AeroElectric-List Digest Archive

Wed 01/21/09


Total Messages Posted: 5



Today's Message Index:
----------------------
 
     1. 10:30 AM - Re: AeroElectric-List Digest: 14 Msgs - 01/19/09 (Jesse Jenks)
     2. 03:34 PM - Re: Re: AeroElectric-List Digest: 14 Msgs - 01/19/09 (BobsV35B@aol.com)
     3. 07:10 PM - Re: Wig Wag system (Sully)
     4. 08:05 PM - Re: Wig Wag system (marcausman)
     5. 09:58 PM - Re: Static wicks (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 10:30:56 AM PST US
    From: Jesse Jenks <jessejenks@hotmail.com>
    Subject: RE: AeroElectric-List Digest: 14 Msgs - 01/19/09
    Thanks guys. You both seem to be saying that bonding is important=2C and st atic wicks not so much. Just wondering why bonding? Jesse > Time: 07:31:39 AM PST US > From: Harley <harley@AgelessWings.com> > Subject: Re: AeroElectric-List: Static wicks > > They can work to dissipate static if they are attached to a conducting > surface. That way=2C they can bypass whatever is creating the static and > insulating the object from a normal ground (like the plastic or rubber > tires on a fork lift). > > But on many homebuilts=2C the plane is made of non conducting materials > (wood and fabric or fiberglass and/or epoxy)=2C and a static wick will > only discharge the point that it is attached. A couple of inches away > from that point=2C the charge remains as strong as ever. > > I had many a discussion with fork lift drivers at Pennwalt when they > would attach a static wick to the plastic part of the frame on the truck > (it was easier to drill a hole into)=2C and then complain that they still > got zapped when they stepped off the truck. For those that really > thought they needed it=2C we would attach the wicks to the metal frame > under the truck. But=2C that often didn't help either=2C because the wick > was often dragging on a non conducting surface (epoxy sealed floors). > Also=2C the line operators used vacuum cleaners to pick up the spilled > foot powder...even though they used a so-called static proof hose (it > had a grounded wire spiraling along the length of it) they would still > get zapped when they put the hose down. The charge was decreased=2C > because of the presence of the wire=2C but still built up on the hose > between the wire coil wraps. > > In short=2C you need a continuous conductive path to discharge a static > charge. From every area where the charge can build. > > Harley > ------------------------------------------------------------------------ > > > Jesse Jenks wrote: > > I have always wondered why (most) certified airplanes have static > > wicks=2C but not homebuilts? This makes me want to know what their > > actual function is? I was always taught "they dissipate static > > electricity". Is static really that big of an issue=2C and if so=2C do > > wicks actually make a difference? I'm building an all metal airplane=2C > > and so far have not given any thought to control surface bonding=2C or > > static wicks. > > Thanks. > Time: 09:23:39 AM PST US > From: BobsV35B@aol.com > Subject: Re: AeroElectric-List: Static wicks > > Good Morning Jesse=2C > > I have almost no experience in homebuilt aircraft=2C but I do have severa l > thousand hours in aircraft that were equipped with static wicks and sever al > thousand hours in aircraft with no static wicks applied. > > My suggestion would be to thoroughly bond all control surfaces=2C flaps > included=2C but not bother with static wicks unless you note a problem. > > The static problem was greater in the days of low frequency radio. It was > not at all uncommon to lose all communication capability when we were usi ng the > > HF transmitters and receiving on low frequency. I have encountered > precipitation static strong enough to knock out VHF communications for j ust a > very few > minutes=2C but that has never lasted more than four or five minutes. > > I have also experienced static discharges=2C but that has always been on > aircraft that were equipped with static wicks. There is no doubt that I h ave flown > > in much heavier precipitation in static wick equipped airplanes than I h ave > in airplanes that are not so equipped=2C but I have flown both in some ra ther > severe situations. > > Wait and see if you have a problem. > > If you lose VHF navigation capability in a heavy thunderstorm=2C you may want > to add static wicks or you may just decide to stay out of such conditions ! > > In any case=2C I have never seen a GPS signal affected by any static buil d up. > > The only time I would suggest using static wicks is if your only means of > navigation is a LORAN. Even then=2C you don't need it if you stay out of > precipitation. > > Summary? Bonding YES=2C Static Wicks? NO > > Happy Skies > > Old Bob > AKA > Bob Siegfried > Ancient Aviator > 628 West 86th Street > Downers Grove=2C IL 60516 > 630 985-8502 > Stearman N3977A > Brookeridge Air Park LL22 > > > In a message dated 1/19/2009 8:52:32 A.M. Central Standard Time=2C > jessejenks@hotmail.com writes: > > I have always wondered why (most) certified airplanes have static wicks =2C but > not homebuilts? This makes me want to know what their actual function is ? I > was always taught "they dissipate static electricity". Is static really that > big of an issue=2C and if so=2C do wicks actually make a difference? I'm building > > an all metal airplane=2C and so far have not given any thought to contro l > surface bonding=2C or static wicks. > Thanks. > _________________________________________________________________ Windows Live=99: E-mail. Chat. Share. Get more ways to connect. http://windowslive.com/explore?ocid=TXT_TAGLM_WL_t2_allup_explore_012009


    Message 2


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    Time: 03:34:35 PM PST US
    From: BobsV35B@aol.com
    Subject: Re: RE: AeroElectric-List Digest: 14 Msgs - 01/19/09
    Good Afternoon Jesse, Bonding is easy, cheap, and light weight. It will probably do some good. In any precipitation at all, different potentials will be built up on isolated components. If all of those isolated components are joined by grounding or bonding straps, any precipitation static that is produced will be minimized and most of it will be shed off the sharp edges of the tail feathers or the ailerons. If you add the static wicks, they will shed the static even better, but the static wicks are heavy, expensive and the most effective ones are so dangerous to personnel that they are generally removed when the airplane is not flying. I don't know if bonding mitigates ten percent of the static or ninety percent of the static, but it is extremely cost effective. Happy Skies Old Bob AKA Bob Siegfried Ancient Aviator 628 West 86th Street Downers Grove, IL 60516 630 985-8502 Stearman N3977A Brookeridge Air Park LL22 In a message dated 1/21/2009 12:32:47 P.M. Central Standard Time, jessejenks@hotmail.com writes: Thanks guys. You both seem to be saying that bonding is important, and static wicks not so much. Just wondering why bonding? Jesse **************A Good Credit Score is 700 or Above. See yours in just 2 easy steps! cemailfooterNO62)


    Message 3


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    Time: 07:10:38 PM PST US
    Subject: Re: Wig Wag system
    From: "Sully" <mr.sully@tx.rr.com>
    Marc, Will the VP-200 wig wag HID lights? -------- Sully RV-7 In-work Read this topic online here: http://forums.matronics.com/viewtopic.php?p=226113#226113


    Message 4


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    Time: 08:05:40 PM PST US
    Subject: Re: Wig Wag system
    From: "marcausman" <marc@verticalpower.com>
    Yes, HID lights need a warm-up period then you can begin wig-wag. The warm up and transition to wig-wag is all automatic. This feature is coming in the next software release, about mid-year 2009. Current customers or customer who purchase prior to the software upgrade can upgrade for free. -------- Marc Ausman http://www.verticalpower.com RV-7 IO-390 Flying Read this topic online here: http://forums.matronics.com/viewtopic.php?p=226125#226125


    Message 5


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    Time: 09:58:15 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Static wicks
    At 08:48 AM 1/19/2009, you wrote: >I have always wondered why (most) certified airplanes have static >wicks, but not homebuilts? This makes me want to know what their >actual function is? I was always taught "they dissipate static >electricity". Is static really that big of an issue, and if so, do >wicks actually make a difference? I'm building an all metal >airplane, and so far have not given any thought to control surface >bonding, or static wicks. >Thanks. When two dissimilar materials slide past each other rapidly, there is a tendency for electrons to be transferred from one material to the other . . . usually from the lesser conductor to the greater conductor. Shuffle your feet on the carpet and you can get a pretty good zap touching a doorknob. Slide out of your car on a cold dry day and it's not uncommon to find your body charged with a noteworthy packet of energy that wakes up your nervous system where the sparks jump from your bod. Airplanes flying in snow, ice particles or even rain can accumulate a surface charge of excess electrons. The faster airspeeds and higher particle density makes the build up stronger. If the quantity of excess charge is great enough AND there's some handy point or edges where the charges tend to collect, you can SEE the effects in the form of a luminous hazy discharge along the edge or at the point. On some models of King Airs we used to get reports of luminous glow around the window frames of glass fitted with internal de-icing heaters. While the airplane is shedding excess charge from trailing edges, antennas, window frames, propeller tips, etc the phenomenon creates a broadband radio noise that HAS been strong enough to disable ADF, LORAN, Omega nav, HF communications and in severe cases, gets the VHF comm and nav receivers too. http://en.wikipedia.org/wiki/St._Elmo%27s_fire http://science.howstuffworks.com/st-elmo-fire1.htm The big problem we were having with discharges around the window frames is that it was etching the glass and in some cases, killing the de-ice heat sensors. VERY expensive. The radio noise comes from the disordered, high density discharge of an un-treated structure. The cure is to provide devices that have a propensity for dropping electrons off into the slip stream. These can be "wicks" . . . a thing that looks like a fine brush of copper cat-hairs . . . http://www.aircraftspruce.com/catalog/elpages/staticdischrgr.php Or an array of tiny points like these: http://www.b737.org.uk/wingtips.htm http://www.aircraftspruce.com/catalog/elpages/nullfieldtip.php This effect is not limited to airplanes. It can be a significant noise problem on stationary radio installations when there is blowing snow, dust, rain or significant convective activity as far away as 20 miles. If you have a sensitive enough ammeter, you can probe and actually measure this current as cited in this article. http://www.repeater-builder.com/pdf/staticbusterarticlecomplete.pdf A number of years ago, Beech did some extensive testing on the discharge characteristics of various brands and styles of wicks in the lab. There was a huge difference in performance of products then offered. I think folks making these things now are much better at it. Doing a GOOD discharger is not a trivial task although many folks have attempted it. Check out some of the techniques suggested here: http://www.aeroelectric.com/Reference_Docs/Patents/Static_Dissipation/ There have been a number of articles and postings to various forums about how to build your own. I've never seen an article that actually tested the handy work on the bench. Given what I witnessed at Beech many moons ago, I'm convinced that performance of DIY static wicks is a dart throw without quantified bench marks. The same process used to test wicks is use to test the airplanes probable discharge locations. The airplane is set up on plastic blocks. A long wand with a spherical end on it and a pico-ammeter in series is raised up to about 100,000 volts dc. You can run the wand along the trailing edges of possible concentration points and see the ammeter go up when the wand is closest to a location that would benefit from an effective discharge wick. Wicks are useful only on metal airplanes and then finding the optimum wick and placement is difficult. The occurrence of p-static is pretty rare for us guys who don't fly for a living. It won't hurt to have a half dozen wicks on your airplane but it may not be all that helpful. Wicks have nothing to do with lightning protection. Bonding the hinges on an airplane has nothing to do with mitigation of p-static effects. The idea here is to avoid welding the hinge rigid in case a lightning strike attaches to the control surface. Here's an short article I did on static-wicks for an EAA chapter newsletter some years back. http://www.eaa326.org/Newsletters/eaa326-3-2005.pdf Bob . . .




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