13.15 Ice and Rain Protection Flashcards
(87 cards)
What effect does icing on forward facing areas of an aircraft cause?
- Decrease in lift (loss of streamline flow of air around the leading edges and top surfaces)
- Increase in drag (rough surface increases skin friction)
- Decrease propeller efficiency (change in blade shape)
- Loss of control (restriction of control surfaces)
- Increase in weight (CofG affected as well)
- Blockage of pitot static heads
- Obscured windows and windshields
What is supercooled water?
Water is present in liquid form at a temperature below the freezing point of 0°C
What is collection efficiency?
Measure of how much ice an aerofoil collects compared with the moisture content of air, droplet size and airspeed
For a small radius leading edge, what can the collection efficiency be?
95%
Why might the horizontal stabiliser have a higher collection efficiency than the wing?
It has a smaller radius than that of the wing
Where will Glaze icing or Runback icing occur?
In very dense clouds
Water particles are large and only slightly supercooled
or
In supercooled rain where the water droplets are of a large size
Temperatures range from 2°C to –10°C
What does glaze or ‘runback’ ice consist of?
Transparent or translucent coating of ice with a glossy surface appearance
Why is glaze or ‘runback’ ice considered the most dangerous?
Much greater spoiling effect on the airflow over the various surfaces
How will rime ice appear?
Light texture having a white crystalline appearance
Describe hoar frost?
Occurs on a surface which is below the freezing point of 0°C
Forms in clear air, water vapour being converted directly into ice crystals forming a white feathery coating
Occurs on the surface of wings where integral fuel tanks are fitted
What has research shown about the relative stalling speed of propeller driven aircraft that are affected by icing?
30% above the normal stalling speed
What is the difference between anti–icing and de–icing?
Anti–icing – prevents the formation of ice
De–icing – removes ice after formation
What are the four methods used for aerofoil ice protection?
Thermal
Electrical
Pneumatic
Fluid
How is bleed air delivered to the leading edge of the wing for anti–icing purposes?
Perforated air duct called a piccolo, or spray tube
What pressure is the ice protection system air regulated to?
18–20 psi
What is the period for which the tail ice protection will be active for, after the crew push the switch marked TAIL?
2 – 2.5 minutes
Overheat switches for ducting which are restricted on the ground, are restricted at what temperature and why?
90°C
No cooling airflow from aircraft movement, means components are at risk of overheating
What is the purpose of the amber VALVE light in the wing anti–icing system?
While the valve is moving between positions (fully open and fully closed)
What indication is there that a wing anti–icing system is turned on?
White ON light
What are the three occasions where you would receive an amber VALVE caption for the wing anti–icing system?
Normal operation when the valve is motoring between stops
When there is a discrepancy between the valve position and the switch position
During test
What causes the anti–ice valve, of the wing anti–icing system, to close during ground test and where is it located?
Ground overheat sensing switch just outboard of each anti–ice valve
Sensing 90°C approximately
What are spray mats also known as?
Heater mats
Where are continuously heated breaker strips fitted and why?
Between intermittently heated area
Ensures that small areas of ice removed are small enough not to cause a hazard to the aircraft
How is the heater mat constructed to provide insulation between mat and aircraft structure, and to provide better transference of heat to the outside where ice forms?
Outer glass fibre layer is thinner than the inner layer