third track to depict a left or right wind correction angle.

23. An aircraft wind indicator as in claim 22 wherein said third track is a linear track with elements extending to the left and right of a reference point for depicting the wind correction angle direction and magnitude.

24. An aircraft wind indicator as in claim 19 wherein:

said display elements include at least one of LED and LCD elements mounted on one side of a printed circuit board; and

said driving circuits include solid state data processing and display element driver circuits mounted on the opposite side of said circuit board.

25. An aircraft wind indicator as in claim 24 wherein said display elements are directed toward a front side of said housing and, when activated, viewable through a substrate imprinted with graphical symbols aligned with said display elements.

26. An aircraft wind indicator as in claim 25 wherein a back side of said housing includes a pad of adhesive for affixing it to an aircraft instrument panel.

27. An aircraft wind indicator as in claim 18 further comprising a two conductor cable for simultaneously conducting both power and data to the driving circuits.

28. An aircraft wind indicator for use on an aircraft, said aircraft wind indicator comprising:

a data input port,

a first array of controllable discrete display elements arranged to graphically depict wind direction data;

a second array of controllable discrete display elements arranged to graphically depict wind speed data when the aircraft is airborne;

a third array of controllable discrete display elements arranged to graphically depict wind correction angle data; and

data processing and display element driving circuits connected between said data input port and said arrays.

29. An aircraft wind indicator as in claim 28 wherein said data input port comprises a pair of electrical conductors supplying power as well as wind-related data to said data processing and light source driving circuits.

30. An aircraft wind indicator as in claim 28 wherein said discrete display elements are at least one of LED and LCD elements.

31. An aircraft wind indicator as in claim 28 wherein said discrete display elements include elements arranged to display numeric digits.

32. An aircraft wind indicator as in claim 28 wherein:

said data processing and display element driving circuits comprise a micro-processor and other drive circuit components disposed on one side of a printed circuit board; and

said arrays of display elements are disposed on an opposite side of said printed circuit board.

33. An aircraft wind indicator as in claim 28 wherein said first array of display elements is disposed along a circular locus.

34. An aircraft wind indicator as in claim 28 wherein said second array of display elements is disposed along a circular locus.

35. An aircraft wind indicator as in claim 28 wherein said first and second arrays of display elements are respectively disposed along concentric circular loci.

36. An aircraft wind indicator as in claim 35 wherein said first array of display elements is disposed along a circular locus that is of greater diameter than that of the second array.

37. An aircraft wind indicator as in claim 36 wherein said third array of display elements is disposed along a linear locus.

38. An aircraft wind indicator as in claim 37 wherein said third array of display elements includes a first sub-array arranged to depict a right wind correction angle and a second sub-array arranged to depict a left wind correction angle.

39. An aircraft wind indicator as in claim 28 wherein said third array of display elements is disposed along a linear locus.

40. An aircraft wind indicator as in claim 39 wherein said third array of display elements includes a first sub-array arranged to depict a right wind correction angle and a second sub-array arranged to depict a left wind correction angle.

41. An aircraft wind indicator as in claim 28 wherein said data input port comprises a two conductor ribbon cable that is substantially invisible to the human eye at normal viewing conditions and at a distance of approximately two feet.

42. An aircraft wind indicator as in claim 28 wherein said data input port also comprises the power supply for said data processing and display element driving circuits which are configured to detect short power interruptions of at least two different durations as input digital data.

43. An aircraft wind indicator as in claim 28 wherein said arrays and said data processing and display element driving circuits are all mounted on a single common printed circuit board.

44. An aircraft wind indicator as in claim 43 wherein said printed circuit board is disposed within a cylindrical housing having a see-through side for viewing said arrays.

45. An aircraft wind indicator as in claim 43 wherein said printed circuit board is disposed within a housing having one see-through side for viewing the arrays and an opposite mounting side adapted for affixation to an aircraft instrument panel.

46. A method for displaying wind data in the cockpit of an aircraft, said method comprising:

generating digital wind data representing the direction and magnitude of wind, being encountered by the aircraft when the aircraft is airborne, and correction angle data;

periodically sending said generated digital wind data to a visual indicator in the aircraft cockpit; and

receiving and processing said digital data at the indicator with a micro-processor to drive plural arrays of display elements at the indicator which thereby simultaneously provide a visual depiction of said wind data.

47. A method as in claim 46 wherein:

wind direction is depicted by selectively activating display elements arrayed in a first circular ring,

wind magnitude is depicted by selectively activating display elements arrayed in a second circular ring; and

said wind correction angle is depicted by selectively activating display elements arrayed in a line.

48. An aircraft wind indicator for use on an aircraft, said aircraft wind indicator comprising:

visible display elements disposed to display a wind correction angle; and

data processing and indicator driving circuits connected to drive said visible display elements in accordance with data representing a wind correction angle when the aircraft is in flight.

49. An aircraft wind indicator as claimed in claim 48, said visible display elements being digital for digitally displaying the wind correction angle.

50. An aircraft wind indicator as claimed in claim 48, said visible display elements also being disposed to display wind speed and wind direction.

51. An aircraft wind indicator as claimed in claim 50, said visible display elements being arranged to form an arcuate bar coded display.