Deicing system

• US 4,191,348 A
• Filed: 11/10/1977
• Issued: 03/04/1980
• Est. Priority Date: 11/10/1977
• Status: Expired due to Term

• Current Assignee: Holwerda-Huizenga Company
• Original Assignee: Holwerda-Huizenga Company
• Inventors: Holwerda, Sidney J.
• Primary Examiner(s): Michalsky, Gerald A.
• Application Number:
  US05/850,229
• Time in Patent Office: 845 Days
• Field of Search: 126/271.1, 134/100, 134/101, 134/105, 134/108, 134/123, 134/172, 137/334, 137/340, 137/341, 137/351, 137/360, 137/563, 137/564, 239/124, 239/135, 239/165, 239/197, 239/199, 244/134 C
• US Class Current: 244/134.00C
• 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
• CPC Class Codes: Y10T 137/6579 Circulating fluid in heat exchange relationship
• CPC Class Codes: Y10T 137/6606 With electric heating element
• CPC Class Codes: Y10T 137/6881 Automotive
• CPC Class Codes: Y10T 137/698 Wall
• CPC Class Codes: Y10T 137/85954 Closed circulating system

Abstract

A centralized deicing system includes, in one embodiment, a large fixed location supply tank of deicing fluid which is heated and supplied to a plurality of terminal boxes located at several aircraft loading ramps. The system includes a recirculation loop for preheating the conduits for the deicing fluid by circulating heated deicer fluid through them before application to an aircraft. Each terminal box includes a coupler for receiving ends of a hose employed on a movable vehicle used for deicing an aircraft to also preheat the hose. In one embodiment of the invention, separate tanks of water and glycol are provided, and the terminal box includes a mixing valve which can be remotely controlled by an operator for blending the heated water and glycol in the desired proportion depending on weather conditions.

Claims

1. A method for deicing aircraft comprising:

providing a central source of deicing fluid;

providing means for and heating said deicing fluid;

providing a plurality of distribution terminals positioned at locations remote from said central source for providing heated deicing fluid thereat, and providing each of said terminals with means for coupling deicing fluid applicating hose means thereto;

coupling each of said terminals to said central source through conduit means;

providing means for circulating heated deicing fluid through said conduits and terminals for preheating said conduits;

providing fluid applicating hose means, coupling said hose means to any of said terminals and applying deicing fluid to an airplane located at said terminal.

2. The method as defined in claim 1 wherein said conduit means comprises a supply conduit coupling said central source to each of said terminals and a return conduit coupling each of said terminals to said central source.

3. The method as defined in claim 2 wherein said central source comprises a tank containing a mixture of water and deicing fluid.

4. The method as defined in claim 3 wherein said heating means comprises a heat exchanger, a first pump, and means coupling said tank, circulation pump and heat exchanger in a loop for the heating of fluid in said tank.

5. The method as defined in claim 4 and including providing a second pump coupled to said conduit means for providing pressurized deicing fluid to said terminals.

6. A deicing system for aircraft comprising:

a central source of deicing fluid including a first tank for water and a second tank for deicing fluid;

means for heating said deicing fluid;

a plurality of distribution terminals positioned at locations remote from said central source for providing deicing fluid thereat;

conduit means for coupling each of said terminals to said central source; and

means for circulating heated deicing fluid through said conduits and terminals for preheating said conduits.

7. The system as defined in claim 6 wherein said conduit means comprises a first supply conduit coupling said first tank to each of said terminals, a second supply conduit coupling said second tank to each of said terminals and a return conduit coupling each of said terminals to said first tank.

8. The system as defined in claim 7 wherein each of said terminals includes means for mixing fluid from said first and second supply conduits in a selectable proportion.

9. The system as defined in claim 8 wherein said heating means comprises a heat exchanger coupled to said first tank for heating said water.

10. The system as defined in claim 9 and including first pump means coupled to said first supply conduit and second pump means coupled to said second supply conduit for supplying pressurized water and deicing fluid respectively to said terminals.

11. A deicing system for aircraft comprising:

a central source of deicing fluid;

means for heating said deicing fluid;

a plurality of distribution terminals positioned at locations remote from said central source for providing deicing fluid thereat;

conduit means for coupling each of said terminals to said central source; and

means for circulating heated deicing fluid through said conduits and terminals for preheating said conduits and wherein each of said terminals includes connector means coupled to said conduit means for permitting an applicating hose to be coupled in the circulation path of heated deicing fluid for preheating the applicating hose.

12. A centralized deicing system for aircraft comprising:

a fixed source of heated fluid used for deicing an aircraft;

a plurality of distribution terminals each located in the area of an aircraft loading ramp, each of said terminals including means for coupling an applicating hose thereto;

conduit means extending between said source of fluid and said terminals; and

recirculation means coupled to said conduit means for recirculating heated fluid in said conduit means for preheating said conduit means.

13. The system as defined in claim 12 wherein said conduit means comprises a supply conduit coupling said source to each of said terminals and a return conduit coupling each of said terminals to said source.

14. The system as defined in claim 13 wherein said source comprises a tank containing a mixture of water and deicing fluid.

15. The system as defined in claim 14 wherein said fluid is heated by a heat exchanger and said system includes a first pump, and means coupling said tank, said pump and said heat exchanger in a loop for the heating of fluid in said tank.

16. The system as defined in claim 15 and further including a second pump coupled to said conduit means for providing pressurized deicing fluid to said terminals.

17. The system as defined in claim 16 wherein each of said terminals includes a bypass conduit coupling said supply and return conduits permitting recirculation of heated fluid in said system.

18. The system as defined in claim 12 wherein said source comprises a first tank for water and a second tank for deicing fluid.

19. The system as defined in claim 18 wherein said conduit means comprises a first supply conduit coupling said first tank to each of said terminals, a second supply conduit coupling said second tank to each of said terminals and a return conduit coupling each of said terminals to said first tank.

20. The system as defined in claim 19 wherein each of said terminals includes means for mixing fluid from said first and second supply conduits in a selectable proportion.

21. The system as defined in claim 20 and further including first pump means coupled to said first supply conduit and second pump means coupled to said second supply conduit for supplying pressurized water and deicing fluid respectively to said terminals.

22. The system as defined in claim 12 wherein each of said terminals includes connector means coupled to said conduit means for permitting an applicating hose to be coupled in the recirculation path of heated fluid for preheating the applicating hose.

23. A method for deicing aircraft comprising:

providing a stationary centrally located source of heated water;

providing a stationary centrally located source of deicing fluid;

providing a plurality of stationary distribution terminals and locating same remote from said sources, each terminal including means for coupling an applicating hose thereto;

coupling each of said centrally located sources to said terminals through conduit means for delivery of deicing fluid to said coupling means; and

providing a mixing valve means coupled to said conduits for selectively mixing water and deicing fluid delivered to coupling means; and

coupling an applicating hose to any of said terminals and applying deicing fluid mixed with heated water to an airplane located at said terminal.

24. A centralized deicing system for aircraft comprising:

a source of heated water;

a source of deicing fluid;

a plurality of distribution terminals remote from said sources, each terminal including means for coupling an applicating hose thereto;

conduit means coupling each of said sources to said terminals for delivery of deicing fluid to said coupling means; and

a mixing valve means comprising a valve positioned in each of said terminals coupled to said conduits for selectively mixing water and deicing fluid delivered to coupling means.

25. The system as defined in claim 24 wherein said valves include electrical means for remotely operating said valves.

26. The system as defined in claim 25 and further including means for recirculating heated water in said conduit means coupling said heated water source to said terminals.

27. The system as defined in claim 26 wherein said conduit means comprises a first supply conduit coupling said source of heated water to each of said terminals, a second supply conduit coupling said source of deicing fluid to each of said terminals and a return conduit coupling each of said terminals to said source of heated water.

28. The system as defined in claim 27 and further including first pump means coupled to said first supply conduit and second pump means coupled to said second supply conduit for supplying pressurized water and deicing fluid respectively to said terminals.

29. The system as defined in claim 28 wherein said recirculation means includes a bypass conduit extending between said first supply conduit and said return conduit and pump means for recirculating heated water in a path including said source of heated water, said first supply conduit, said bypass conduit and said return conduit.

30. The system as defined in claim 29 wherein each of said terminals includes connector means coupled to said conduit means for permitting an applicating hose to be coupled in the circulation path of heated water for preheating the applicating hose.

31. A centralized deicing system for aircraft comprising:

a source of heated fluid used for deicing an aircraft;

a plurality of terminals positioned remotely from said source and including a pair of connectors;

supply conduit means coupled to said source and to one connector of said pair of connectors;

return conduit means coupled to the other one of said pair of connectors;

a portable vehicle for the application of deicing fluid to an aircraft including an applicating hose having connector means at opposite ends for coupling said hose between said pair of connectors at said terminal; and

means for recirculating heated fluid through said applicating hose for preheating of said hose.

32. The system as defined in claim 31 and further including adjustable bypass conduit means in each of said terminals coupling said supply and return conduits and means for circulating heated fluid through said conduits including said bypass conduit during a standby mode of operation.