Hybrid deicing system and method of operation

• US 6,293,498 B1
• Filed: 02/18/2000
• Issued: 09/25/2001
• Est. Priority Date: 06/28/1996
• Status: Expired due to Term

• Current Assignee: Premier Engineering & Manufacturing Inc (Textron Inc)
• Original Assignee: Honeywell International Inc.
• Inventors: Stanko, John, Pearson, Lowell
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): Steele, George L.
• Application Number:
  US09/507,404
• Time in Patent Office: 585 Days
• Field of Search: 244/134.R, 244/134.C, 239/423, 134/102.2
• US Class Current: 244/134.00R
• 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

This invention overcomes the disadvantage of the prior systems and produces a high velocity specially formed and constituted pressure aerodynamic stream system for efficiently and effectively removing ice from an aircraft. The specially formed stream system includes a stream within a stream, wherein a deicing fluid such a glycol is entrained within and encased by a surrounding jacket of entraining fluid such as air. This deicing is now known as coaxial stream/stream within a stream deicing. The special nozzle allows the stream to maintain fluid separation over its flight path so that aircraft contact is made by to be known as coaxial stream/stream within a stream deicing. The coaxial stream/stream within a stream deicing is further enhanced by pressurizing the stream to deliver the stream as a high pressure, high velocity stream to improve the aerodynamic sweeping action of the airstream.

Claims

1. An apparatus comprising:

a deicing fluid nozzle that is configured to have exit therefrom a deicing fluid stream; and

an air nozzle that is configured to have exit therefrom an airstream,

wherein said deicing fluid nozzle and said air nozzle are arranged so that the airstream surrounds the deicing fluid stream.

2. An apparatus according to claim 1, wherein said deicing fluid nozzle is disposed within said air nozzle.

3. An apparatus according to claim 2, wherein said air nozzle has an annular orifice through which said airstream exits.

4. An apparatus according to claim 1, wherein the deicing fluid stream comprises glycol.

5. An apparatus according to claim 4, wherein the glycol comprises ethylene glycol.

6. An apparatus according to claim 1, wherein said deicing fluid nozzle comprises a jetting orifice that is configured to produce a conical-shaped jet of the deicing fluid.

7. An apparatus according to claim 2, further comprising another deicing fluid nozzle disposed within said air nozzle and in which said deicing fluid nozzle is disposed, said another deicing fluid nozzle having an annular array of orifices from which a stream of deicing fluid exits.

8. An apparatus comprising:

a nozzle assembly having a central deicing fluid orifice, an annular array of deicing fluid orifices disposed around said central deicing fluid orifice, and an annular air orifice disposed around said array of deicing fluid orifices;

deicing fluid providing means for providing deicing fluid to said central deicing fluid orifice or said annular array of deicing fluid orifices; and

air providing means for providing air to said annular air orifice.

9. An apparatus according to claim 8, wherein said deicing fluid providing means comprises switching means for switching between providing deicing fluid to said central deicing fluid orifice and said annular array of deicing fluid orifices in accordance with a selection by an operator.

10. An apparatus according to claim 8, wherein said apparatus is configured so that deicing fluid exits at a lower pressure and higher flow rate from said annular array of deicing fluid orifices and at a higher pressure and lower flow rate from said central deicing fluid orifice.

11. An apparatus according to claim 8, wherein a deicing fluid stream exiting from said central deicing fluid orifice or said annular array of deicing fluid orifices is a stream within a stream with respect to an air stream exiting from said annular air orifice.

12. An apparatus according to claim 8, wherein a deicing fluid stream exiting from said central deicing fluid orifice or said annular array of deicing fluid orifices is substantially independent from and radially encased within an air stream exiting from said annular air orifice.

13. An apparatus comprising:

a first passage that provides air;

a second passage disposed within said first passage that provides deicing fluid;

a nozzle assembly coupled with said first and second passages that is configured to have exit therefrom a stream of the deicing fluid encased within a stream of the air.

14. An apparatus comprising:

an air passage that provides air;

a deicing fluid passage coaxially disposed within said air passage that provides deicing fluid;

an air nozzle coupled to said air passage that is configured to have exit therefrom a stream of the air; and

a deicing fluid nozzle coupled to said deicing fluid passage and disposed within said air nozzle that is configured to have exit therefrom a stream of the deicing fluid.

15. An apparatus comprising:

deicing fluid stream and air stream generating means for generating a central stream of deicing fluid within an outer stream of air; and

means for directing the deicing fluid and air streams to an aircraft for deicing the aircraft.

16. A method comprising the steps of:

providing an airstream surrounding a stream of deicing fluid; and

directing the airstream and deicing fluid stream onto an aircraft to deice the aircraft.

17. A deicer vehicle comprising:

a vehicle having a fluid pump and an air compressor;

a deicing fluid nozzle that is configured to have exit therefrom a deicing fluid stream, wherein said fluid pump provides deicing fluid for the deicing fluid stream; and

an air nozzle that is configured to have exit therefrom an airstream, wherein said air compressor provides air for the airstream,

wherein said deicing fluid nozzle and said air nozzle are arranged so that the airstream surrounds the deicing fluid stream.

18. An apparatus according to claim 17, wherein said deicing fluid nozzle is disposed within said air nozzle.

19. An apparatus according to claim 18, wherein said air nozzle has an annular orifice through which said airstream exits.

20. An apparatus according to claim 17, wherein the deicing fluid stream comprises glycol.

21. An apparatus according to claim 20, wherein the glycol comprises ethylene glycol.

22. An apparatus according to claim 17, wherein said deicing fluid nozzle comprises a jetting orifice that is configured to produce a conical-shaped jet of the deicing fluid.

23. An apparatus according to claim 18, further comprising another deicing fluid nozzle disposed within said air nozzle and in which said deicing fluid nozzle is disposed, said another deicing fluid nozzle having an annular array of orifices from which a stream of deicing fluid exits.

24. A deicer vehicle comprising:

a vehicle having a fluid pump and an air compressor;

a first passage connected to said air compressor that provides air from said air compressor;

a second passage disposed within said first passage and connected to said fluid pump that provides deicing fluid from said fluid pump; and

a nozzle assembly coupled with said first and second passages that is configured to have exit therefrom a stream of the deicing fluid encased within a stream of the air.

25. A deicer vehicle comprising:

a vehicle having a fluid pump and an air compressor;

deicing fluid stream and air stream generating means for generating a central stream of deicing fluid within an outer stream of air, wherein said fluid pump provides deicing fluid for the stream of deicing fluid and said air compressor provides air for the stream of air; and

means for directing the deicing fluid and air streams to an aircraft for deicing the aircraft.