Mobile system for deicing aircraft
First Claim
1. A deicing system for applying a deicing mixture to an aircraft, the system comprising:
- a first tank for holding water;
a second tank for holding deicing fluid;
a water heater in fluid communication with said first tank for heating the water;
a heat exchanger, located in said second tank and in fluid communication with said heater, for accepting the heated water to heat the deicing fluid;
a first pump in fluid communication with said first tank for pumping water;
a second pump in fluid communication with said second tank for pumping deicing fluid;
heater control means, coupled with said first pump, for controlling flow of the heated water through said heat exchanger until the temperature of the deicing fluid in said second tank reaches a preselected temperature;
mixing means in fluid communication with said first and second tanks for mixing the water and the deicing fluid;
mixing control means for providing a choice of a plurality of selected mixtures of water and deicing fluid to said mixing means; and
a nozzle in fluid communication with said mixing means to apply one of the preselected mixtures to the aircraft.
3 Assignments
0 Petitions
Accused Products
Abstract
A deicing system for applying a deicing mixture to an aircraft is provided. Water is enclosed in a first tank, and deicing fluid in a second tank. A first pump transfers water through a heater, to a heat exchanger located in the second tank. The deicing fluid is thereby heated to a desired operating temperature by the hot water flowing through the heat exchanger, with the flow of hot water controlled by a heater control device. The first pump and second pump transfer heated water and heated deicing fluid, respectively, to a mixing chamber. A mixing control means controls the respective flows to provide the desired mixture. The mixture of water and deicing fluid is then applied to the aircraft via a nozzle.
112 Citations
26 Claims
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1. A deicing system for applying a deicing mixture to an aircraft, the system comprising:
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a first tank for holding water; a second tank for holding deicing fluid; a water heater in fluid communication with said first tank for heating the water; a heat exchanger, located in said second tank and in fluid communication with said heater, for accepting the heated water to heat the deicing fluid; a first pump in fluid communication with said first tank for pumping water; a second pump in fluid communication with said second tank for pumping deicing fluid; heater control means, coupled with said first pump, for controlling flow of the heated water through said heat exchanger until the temperature of the deicing fluid in said second tank reaches a preselected temperature; mixing means in fluid communication with said first and second tanks for mixing the water and the deicing fluid; mixing control means for providing a choice of a plurality of selected mixtures of water and deicing fluid to said mixing means; and a nozzle in fluid communication with said mixing means to apply one of the preselected mixtures to the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16)
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17. A deicing system for applying a deicing mixture including a Type II deicing fluid to an aircraft, the system comprising:
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a first tank for holding water; a second tank for holding Type II deicing fluid a water heater in fluid communication with said first tank for heating the water; a heat exchanger, located in second tank and in fluid communication with said heater, for accepting the heated water to heat the Type II deicing fluid; a first pump in fluid communication with said first tank for pumping water; a second pump in fluid communication with said second tank for pumping Type II deicing fluid without degenerating said Type II fluid; a heater control means, coupled with said first pump, for controlling flow of the heated water through said heat exchanger until the temperature of the Type II deicing fluid in said second tank reaches a preselected temperature; a mixing tube in fluid communication with said first and second tanks for mixing the water and the Type II fluid; a mixing control means for providing a choice of a plurality of preselected mixtures of heated water and heated Type II deicing fluid to said mixing means; as nozzle in fluid communication with said mixing means to apply one of the preselected mixtures to the aircraft; and second pump control means for activating said second pump when the spray nozzle is open and for deactivating said second pump when the spray nozzle is closed. - View Dependent Claims (18, 19, 20, 21, 22, 23, 24, 25, 26)
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Specification