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High-Tech Electro-Defroster

DahBaker writes to mention a News.com story about an ingenious way to de-ice a surface. From the article: "Dartmouth College engineering professor Victor Petrenko, not to be confused with one of the Champions on Ice, has devised a way to use a burst of electricity to remove ice caked on walls or windows. For surfaces coated with a special film, the jolt gets rid of ice in less than a second, far less time than it takes to hack at it with an ice scraper. While drivers might find easy-cleaning windshields convenient, the technology--called thin-film pulse electrothermal de-icing, or PETD--could have significant economic impact if widely deployed. It could, for example, cut the costs of repairing power lines downed by ice storms and keep plane windshields frost-free, decreasing fuel consumption."

21 of 109 comments (clear)

  1. Not just plane windshields by MadEE · · Score: 5, Insightful

    Assuming the material is durable enough it would be great on the flying surfaces too preventing icing which adds considerable weight and changes the aerodynamics of the plane. This would probably be far lighter then current solutions for this.

    1. Re:Not just plane windshields by Maxwell'sSilverLART · · Score: 4, Insightful

      Assuming the material is durable enough it would be great on the flying surfaces too preventing icing which adds considerable weight and changes the aerodynamics of the plane. This would probably be far lighter then current solutions for this.

      Actually, this was my first thought too, but after reading the article, I'm not sure how much use it would be in aviation. As you correctly point out, the big problem with ice in aircraft isn't the windshield, but airframe icing (wings and tail); ice (or even frost) changes the shape of the airfoil, destroying the lifting capabilities of the surfaces.

      With a small panel, like a windshield, the power problem is manageable, but the leading edge of an airliner's wing is several hundred square feet (even a relatively small 737 has a wingspan of over a hundred feet for the later models, and you need to go at least a foot or two back on both top and bottom). Even assuming we only work on the leading edge, that's a hell of a lot of surface, and thus a lot of power. In reality, jet aircraft use hot wings, heated by bleed air from the turbines, and they heat the water on the leading edges enough that it stays liquid all the way to the trailing edge--these systems are more correctly called "anti-icing" than "de-icing."

      Smaller aircraft do use de-icing systems, in the form of pneumatic boots. With such systems, ice is allowed to accumulate until it reaches sufficient thickness to be thoroughly broken by inflating the boots, causing it to crack and fall off (deploying the boots early can result in the ice simply forming around the shape of the inflated boots, rather than their deflated shape, rendering the boots ineffective). I'd be interested to see whether this system suffers from a similar problem, or if it is effective against even trace buildups.

      The problem with it in light aircraft, though, is that such aircraft tend to have very low power budgets--there's not much surplus energy around. If there were, they'd use anti-icing systems, but intermittently shedding accumulated ice is very energy-efficient, especially when compared to energetic ice prevention (some aircraft carry alcohol anti-icing solution, which is excreted through "weeping wings" to forestall ice formation, but such systems are limited in the protection they can offer, both in severity and duration of icing conditions). Thermal anti-icing is cost-prohibitive, and electrical systems in light aircraft tend to be adequate, but with little overhead--while this system is more efficient than (presumably electrical) heating, it still may not be efficient enough. I'd also be interested to see what kind of electrical and magnetic noise this system might generate, though I'm sure that's been considered.

      All in all, this sounds like a neat idea, but I'm not sure it's going to find its market in aviation.

      --
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    2. Re:Not just plane windshields by Needles · · Score: 2, Interesting

      When I was in school, during one of the ASME meetings we had a presentation of a device to remove the ice from the wings. The plan was to have a series of these plates on the leading edge of the plane. during normal flight they would be inlayed into the wing and be aerodynamic. If you were in an icing condition you would start a trickle charge a bank of compactors. Then once the charge was built up a series of panels would "pop" pushing the ice off the wing. Then the caps would recharge and a second series of panels would knock more ice off. and so on. Don't know what happened to the project. anything dealing with aviation takes a long time to develop. It has only been 8 years, which is not really that long for a industry with those types of safety standards.

    3. Re:Not just plane windshields by MadEE · · Score: 2, Interesting

      The problem with it in light aircraft, though, is that such aircraft tend to have very low power budgets--there's not much surplus energy around. If there were, they'd use anti-icing systems, but intermittently shedding accumulated ice is very energy-efficient, especially when compared to energetic ice prevention (some aircraft carry alcohol anti-icing solution, which is excreted through "weeping wings" to forestall ice formation, but such systems are limited in the protection they can offer, both in severity and duration of icing conditions). Thermal anti-icing is cost-prohibitive, and electrical systems in light aircraft tend to be adequate, but with little overhead--while this system is more efficient than (presumably electrical) heating, it still may not be efficient enough. I'd also be interested to see what kind of electrical and magnetic noise this system might generate, though I'm sure that's been considered.

      The actual pulse needed to operate the stuff according to the article is in the manner of milliseconds all but the most heavily avionics laden aircraft should be able to handle the short pulse required to remove the ice from the surfaces.

    4. Re:Not just plane windshields by Hal9000_sn3 · · Score: 2, Interesting

      When I was at Cessna, working in the Experimental department, we tested just such a system. That was in 1985 or 1986. One major issue was that the interference with avionics was quite unacceptable, another was that the manufacturing cost was a lot more than the pneumatically inflated de-icing boots that were the status quo. It was quite fun to hold a penny near the leading edge and have it disappear, then hear it hit the wall on the other side of the hangar. Oh, yeah. That reminds me. Metal fatigue of the underlying structure. Simply not acceptable in aircraft.

    5. Re:Not just plane windshields by aibrahim · · Score: 3, Informative

      Maybe instead of "thinking" about the issue you should have checked out the company site where they have a video of ice being removed from an airfoil in a wind tunnel.

      That seemed like a fairly conclusive demonstration of the practicality of this process for that purpose.

      Now where is that damn pretty floral bonnet of mine...

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    6. Re:Not just plane windshields by darthwader · · Score: 4, Informative
      (deploying the boots early can result in the ice simply forming around the shape of the inflated boots, rather than their deflated shape, rendering the boots ineffective.)

      I really hope that no pilots are getting their flying advice from slashdot (just like no lawyers are getting legal advice here), but just in case: the latest research indicates that ice bridging is a myth, and you should use the boots as soon as you detect any icing, rather than waiting for build-up.

      http://www.aopa.org/pilot/features/inflight9910.ht ml, http://www.elliottaviation.com/wavelink/1999q1/wav art21.asp and http://www.faa.gov/library/manuals/examiners_inspe ctors/8400/fsat/media/fsat9818.doc are good references.

      http://www.pilotfriend.com/safe/safety/icing_condi tions.htm is a great article about all sorts of aircraft de-icing and anti-icing methods.

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    7. Re:Not just plane windshields by drkich · · Score: 2, Insightful

      I guess one of the points is, with the de-icing fluid carrys cost with it. One for the actual cost of the liquid, two the environmental clean up and three the man hours to do the work. And if I recall correctly, do they not actually sometimes do it multiple times before take off?

      So the question is, over the life of the plane, and the number of times it will be deiced, what is the cost benefit ratio. Do we save money even with the extra weight? Or is it still cheaper with the old method? That is something for the accountants to figure out. I am sure someone, somewhere will at least do the study.

    8. Re:Not just plane windshields by Silentnite · · Score: 2, Insightful

      Since no one else here is going to pipe in with airline experiance I may as well.

      When you de-ice/anti-ice an aircraft you spray it with a chemical. The De-ice is by all other virtue and for the sake of this argument just hot water. The Anti-ice is an expensive(and I mean EXPENSIVE) compound that resembles the slime left in the wake of ghostbuster's three with slimer(was that three? or two?). In order to provide an effective coating and bumping up the hold-over times(the time to get from the gate and into the air) you need a good thick coat. Mind you it slides off after takeoff once they get up to speed, but the reason its accounted for in airplane weight is the take off. Due to the excess weight of the anti-ice fluid, planes need longer to take off, and usually can carry less.

      Ah, if only we could load people and bags in the air like the airforce does with fuel. Damn.

    9. Re:Not just plane windshields by aibrahim · · Score: 2, Informative

      I can see that being an ass generates a pile of interest. It unfortunately doesn't engender any actual reasoning, just more "thinking." You people are intellectually lazy.

      Maybe I should try leading by example instead.

      The key is that the GP says power, but he is really talking about energy budgets. This thing needs power over a very short time. Not a huge pile of energy.

      How much energy... How about a calculation... oh dear is that sort of thing even possible on /. ? I'll try anyways. One caveat, whenever I trot out numbers: I *insist* you double check before believing them.

      Lets pretend we are de-icing the entire surface area of a 747-400D, 541.2m^2. This is a huge overestimate of our work loads, because we really only have to defrost the leading edges and a foot or two back.

      The C|Net article linked says he only needs to melt a micron or two for it to work, so we'll aim for three microns, or 3*10^-6 meters.

      Ladies and gentlemen the total volume of water we are talking about over that vast area with the assumptions I have made is 1.6 mm^3. That is only about .146 grams of water.

      That means we must expend .146 calories people. That's .611 joules.

      You think a plane of any sort can spare lets say 611 joules, enough energy to de-ice the wings of a 747 a thousand times a flight ?

      If you really think they don't have the energy budget, maybe we can just stick a D-Cell battery on board. Of course that's overkill because a D-Cell stores 10000 joules.

      What about efficiency ? According to Petrenko's site at Dartmouth the system is wastes almost zero heat energy because of the short time over which it operates. Basically there is no time for it to go anywhere else.

      You think we can somehow draw such a tiny amount of energy on even the flimsiest Cessna ? If not, I'm not getting into the damn thing.

      In any case, it turns out Goodrich Aerospace has had good results flight testing the system on propeller driven aircraft, and is preparing to flight test it on jets. No details I got that from Petrenko's page at Dartmouth too.

      Are you all starting to understand how cool this technology is ?

      --

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    10. Re:Not just plane windshields by ipfwadm · · Score: 2, Informative

      Someone else already pointed out your obvious mistake in converting cubic meters to cubic millimeters, but that's not the only error...

      the total volume of water we are talking about over that vast area with the assumptions I have made is 1.6 mm^3. That is only about .146 grams of water.

      Isn't one of the supposed beauties of the metric system that you can deal with powers of 10? So how can it possibly be the case that 1.6 cubic millimeters is equivalent to .146 grams? That would be a factor of 10.9589. Of course, even if we were to use a factor of 10 we'd still be wrong since you again screwed up the conversion due to not working in three dimensions: there are 1000 cubic millimeters in a cubic centimeter, not 10. So if the starting number were really 1.6mm^3 (which it's not as the other poster pointed out), that would equate to 0.0016 grams of water, not 0.16, and certainly not 0.146.

      So, combining the original screw-up (which made your number low by a factor of a million) with this one (which made you high by a factor of a hundred), as well as your whacked out mm^3 -> gram conversion (which made you low by 10%), the final answer should be... about 6.8 kJ. Or 6.8 MJ if you want to do it a thousand times in a flight.

      But wait, there's more! You're assuming that the temperature of the ice needs only be raised by 1 degree C. The article says it needs to be raised TO 1 or 2 degrees C, but who knows what the starting temperature of an iced-up wing is. But let's say we need to raise it 5 degrees. Now we're up to 34 kJ.

      But wait, there's STILL more -- and this one's a biggie! You're (conveniently) ignoring heat of fusion. Remember that from chemistry class? So tack on another 334 joules per gram of water. At 1600 grams, that's another 534kJ every time you fire off this thing, for a grand total of 567kJ per use, or so many megajoules if it's used 1000 times in a flight. Not gonna de-ice a 747 with a D cell anymore, are we?

      And just as an aside, 541 meters^2 isn't as big an overestimation as it may seem at first glance, because that is not the "total surface area" of the wings, it is the wing area. You'd need to multiply 541 by 2 to get the total wing surface area, as wings have two sides - you know, a top and a bottom. You may even need to multiply it by a little more than 2 since I'm assuming wing area is just the area of the wing's planform, and not actual surface area which would be higher due to the airfoil shape, but I'm not an aeronautical engineer so I don't know.

      Don't post innacurate information

      How about your hideously wrong math, does that count as inaccurate information? And what about your hideously wrong spelling of inaccurate?

  2. Re:Is it me.. by MyLongNickName · · Score: 4, Funny

    Everyone was out on a hot date, or getting ready for the celebration of Christ's resurection. This is Slashdot after all.

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  3. Re:Is it me.. by Anonymous Coward · · Score: 2, Funny

    It says a lot about the editors when they post three (3) Ask Slashdot questions during a period when nobody can post comments...

  4. Re:Is it me.. by MadEE · · Score: 2, Funny

    It's Saturday! You expect people to browse here when they are not getting paid to do something else?

  5. Sure, the windshields are more important. by TheDreadSlashdotterD · · Score: 2, Insightful

    It could be more useful on the wings. Keeping a plane in the air might be important too.

    --
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  6. Re:Is it me.. by topham · · Score: 2, Insightful

    I tried posting, but received a message the database was down for maintenance. fair enough, but I thought it was kind of dumb to post Ask Slashdot questions then.

    As for this article.. very cool. I need it on my car. bad.

  7. High tech, how? by evilviper · · Score: 2, Insightful

    I must be missing something... Maybe the article is just light on details, but I can't see how this is any more advanced than the rear window defroster standard in every car made in the past couple decades.

    Electricity turns to heat, and melts the ice. Yippie. In this instance it sounds like electricity is being applied directly to the ice, possibly making this slightly quicker and more effecient, but I don't see anything revolutionary here. I also can't see how this is any less obtrusive...

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  8. Re:Does this quote from TFA sound like BS? by Manchot · · Score: 2, Informative

    Well, this New Scientist article from 2002 is also about Victor Petrenko, and goes into a little more depth.
     
    Apparently, it is is the protons which are the majority charge carrier. If you remember your high school chemistry, there exists a small amount of hydrogen and hydroxl ions even in water with a pH of 7. Presumably, ice, which is a crystalline version of water, also has a small concentration of hydrogen and hydroxyl ions. According to the article, the free hydrogen ions (a.k.a. protons) travel between the crystalline structure of the ice, carrying current. I would guess that the hydroxyl ions don't do the same thing simply because they are much larger than hydrogen ions, and are effectively immobile in the lattice.

  9. Champions of the Ice by roman_mir · · Score: 3, Funny

    Victor Petrenko, not to be confused with one of the Champions on Ice - If you put those two into the same room, hilarity and confusion are bound to ensue, since they seem to be the Ice Champion and the Anti Ice Champion, the Ying and the Yang. We must keep them as far away from each other as possible, or there could be an anti-matter equivalent explosion.

  10. Forget the stuff about semiconductors by Flying+pig · · Score: 2, Insightful
    For windshields, this just seems to be all over defrosting from the inside by a fast pulse, a fast version of what Ford have been doing for years. You still have to remove the ice mechanically before it refreezes, otherwise the sheet will just stay in place and, as the article says, bond even more tightly than before (I've noticed this with Ford windshields - if you don't complete the melt cycle for some reason, you can get very firmly bonded ice.) Plus, what's the world indium supply like? And what is the chance of cracking the windshiled due to thermal shock? Heating the outside to 2 degrees C while the inside is at -10 doesn't sound terribly smart.

    So I suspect that to commercialise this a lot of research will be needed. Changes to windshield composition and design. Changes to wiper design. Uprated batteries. It might actually be cheaper to fit one of those nice Kenlowe or Eberspacher heaters with mobile phone control so you can simply start the car heating ten minutes before you leave the house or the office. After all, no matter how well the pulse technology works, at the end of it you are sitting in a freezing cold car, even if you can now see through the windshield.

    --
    Pining for the fjords
  11. Re:not new pricey answer to a nonexistent problem. by necro81 · · Score: 3, Interesting

    Preface: I was a grad student at the Thayer School of Engineering, where Petrenko does this research. During a power electronics class, we learned about the workings of some of this technology, and some classmates of mine designed some of the HF electronics that are behind this.

    Electrically heated windshields, propellers, etc... have been around for 70+ years. Yes, but those devices have heating elements that conduct heat into the bulk ice. You don't want to spend all the energy needed to melt all of the ice, or even a sizeable portion of it, but rather melt just the ice that's adhered to the windshield or airfoil. This technology does that. It creates HF eddy currents in the ice at the ice-windshield interface, liquifying that thin layer almost instantly. The liquification happens quickly enough that very little heat is conducted away into the bulk, which means that you aren't wasting or losing much energy. What's more, the heat is applied directly to the ice - no heater elements needed. Instead of pumping XX watts of power into heater elements and waiting for enough ice to melt to easily be removed, you pump (let's say) 10 times the power for 1/1000 the time into just the ice that matters, then let gravity, airflow, and wiper blades take care of the rest. It is a far more efficient way to remove ice.

    Jet planes spend 95% of their flying time way above or below the icing levels. Unfortunately, the place where icing is most likely is also the place where it is most dangerous: during takeoff and landing. Just because it is not a continuous threat during the flight doesn't mean that it isn't still extremely dangerous.

    Jet turbines have a virtually free and unlimited amount of hot air availbale for deicing. The hot gasses need to be hot if they are to produce thrust. Were the gasses diverted through some complicated heat exchanger to melt ice from the airfoils of aircraft, the exit gasses wouldn't produce nearly as much thrust. Once again, this technology works only on the ice that is adhered to the surface, and so works very efficiently. Using hot gasses, like heater elements, inevitably has most of its heat conducted into the bulk, where it does little good.

    It's not affordable to load down a plane with 100's of pounds of extra generators, batteries, and/or capacitors that are only needed in very rare and usally avoidable circumstances. This is not additional equipment for an airplane, it is meant to replace the de-icing equipment that some already have. Consider the cost of applying thousands of gallons of chemical de-icing to aircraft wings on the ground, or the electrical equipment needed to generate the huge amount of electrical power that goes into heating elements. If anything, this technology would have less equipment associated with it than other methods, because it uses far less energy. The amount of energy that it takes to use this equipment, even over the entire leading edge of an aircraft's wing, it relatively small compared to the power needed to run everything else, or the tremendous power output of the engines. It makes use of high-frequency power electronics, which are much more compact and efficient than traditional power electronics. True, it isn't need all the time, but there is tons (literally, tons) of equipment in an airplane that is only used occassionally. They all serve a specific purpose. I will admit that it will be expensive technology at the beginning, especially for retrofits, but most new technology is. Airbags were initially only seen in high-end luxury cars, but eventually trickled down to lower models.

    The planes that would need this the most, little prop planes that can't climb above icing, are also the ones that can least afford the weight penalty of this deicing system. Adding even 150 pounds to a small plane can make it a non-viable flying machine. Once again, this is not additional equipment, it is meant to replace existing de-icing equipment on a plane.