Aircraft propeller deicing systems prevent ice accumulation on propeller blades, helping maintain thrust efficiency and safe engine operation during icing conditions.
The formation of ice on the propeller leading edges, cuffs, and spinner reduces the efficiency of the powerplant system. Deice systems using electrical heating elements and systems using chemical deicing fluid are also used.
Electrothermal Propeller Deice System
Many propellers are deiced by an electrically heated boot on each blade. The boot is firmly cemented in place, receives current from a slip ring and brush assembly on the spinner bulkhead. The slip ring transmits current to the deice boot. The centrifugal force of the spinning propeller and airflow breaks the ice particles loose from the heated blades. [Figure 1]
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| Figure 1. Electro thermal propeller deice system components |
On one aircraft model, the boots are heated in a preset sequence, which is an automatic function controlled by a timer. This sequence is as follows: 30 seconds for the right prop outer elements; 30 seconds for the right prop inner elements; 30 seconds for the left prop outer elements; and, 30 seconds for the left prop inner elements. Once the system is turned on and automatic mode is activated, it cycles continuously. A manual bypass of the timer is incorporated. [Figure 2]
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| Figure 2. Propeller electrical deice system schematic |
Chemical Propeller Deice
Some aircraft models, especially single-engine GA aircraft, use a chemical deicing system for the propellers. Ice usually appears on the propeller before it forms on the wing. The glycol-based fluid is metered from a tank by a small electrically driven pump through a microfilter to the slinger rings on the prop hub. The propeller system can be a stand-alone system, or it can be part of a chemical wing and stabilizer deicing system such as the TKS™ weeping system.
How does an electrothermal propeller deice system function?
What is a slinger ring in a chemical deicing system?
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