Apparatus and method for deicing aircraft

• US 6,209,823 B1
• Filed: 09/09/1999
• Issued: 04/03/2001
• 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, J. Woodrow
• Application Number:
  US09/392,701
• Time in Patent Office: 572 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 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 compressor having an air outlet. A deicer air jet nozzle is located at the free end of the boom and operatively coupled to the air outlet of the compressor for receiving air and discharging the air for a deicer application.

Claims

1. An apparatus for deicing comprising:

a vehicle frame;

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

a compressor supported by the boom and having an air outlet; and

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

2. An apparatus according to claim 1, and further comprising a hydraulic motor having an output connected to said compressor for driving said compressor, and 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, including a vehicle engine supported by said vehicle frame 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 2, and further comprising a drive gear unit operatively connected between said compressor and said hydraulic motor for stepping up the revolutions per minute of said 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 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 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 pump forces air through said deicer air jet nozzle at about 80 to about 100 pounds per minute.

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

10. An apparatus for deicing 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 compressor having an air outlet; and

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

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

12. An apparatus according to claim 10, and further comprising a motor having an output, 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, and further comprising a vehicle 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.

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

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

compressing air within a compressor supported by a vehicle boom; and

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

19. A method according to claim 18, wherein the air is discharged from the deicer air jet nozzle at about 10 to about 13 pounds per square inch.

20. A method according to claim 18, wherein the air is discharged through air jet nozzle that defines an axisymmetric contour having a converging portion.

21. A method according to claim 18, and further comprising the step of hydraulically driving a motor coupled to the compressor, wherein the motor comprises a hydraulic motor.

22. A method according to claim 21, and further comprising the step of driving the hydraulic motor from a hydraulic pump located on a vehicle frame.

23. A method according to claim 22, and further comprising the step of operating the hydraulic pump from directly from the engine used for driving the vehicle.

24. A method according to claim 21, and further comprising the step of stepping up the revolutions per minute of the compressor relative to the output of the motor by a gear drive coupled between the centrifugal compressor and the motor.

25. A method according to claim 18, and further comprising the step of discharging the air from the nozzle at above 15 degrees above ambient temperature.

28. A method according to claim 18, and further comprising the step of forcing air outward from the deicer air jet nozzle at about 100 pounds per minute.