AeroElectric-List Digest Archive

Thu 01/23/14


Total Messages Posted: 6



Today's Message Index:
----------------------
 
     1. 05:58 AM - Re: Strobe switches (racerjerry)
     2. 06:29 AM - Re: Re: Strobe switches (Rene Felker)
     3. 07:08 AM - Re: Strobe switches (Eric M. Jones)
     4. 07:44 AM - Re: Re: Strobe switches (Robert L. Nuckolls, III)
     5. 07:45 AM - Re: Strobe switches (Robert L. Nuckolls, III)
     6. 08:06 AM - Re: Re: Strobe switches (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 05:58:44 AM PST US
    Subject: Re: Strobe switches
    From: "racerjerry" <gki@suffolk.lib.ny.us>
    I am very reluctant to throw in my two cents here, as there are much greater minds than mine on this list. I figger that strobe power pack current characteristics may be causing switch arcing; slowly damaging the switch contact material, increasing contact resistance to the point where local heating and a snowball type failure occurs. There are quite a few different materials used for switch contacts. Depending on switch requirements and UL ratings; all contacts have their own characteristics and ability survive differing harsh environments. Ol tungsten lamps are similarly known for their high initial current inrush characteristics and switches require a T rating from UL, but these are AC switches and any arc is self extinguishing at the zero crossing point of the AC wave. DC switches are a different animal. DC switches require a quick snap action which is independent of operator manipulation. One trick for switch survival in such instances is to use a double pole switch with both sets of contacts wired in series to double arc distance and contact separation speed. (Thank you Mr. Tibolla, wherever you are). Again, if I were to guess, I would first suspect the initial current draw of the large strobe capacitor would be the cause. Any contact bounce on switch closing would definitely aggravate things and hasten failure. I too would want to check the current / voltage profile of that strobe. Carling generally makes darned good switches. -------- Jerry King Read this topic online here: http://forums.matronics.com/viewtopic.php?p=417461#417461


    Message 2


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    Time: 06:29:16 AM PST US
    From: "Rene Felker" <rene@felker.com>
    Subject: Re: Strobe switches
    Jerry, thanks for your input. I learned a lot. I do not have this problem in my airplane, but a better understanding of this failure mode will help me with future projects. Do not archive Rene' Felker N423CF 801-721-6080 -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of racerjerry Sent: Thursday, January 23, 2014 6:58 AM Subject: AeroElectric-List: Re: Strobe switches --> <gki@suffolk.lib.ny.us> I am very reluctant to throw in my two cents here, as there are much greater minds than mine on this list. I figger that strobe power pack current characteristics may be causing switch arcing; slowly damaging the switch contact material, increasing contact resistance to the point where local heating and a snowball type failure occurs. There are quite a few different materials used for switch contacts. Depending on switch requirements and UL ratings; all contacts have their own characteristics and ability survive differing harsh environments. Ol tungsten lamps are similarly known for their high initial current inrush characteristics and switches require a T rating from UL, but these are AC switches and any arc is self extinguishing at the zero crossing point of the AC wave. DC switches are a different animal. DC switches require a quick snap action which is independent of operator manipulation. One trick for switch survival in such instances is to use a double pole switch with both sets of contacts wired in series to double arc distance and contact separation speed. (Thank you Mr. Tibolla, wherever you are). Again, if I were to guess, I would first suspect the initial current draw of the large strobe capacitor would be the cause. Any contact bounce on switch closing would definitely aggravate things and hasten failure. I too would want to check the current / voltage profile of that strobe. Carling generally makes darned good switches. -------- Jerry King Read this topic online here: http://forums.matronics.com/viewtopic.php?p=417461#417461


    Message 3


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    Time: 07:08:41 AM PST US
    Subject: Re: Strobe switches
    From: "Eric M. Jones" <emjones@charter.net>
    Here's my guess: The only key difference in strobe supplies is their really big capacitors. When caps are flat (perhaps after long storage), their current demand is gigantic for a short time. Good design would put a peak current limiter like a CL-11 surge suppressor in the input circuit. An O-scope would show this, but maybe only on the first start after long storage. Furthermore the test design for this is tricky because the current you are trying to capture is very high and very short. A solid state relay, or any other relay, probably isn't the solution to the problem. -------- Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge, MA 01550 (508) 764-2072 emjones(at)charter.net Read this topic online here: http://forums.matronics.com/viewtopic.php?p=417468#417468


    Message 4


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    Time: 07:44:54 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Strobe switches
    At 07:57 AM 1/23/2014, you wrote: I am very reluctant to throw in my two cents here, as there are much greater minds than mine on this list. I figger that strobe power pack current characteristics may be causing switch arcing; slowly damaging the switch contact material, increasing contact resistance to the point where local heating and a snowball type failure occurs. I agree that some stress of this nature is in play. A stress that seems to be unique to a sub-set of the family of strobe products. I can't speak to the contact style of switches pre-Carling- rockers on the Cessnas. Without a doubt, the mechanical features of these switches went un-changed for decades and, perhaps, persist to this day. Here's a breakdown of the electron- pathway through a fast-on-tabbed Carling switch . . . http://tinyurl.com/qcmyt4e There are quite a few different materials used for switch contacts. Depending on switch requirements and UL ratings; all contacts have their own characteristics and ability survive differing harsh environments. Ol tungsten lamps are similarly known for their high initial current inrush characteristics and switches require a T rating from UL, but these are AC switches and any arc is self extinguishing at the zero crossing point of the AC wave. DC switches are a different animal. DC switches require a quick snap action which is independent of operator manipulation. One trick for switch survival in such instances is to use a double pole switch with both sets of contacts wired in series to double arc distance and contact separation speed. (Thank you Mr. Tibolla, wherever you are). Keep in mind that we've seen failures across the entire spectrum of metal-to-metal interfaces. http://tinyurl.com/96yqmg http://tinyurl.com/8zzkfbb Failures of terminals are almost always a failure to achieve gas-tight joining. Failure of the rivet joints are probably precipitated by degradation of the plastic housing material that relieves mate-up pressures between the tab and the contact-rivet. Degradation rooted in elevated temperatures at a slowly failing junction. Again, if I were to guess, I would first suspect the initial current draw of the large strobe capacitor would be the cause. Any contact bounce on switch closing would definitely aggravate things and hasten failure. I too would want to check the current / voltage profile of that strobe. Carling generally makes darned good switches. Carling's demonstrated service history has offered no incentives for folks in the airplane business to boot them off the airplanes. At the same time, tens of thousands of these same switches have endured the test of time as controls for strobe lighting systems. Some years ago, a company that employed my services banned a particular brand of relay from the fleet of products . . . they purged stock and replaced with Brand-M based on anecdotal information that Brand-M demonstrated a 'longer service life' in the same abusive slot on the airplane. Brand-M STILL stuck but only 1/3rd as often. It took several years of P&P (play and ponder) to finally deduce root cause . . . an effect that was not covered in any of the relay engineering manuals but repeated demonstrated on my workbench. The 'fixes' I recommended based on findings were never implemented. The failure rate had dropped down enough to fall off the ten-worst- problems list and the bean-counters lost interest. Observations of anecdotes here on the List suggest that what ever differences exist across the family of strobe lighting systems, there IS a characteristic that will bring out the worst joint in any bus-voltage pathway to the strobe supply. The 'worst' has manifested mostly in failures in and around the strobe switch. But Listers have told us that the fast-on terminal to their fuse-block has proven to be the weak-link that succumbed to the ravages of whatever weapon their strobe brought to the fight. I think we've observed and analyzed enough history to suggest that an investigation into weaponry is in order. Hence my decision to acquire tools of investigation which, with the help of others here on the List, may peel back the layers of the onion and make all secrets known. Our work here on the strobe switch failure mystery has little to zero chance of causing anyone to change their designs. The best we can hope for is to identify root cause and craft tools to identify its recurrence so that some brands of strobes can be avoided. Ever hear of "too-little, too-late"? By the time we figure this out, xenon strobes may be on their way out of the marketplace and the 'problem' will simply go away. But there are simple-ideas and science to be identified that will give foundation for any future investigation into mysterious failures of perfectly good switches and terminals. Bob . . .


    Message 5


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    Time: 07:45:29 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Strobe switches
    At 07:38 PM 1/22/2014, you wrote: > >Yes I still have the problem system and would be happy to send to you. >Just let me know the address and it's on it's way. No return required. Sure. P.O. Box 130, Medicine Lodge, Ks, 67104-0130 Thanks! Bob . . .


    Message 6


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    Time: 08:06:53 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Strobe switches
    At 09:07 AM 1/23/2014, you wrote: Here's my guess: The only key difference in strobe supplies is their really big capacitors. When caps are flat (perhaps after long storage), their current demand is gigantic for a short time. Good design would put a peak current limiter like a CL-11 surge suppressor in the input circuit. But we've seen failures in switches that are always left on. Initial inrush events, while most severe, occur only at turn-on . . . what we're seeing appears to be a manifestation of persistent RMS heating . . . i.e. a recurring condition during operation. An O-scope would show this, but maybe only on the first start after long storage. Furthermore the test design for this is tricky because the current you are trying to capture is very high and very short. Actually, no worse that for getting a 100w landing light lit up from a cold start. Such inrush currents are generally limited by ship's wiring. Here's an exemplar plot for starting a 55W lamp. http://tinyurl.com/mvugala Cold resistance of the lamp was measured at 150 mOhm, wiring added another 165 mOhm for a total of 315 mOhm and a predictable inrush on the order of 14/.315 or 44A. If the bulb had a monster capacitor across it then the absolute max inrush would still be limited by a/c wiring to 14/.165 or 84A. This is in the ballpark for expected tungsten lamp inrush values cited when switches are rated in the lab. Ratings that assume the system integrator expects a service life in the thousands of cycles. We're witnessing failures in under 1000 cycles . . . perhaps as few as 200 cycles. The failures include devices that don't have to switch . . . only carry the load. It may be that initial inrush is a factor but I'm guessing it's not the dominate effect. The fact that many strobe systems do not exhibit the problem while one system can duplicate the problem several times suggests that root cause can be chased down by comparing problem children with well behaved children . . . A solid state relay, or any other relay, probably isn't the solution to the problem. A solid state relay will eliminate the failures with roots in contact resistance . . . but there are other metal-to-metal joints at risk. You're right, there's more going on here than can be explained by failure to observe switch ratings from the catalogs. Bob . . .




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