Apparatus and method for deicing aircraft

• US 6,029,934 A
• Filed: 09/09/1999
• Issued: 02/29/2000
• Est. Priority Date: 08/05/1998
• Status: Expired due to Fees

• Current Assignee: FMC Corporation
• Original Assignee: FMC Corporation
• Inventors: Foster, Clifton L.
• Primary Examiner(s): ELDRED, JOHN W
• Application Number:
  US09/392,524
• Time in Patent Office: 173 Days
• Field of Search: 244/134 R, 244/134 C
• US Class Current: 244/134.00C
• CPC Class Codes: B60S 3/002 Vehicle drying apparatus
• CPC Class Codes: B64F 5/20 Ground installations for de-icing aircraft
• CPC Class Codes: B64F 5/23 by liquid application; Spraying installations therefor, e.g. fitted on vehicles

Abstract

An apparatus for deicing aircraft includes a vehicle frame, such as part of a truck, and a boom having one end mounted on the vehicle frame and a free end. A compressor unit is supported by the boom and includes a motor having an output and a centrifugal compressor operatively connected to the motor output. A deicer air jet nozzle is located at the boom and operatively coupled to the air outlet of the centrifugal compressor for receiving air and discharging the air for a deicer application.

Claims

1. An apparatus for deicing aircraft comprising:

a vehicle frame;

a boom having an end mounted on the vehicle frame and a free end;

a compressor unit supported by the boom, said compressor unit comprising;

a hydraulic motor having an output, and

a centrifugal compressor operatively connected to the hydraulic motor output and having an impeller and an air outlet; and

a deicer air jet nozzle located at the boom and operatively coupled to the air outlet of the centrifugal compressor for receiving air and discharging the air for a deicer application.

2. An apparatus according to claim 1, and further comprising a hydraulic pump mounted on the vehicle frame and hydraulic feed lines extending from said hydraulic pump along said boom to said hydraulic motor for supplying hydraulic fluid under pressure to said hydraulic motor.

3. An apparatus according to claim 2, wherein said vehicle frame includes a vehicle engine, and a transmission driven from said vehicle engine and interconnecting said hydraulic pump for supplying power to said hydraulic pump.

4. An apparatus according to claim 1, and further comprising a drive gear unit operatively connected between said centrifugal compressor and said hydraulic motor for stepping up the revolutions per minute of said centrifugal compressor relative to the output of said hydraulic motor.

5. An apparatus according to claim 4, wherein said drive gear unit further comprises an input spur gear driven from said hydraulic motor and an output spur gear driving said centrifugal compressor.

6. An apparatus according to claim 5, wherein input spur gear and output spur gear defines about a 2:

1 to about 4;

1 gear ratio.

7. An apparatus according to claim 1, wherein said deicer air jet nozzle defines an axisymmetric contour having a converging portion.

8. An apparatus according to claim 1, and further comprising a fluid nozzle mounted on said deicer air jet nozzle, a source of deicing fluid, a supply tube interconnecting said source of deicing fluid and fluid nozzle, and a centrifugal fluid pump for pumping deicing fluid from the source of deicing fluid and through the supply tube and fluid nozzle.

9. An apparatus according to claim 1, wherein said centrifugal pump forces air through said deicer air jet nozzle at about 80 to about 100 pounds per minute.

35. An apparatus according to claim 1, wherein said deicer air jet nozzle is located at the free end of the boom.

36. An apparatus according to claim 1, wherein said deicer air jet nozzle is supported by the boom.

10. An apparatus for deicing aircraft comprising:

a vehicle frame;

a boom having an end mounted on the vehicle frame and a free end;

a compressor unit supported by the boom, said compressor unit comprising;

a motor having an output, and

a centrifugal compressor operatively connected to the motor output and having an impeller and an air outlet; and

a deicer air jet nozzle located at the boom and operatively coupled to the air outlet of the centrifugal compressor for receiving air and discharging the air for a deicer application.

11. An apparatus according to claim 10, wherein said centrifugal compressor forces air through said deicer air jet nozzle at about 80 to 100 pounds per minute.

12. An apparatus according to claim 10, wherein said motor comprises a hydraulic motor, and further including a hydraulic pump and hydraulic feed lines extending from said hydraulic pump to said hydraulic motor.

13. An apparatus according to claim 12, wherein said hydraulic pump is mounted on said vehicle frame, and said hydraulic feed lines extend from said hydraulic pump along said boom to said hydraulic motor for supplying hydraulic fluid under pressure to said hydraulic motor.

14. An apparatus according to claim 13, and further comprising a hydraulic pump mounted on the vehicle frame and hydraulic feed lines extending from said hydraulic pump along said boom to said hydraulic motor for supplying hydraulic fluid under pressure to said hydraulic pump.

15. An apparatus according to claim 14, including an engine mounted on said vehicle frame and a transmission driven from said vehicle engine and interconnecting said hydraulic pump for supplying power to said hydraulic pump.

16. An apparatus according to claim 10, wherein said deicer air jet nozzle defines an axisymmetric contour having a converging portion.

17. An apparatus according to claim 10, and further comprising a fluid nozzle mounted on said deicer air jet nozzle, a source of deicing fluid, a supply tube interconnecting said source of deicing fluid and fluid nozzle, and a centrifugal fluid pump for pumping deicing fluid from the source of deicing fluid and through the supply tube and fluid nozzle.

37. An apparatus according to claim 10, wherein said deicer air jet nozzle is located at the free end of the boom.

38. An apparatus according to claim 10, wherein said deicer air jet nozzle is supported by the boom.

18. An apparatus for deicing aircraft comprising:

a vehicle frame;

a boom having an end mounted on the vehicle frame and a free end;

a compressor unit supported by the boom, said compressor unit comprising;

a motor having an output,

an input spur gear connected to the motor output,

an output spur gear meshing with the input spur gear;

a centrifugal compressor operatively connected to the output spur gear and having an impeller and an air outlet; and

a deicer air jet nozzle located at the boom and operatively coupled to the air outlet of the centrifugal compressor for receiving air and discharging the air for a deicer application.

19. An apparatus according to claim 18, wherein said centrifugal compressor forces air through said deicer air jet nozzle at about 100 pounds per minute.

20. An apparatus according to claim 18, wherein said motor comprises a hydraulic motor, and further including a hydraulic pump and hydraulic feed lines extending from said hydraulic pump to said hydraulic motor.

21. An apparatus according to claim 20, wherein said hydraulic pump is mounted on said vehicle frame, and said hydraulic feed lines extend from said hydraulic pump along said boom to said hydraulic motor for supplying hydraulic fluid under pressure to said hydraulic motor.

22. An apparatus according to claim 21, wherein said vehicle frame includes a vehicle engine, and a transmission driven from said vehicle engine and interconnecting said hydraulic pump for supplying power to said hydraulic pump.

23. An apparatus according to claim 18, wherein said deicer air jet nozzle defines an axisymmetric contour having a converging portion.

24. An apparatus according to claim 18, and further comprising a fluid nozzle mounted on said deicer air jet nozzle, a source of deicing fluid, a supply tube interconnecting said source of deicing fluid and fluid nozzle, and a centrifugal fluid pump for pumping deicing fluid from the source of deicing fluid and through the supply tube and fluid nozzle.

39. An apparatus according to claim 18, wherein said deicer air jet nozzle is located at the free end of the boom.

40. An apparatus according to claim 18, wherein said deicer air jet nozzle is supported by the boom.

25. A deicer assembly comprising:

a compressor mounting frame;

a mounting mechanism secured to the frame for attaching the compressor mounting frame to a boom of a vehicle;

a centrifugal compressor mounted on the compressor mounting frame, said centrifugal compressor having an input shaft, an impeller and an air outlet;

a drive gear unit mounted on the centrifugal compressor, and having an input spur gear and output spur gear connected to the input shaft of the centrifugal compressor; and

a hydraulic motor mounted on the drive gear unit and having an output connected to the input spur gear.

26. An apparatus according to claim 25, wherein said drive gear unit defines about a 2:

1 to about 4;

1 gear ratio.

27. A method for deicing aircraft comprising the steps of:

compressing air within a centrifugal compressor supported by a vehicle boom by driving a motor coupled to the centrifugal compressor; and

discharging the air from a deicer air jet nozzle located at the vehicle boom such that air is forced outward from the deicer air jet nozzle.

28. A method according to claim 27, wherein the air is discharged from the deicer air jet nozzle at about 10 to about 13 pounds per square inch.

29. A method according to claim 27, wherein the air is discharged through air jet nozzle that defines an axisymmetric contour having a converging portion.

30. A method according to claim 27, and further comprising the step of hydraulically driving the motor, wherein the motor comprises a hydraulic motor.

31. A method according to claim 30, and further comprising the step of driving the hydraulic motor from a hydraulic pump located on a vehicle frame.

32. A method according to claim 31, and further comprising the step of operating the hydraulic pump from directly from the engine used for driving the vehicle.

33. A method according to claim 30, and further comprising the step of stepping up the revolutions per minute of the centrifugal compressor relative to the output of the motor by a gear drive coupled between the centrifugal compressor and the motor.

34. A method according to claim 27, and further comprising the step of discharging the air from the nozzle at above 15 degrees above ambient temperature.

41. A method according to claim 27, and further comprising the step of discharging the air from the deicer air jet nozzle at about 100 pounds per minute.

42. A method according to claim 27, wherein the deicer air jet nozzle is located at the free end of the boom.

43. A method according to claim 27, wherein the deicer air jet nozzle is supported by the boom.