| 摘要 |
An external system installed on a helicopter to spray a freezing point depressant fluid onto the main rotor blade of a single rotor helicopter to prevent the collection of ice when flying through icing weather. Actuation of this ice protection system will cause a pump to force a glycerine-alcohol mixture through a series of fixed nozzles to create a spray of freezing point depressant. The main rotor blade will move through this spray and be coated, thus preventing the collection of ice on the blade. Such protection is of vital importance to all-weather helicopter operations as experience has shown that the collection of ice on the rotor blades of helicopters is a safety of flight problem.
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