Tuesday, September 16, 2008

Deicing

From Wikipedia, the free encyclopedia
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De-icing is the process of removing ice from a surface.

Anti-icing is the process of preventing ice from forming on a surface.

De-icing can be accomplished by mechanical methods (scraping); through the application of heat; by use of chemicals, known as icemelters, designed to lower the freezing point of water (various salts or alcohols); or by a combination of these different techniques.

Aircraft

See also: ice protection system

When there are freezing conditions and precipitation, it is critical that an aircraft be de-iced. Failure to do so means the surface of the aircraft's wings will be too rough to provide for the smooth flow of air and thereby greatly degrading the ability of the wing to generate lift, possibly resulting in a crash. If large pieces of ice separate once the aircraft is in motion, they can be ingested into turbine engines or impact moving propellers and cause catastrophic failure. Thick ice can also lock up the control surfaces and prevent them from moving properly. Because of this potentially severe consequence, de-icing is performed at airports where temperatures are likely to dip below the freezing point.

De-icing techniques are also employed to ensure that engine inlets and various sensors on the outside of the aircraft are clear of contamination caused by ice or snow.

De-icing on the ground is usually done by spraying aircraft with a deicing fluid such as monopropylene glycol, similar to ethylene glycol antifreeze used in some automobile engine coolants. Ethylene glycol is still in use for aircraft deicing in some parts of the world, but Monopropylene glycol is more common because it is classified as non-toxic, unlike ethylene glycol. Nevertheless, it still must be used with a containment system to capture all of the used liquid, so that it cannot seep into the ground and streams. Even if it is classified as non-toxic, it still has negative effects in nature, as it uses oxygen as it breaks down, causing other life to suffocate. (In one case, a significant snow in Atlanta in early January 2002 caused an overflow of such a system, briefly contaminating the Flint River downstream of the Atlanta airport.) Many airports successfully recycle used deicing fluid, separating out water and solid contaminants in order to be able to reuse the fluid.

Though there are several different formulations of deicing fluid, they fall into two basic categories: Heated glycol diluted with water for deicing and snow/frost removal, also referred to as "Newtonian fluids", and unheated, undiluted glycol that has been thickened (imagine half-set gelatin), also referred to as "Non-Newtonian fluids", that is applied as an agent to retard the future development of ice or to prevent falling snow or sleet from accumulating. In some cases both types of fluid are applied, first the heated glycol/water mixture to remove contaminants, followed by the unheated thickened fluid to keep ice from reforming before the aircraft takes off. This is referred to as "a two-step procedure".

Inflight ice buildups are most frequent on the leading edges of the wings, tail and engines (including the propellors or fan blades). Lower speed aircraft frequently use pneumatic boots on the leading edges of wings and tail to affect de-icing in flight. The rubber coverings are periodically inflated, causing ice to crack and flake off in the slipstream. Once the system is activated by the pilot, the inflation/deflation cycle is automatically controlled. In the past, it was thought such systems can be defeated if they are inflated too soon; that the pilot must allow a fairly thick layer of ice to form before inflating the boots. More recent research shows “bridging” does not occur with any modern boots.[1]

B-17 bomber. The black strips on the leading edges of the tail, stabilizers and wing are decicer boots made of rubber.
B-17 bomber. The black strips on the leading edges of the tail, stabilizers and wing are decicer boots made of rubber.

Some aircraft may also use electrically heated resistive elements embedded in a rubber sheet cemented to the leading edges of wings and tail surfaces, propeller leading edges, and helicopter rotor blade leading edges. Such systems usually operate continuously. When ice is detected, they first function as de-icing systems, then as anti-icing systems for the duration of flight in icing conditions. Some aircraft use chemical de-icing systems which pump antifreeze such as alcohol or propylene glycol through small holes in the wing surfaces and at the roots of propeller blades, causing the ice to melt and making the surface inhospitable to further ice formation. A fourth system, developed by the National Aeronautics and Space Administration, detects ice on the surface by sensing a change in resonance frequency. Once an electronic control module has determined that ice has formed, a large current spike is pumped into the transducers to generate a sharp mechanical shock, cracking the ice layer and causing it to be peeled off by the slipstream.

Many modern civil fixed-wing transport aircraft use anti-ice systems on the leading edge of wings, engine inlets and air data probes using warm air. This is bled off the powerplants and is ducted into a cavity just under the surface to be anti-iced. The warm air heats the surface up to a few degrees above zero, preventing ice from forming on that surface. The system may operate completely autonomously, switching itself on and off as the aircraft enters and leaves icing conditions.

Infrared deicing

Infrared is the transmission of energy by means of electromagnetic waves or rays. Infrared is invisible and travels at the speed of light in straight lines from the heat source (the emitter) to all surfaces and objects (the receivers) without significantly heating the space (air) through which they pass. When infrared waves strike an object, they release their energy as heat. This heat is then either absorbed or reflected by the cooler surface. Infrared energy is continually exchanged between "hot" and "cold" surfaces until all surfaces have reached the same temperature (equilibrium). The colder the surfaces, the more effective the infrared transfer from the emitter. This heat transfer mechanism is substantially faster than conventional heat transfer modes used by conventional deicing (convection and conduction) due to the cooling effect of the air on the deicing fluid spray.

References

See also

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