AeroElectric-List Digest Archive

Sun 12/22/13


Total Messages Posted: 14



Today's Message Index:
----------------------
 
     1. 01:51 AM - Re: Re: Solicitation for opinions on backups (Peter Pengilly)
     2. 03:32 AM - Replacement crimpers  (Ralph Hoover)
     3. 06:00 AM - Re: Re: Solicitation for opinions on backups (Bill Watson)
     4. 08:28 AM - Any know is there a typical faliure mode for Soild State Relays (Jeffrey Skiba)
     5. 08:58 AM - Re: Re: Solicitation for opinions on backups (Robert L. Nuckolls, III)
     6. 09:44 AM - Re: Any know is there a typical faliure mode for Soild State Relays (Vern Little)
     7. 10:01 AM - Re: Any know is there a typical failure mode for Solid State Relays (Bob McCallum)
     8. 10:11 AM - Switch schematic (Carlos Trigo)
     9. 10:30 AM - Re: Switch schematic (rayj)
    10. 10:51 AM - Re: Switch schematic (rayj)
    11. 01:38 PM - Re: Any know is there a typical faliure mode for Soild State Relays (Robert L. Nuckolls, III)
    12. 06:09 PM - Re: Any know is there a typical faliure mode for Soild State R (Eric M. Jones)
    13. 09:00 PM - Re: Any know is there a typical faliure mode for Soild State Relays ()
    14. 09:52 PM - Re: Any know is there a typical faliure mode for Soild State Relays (Jeff Luckey)
 
 
 


Message 1


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    Time: 01:51:22 AM PST US
    From: Peter Pengilly <peter@sportingaero.com>
    Subject: Re: Solicitation for opinions on backups
    Don, My opinion is that I would provide power to your EFIS and main radios that does not involve the VPX. You have 2 alternators, so if the engine is turning you will likely have a power supply. When stuff goes wrong the work load goes through the roof very quickly, so keeping as much of your panel working as possible will minimise the rise in workload - and therefore your ability to continue to fly the airplane. I would suggest a D1 and an iPad are already plan f rather than plan b. Plan b should make the failure of any one component (including the VPX) almost transparent to the pilot. That means providing power to the EFIS and main radio that does not involve the VPX. It would be daft to have power available but a dark panel because one component in your system went down. Peter On 22/12/2013 03:43, donjohnston wrote: > > >> Please forgive my tongue in cheek reference to over-worrying >> a problem. > Apologies. I was unable to discern the location of your tongue for that post. [Laughing] > > >> My intent was to highlight a common problem with plug-n-play >> responses to incomplete questions. > And I wasn't really looking for an answer since I really didn't have a true question. I was really just looking (fishing, if you will) for opinions as to how far is too far when dealing with putting in "backups". > > My approach is fairly straightforward (at least for me). > > I'm running a standard, stock aircraft engine, mags (not an electronic ignition). My only deviation from what's been used in the foundation of GA aircraft for years is the VP-X. If the stock alternator fails, I've got a B&C SD-20. If that fails, I've got the battery. If the VP-X fails, the engine will continue producing power (the boost pump can pull power from the VP-X or directly from the battery). I'll be able to keep the shiny side up with the Dynon D1 for up to four hours (much longer than the battery would probably last). I've got a iPad with a GPS and a Garmin 396 to help me figure out where I'm going. > > So I think that I've got a good Plan B, C, D, E and F. > > I was just looking for opinions (not answers, opinions) on whether the additional wire, hardware, etc. required to keep the EFIS glowing happily running after the unlikely event of a VP-X failure was worth the trouble. And since I wasn't born yesterday, I know that opinions are like buttholes (everyone else's stink). > > We cool? 8) > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=416032#416032 > >


    Message 2


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    Time: 03:32:37 AM PST US
    Subject: Replacement crimpers
    From: Ralph Hoover <hooverra@comcast.net>
    OC asked about the simple procedure for AMP crimp QA. Their PIDG crimpers have a witness mark in the die that is visible in a crimp. It at least allows you to know that the proper crimper was used. The crimpers is also controlled cycle so that it must be closed all the way before it will release. Ralph Sent from my iPad


    Message 3


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    Time: 06:00:06 AM PST US
    From: Bill Watson <Mauledriver@nc.rr.com>
    Subject: Re: Solicitation for opinions on backups
    After reading this comment, I finally decided to actually read the Vertical Power overview. When I was designing my electrical system and panel 5 or 6 years ago, VP-X wasn't on my scope and I never looked back. If a recommendation is that I need to backup wire around the VP-X, I had to go "huh?" I can see that it can simplify the electrical system design task and adds some functionality. I can see the appeal. do not archive > My opinion is that I would provide power to your EFIS and main radios > that does not involve the VPX. > > You have 2 alternators, so if the engine is turning you will likely > have a power supply. > > When stuff goes wrong the work load goes through the roof very > quickly, so keeping as much of your panel working as possible will > minimise the rise in workload - and therefore your ability to continue > to fly the airplane. I would suggest a D1 and an iPad are already plan > f rather than plan b. > > Plan b should make the failure of any one component (including the > VPX) almost transparent to the pilot. That means providing power to > the EFIS and main radio that does not involve the VPX. It would be > daft to have power available but a dark panel because one component in > your system went down.


    Message 4


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    Time: 08:28:46 AM PST US
    From: Jeffrey Skiba <jskiba@icosa.net>
    Subject: Any know is there a typical faliure mode for Soild
    State Relays Any know is there a typical failure mode for Solid State Relays? Like do they typically fail OPEN ??? or do they Typical fail CLOSED (just l ike sometimes of a typical mechanical relay that the points weld together o r the spring fails ?) I am considering using solid state relays to replace mechanical relays but do not know if the ssr has a failure mode worse than them. I have attached one relay I found thus far to possibly replace a hydraulic motor contactor for a landing gear pump. Thanks in advance and HAPPY HOLIDAYS ! ________________________________ No virus found in this message. Checked by AVG - www.avg.com<http://www.avg.com>


    Message 5


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    Time: 08:58:50 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Solicitation for opinions on backups
    At 07:58 AM 12/22/2013, you wrote: After reading this comment, I finally decided to actually read the Vertical Power overview. When I was designing my electrical system and panel 5 or 6 years ago, VP-X wasn't on my scope and I never looked back. GOOD FOR YOU! It pays to be informed . . . If a recommendation is that I need to backup wire around the VP-X, I had to go "huh?" I can see that it can simplify the electrical system design task and adds some functionality. I can see the appeal. I don't think anyone has recommended any such thing yet. The phrase "catastrophic failure" was used as a worry-topic for the VP-X. I stretched the premise past the absurd by suggesting that 'meteors through the crankcase' might also be considered. The knowledgeable and skilled retorts might be something like this: "well considered chances of meteors through the crankcase is Z.F x 10 to the minus gazillion events per flight hour and the chances of a failure that cripples multiple systems in a VP-X system is G.C x 10 to the minus 6, 7 or 8 events per flight hour, hence there are NO practical worry points for either event. Given that nobody has come forth with a skilled MTBF study on VP-X (and none is expected), then we are left with the kinds of analysis that can be accomplished by judicious consideration of design features . . . or failure modes effects analysis. This is an activity that I encouraged Marc to conduct throughout the evolutionary advances to his design. We met in the pilot's lounge of KAAO about ten years ago when the VP-X system was but a gleam in his eye. Unlike some other products offered onto the OBAM and even TC aviation markets, there has been no hue and cry of customer dissatisfaction nor flurry of ADs against VP-X products so I am hopeful that Marc took my advice to heart and had conducted due diligence in the design, manufacturing and marketing of his products. At the same time, all of you as mney paying consumers of those products have every right to make detailed inquiry as to his design and verification processes. If you value your aluminum AND bones, then you have a DUTY to make such inquiry. The VP-X system is capable of taking on task criticality on a par with say an engine. We cannot carry back-up engines. Unless we have a confidence level in the VP-X system that is within a few orders of magnitude of that which we assign to engines, then the question of "back up" becomes more problematic. The difference here is whether we add a back-up because we DON'T know or because we DO KNOW. My bosses have paid me to find out such things for 50 years. . . . and yes, I'm reasonably certain that meteor shields built into the cowl will only add cost, weight and no value. You are your own boss. Okay boss, what's the drill going to be for assessing the necessity and/or value of adding a backup feature YOUR implementation of the VP-X system? Further, arriving at some useful conclusion will be much easier if it's crafted and sifted here on the List. GOOD information for doing . . . or NOT doing things is worth sharing. Bob . . .


    Message 6


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    Time: 09:44:07 AM PST US
    From: "Vern Little" <sprocket@vx-aviation.com>
    Subject: Re: Any know is there a typical faliure mode for Soild
    State Relays The failure mode for these devices are highly dependent on the internal construction. Contacting the manufacturer is only way to be sure. If it was just the internal powerFET that was the issue, the failure modes are well understood but details of the mechanical packaging may dominate. Vern From: Jeffrey Skiba Sent: Sunday, December 22, 2013 8:27 AM Subject: AeroElectric-List: Any know is there a typical faliure mode for Soild State Relays Any know is there a typical failure mode for Solid State Relays? Like do they typically fail OPEN ??? or do they Typical fail CLOSED (just like sometimes of a typical mechanical relay that the points weld together or the spring fails ?) I am considering using solid state relays to replace mechanical relays but do not know if the ssr has a failure mode worse than them. I have attached one relay I found thus far to possibly replace a hydraulic motor contactor for a landing gear pump. Thanks in advance and HAPPY HOLIDAYS ! ------------------------------------------------------------------------- ------- No virus found in this message. Checked by AVG - www.avg.com p> ------------------------------------------------------------------------- ------- No virus found in this message. Checked by AVG - www.avg.com 12/22/13


    Message 7


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    Time: 10:01:02 AM PST US
    From: Bob McCallum <robert.mccallum2@sympatico.ca>
    Subject: Any know is there a typical failure mode for Solid
    State Relays Jeffrey; I have not used the DC relays which you've linked to, but at work we have used the AC version of this particular brand of relay for controlling heating elements for approximately 25 years. Their biggest enemy, as with a lot of electronics, is heat. Because we do not implement large heat sinks to cool these relays ($cost$) we oversize them by approx 4X to ensure no heating issues and typically see less than .1% failures. (we do bolt them to steel enclosures, so they have some heat sinking) I have no statistics on the relative age or loads on the failed units. When the failures do occur they are almost always failure to close (in other words fail open) I have had one and only one fail closed however, so it would appear both failure modes are possible. We have also experimented with sizing them to approx 2X load current and have seen the five year failure rates rise, in this group, to approx 5%. As a result we returned to using the 50 amp models for greater reliability of our product. (loads are in the 3 to 14 amp range) While this anecdotal information may or may not apply to the DC versions of Crydom's product we're quite satisfied with the AC versions performance. I should also mention that the equipment we manufacture typically employing these relays runs 24/7 and these relays are controlled via a temperature controller cycling on/off up to as much as 50 cycles per minute, so we give them a good workout although we lightly load them. Bob McC _____ From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Jeffrey Skiba Sent: Sunday, December 22, 2013 11:27 AM Subject: AeroElectric-List: Any know is there a typical faliure mode for Soild State Relays Any know is there a typical failure mode for Solid State Relays? Like do they typically fail OPEN ??? or do they Typical fail CLOSED (just like sometimes of a typical mechanical relay that the points weld together or the spring fails ?) I am considering using solid state relays to replace mechanical relays but do not know if the ssr has a failure mode worse than them. I have attached one relay I found thus far to possibly replace a hydraulic motor contactor for a landing gear pump. Thanks in advance and HAPPY HOLIDAYS ! _____ No virus found in this message. Checked by AVG - www.avg.com p>


    Message 8


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    Time: 10:11:22 AM PST US
    From: "Carlos Trigo" <trigo@mail.telepac.pt>
    Subject: Switch schematic
    Guys Since I am not sure if this switch will suite my need can somebody please post a drawing of its eletric schematic. Thanks Carlos P.S. - I am looking for a switch for the fuel pump that can be powered from 2 independent power sources, being the middle position the OFF position


    Message 9


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    Time: 10:30:38 AM PST US
    From: rayj <raymondj@frontiernet.net>
    Subject: Re: Switch schematic


    Message 10


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    Time: 10:51:38 AM PST US
    From: rayj <raymondj@frontiernet.net>
    Subject: Re: Switch schematic
    Hope these will answer your questions. http://www.jameco.com/1/1/40651-2tl1-10a-switch-toggle-ms27408-4a.html http://www.jameco.com/Jameco/Products/ProdDS/1817426.pdf Raymond Julian Kettle River, MN. "And you know that I could have me a million more friends, and all I'd have to lose is my point of view." - John Prine On 12/22/2013 12:11 PM, Carlos Trigo wrote: > > Guys > > Since I am not sure if this switch will suite my need > Picture removed. > > can somebody please post a drawing of its eletric schematic. > > Thanks > > Carlos > > P.S. -- I am looking for a switch for the fuel pump that can be > powered from 2 independent power sources, being the middle position > the OFF position >


    Message 11


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    Time: 01:38:12 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Any know is there a typical faliure mode for
    Soild State Relays At 10:27 AM 12/22/2013, you wrote: Any know is there a typical failure mode for Solid State Relays? Like do they typically fail OPEN ??? or do they Typical fail CLOSED (just like sometimes of a typical mechanical relay that the points weld together or the spring fails ?) I am considering using solid state relays to replace mechanical relays but do not know if the ssr has a failure mode worse than them. I have attached one relay I found thus far to possibly replace a hydraulic motor contactor for a landing gear pump. Thanks in advance and HAPPY HOLIDAYS ! They can fail in ANY mode. I.e. stuck closed or stuck open. It depends on the stress that might have precipitated the failure. Were I considering such a device for use in a TC aircraft, the litany of deliberations goes something like this: 1. How many ways can this part fail? 2. How will each failure affect system operation? 3. How will I know it failed? 4. Is the failure pre-flight detectable? 5. Is failure of this part, in any failure mode, likely to create a hazard to flight? 6. Will failure of this part be likely to overtax my piloting skills for comfortably terminating the flight? Come of the gate ASSUMING the part will fail in every conceivable way . . . how do the answers to the above questions affect the way you use the part and how you react to the failure. Rule #1 Things Break Rule #2 Systems shall be designed so that when things break, no immediate hazard is created. Rule #3 Things needed for comfortable termination of flight require backup or special considerations to insure operation and availability. Rule #4 Upgrading the quality or reliability of a part shall be because you are tired of replacing it or want some new feature, not because it damned near got you killed. Suggest you review this short piece on FMEA. The FMEA worka around the problem of not knowing the whether or not the part has established reliability numbers. Assume that it will fail, rework the design or craft a plan-b so you can be pleasantly surprised when it never fails but have a comfortable response if it does. This philosophy for systems design is spelled out in more detail here http://tinyurl.com/ljl9qe6 http://tinyurl.com/lfkm2fl As a final note, be aware that your hydraulic pump motor is probably a permanent magnet variety with hefty inrush current. Make sure the device you pick can stand 500-1000 amp inrush for a few milliseconds . . . i.e. "rated" for motor or large incandescent lamp control. Bob . . .


    Message 12


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    Time: 06:09:25 PM PST US
    Subject: Re: Any know is there a typical faliure mode for Soild
    State R
    From: "Eric M. Jones" <emjones@charter.net>
    There is arguably no "typical" failure mode for anything at all. If there were, the engineers would be happy to see it because it would be an easy fix. A failure can be "typical" if a device is being misused. "Hey, the device typically fails if being misused!" I'll bet there are a million engineering stories there. Note: I have sold many SSRs, and I sometimes get "complaints" from customers who think that the apparent SSR no load output voltage when the relay is OFF indicates some flaw. Hmmmmmm....Well...there is always an no-load output voltage on every switch or relay...ON or OFF. But an SSR won't pass more than a microamp or so when OFF. So it won't light an LED. It is DEFINED as OFF for all practical purposes. -------- 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=416083#416083


    Message 13


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    Time: 09:00:49 PM PST US
    From: <berkut13@berkut13.com>
    Subject: Re: Any know is there a typical faliure mode for Soild
    State Relays That=99s what I did...less weight, less space, less environmental issues, cleaner operation (no contact bounce), etc. http://www.berkut13.com/berkut50.htm#SSR If you hydraulic system is anything like mine, you should also be used the snap action hydraulic pressure switches. Good luck, James Berkut/Race 13 www.berkut13.com Facebook: Berkut13 From: Jeffrey Skiba Sent: Sunday, December 22, 2013 10:27 AM Subject: AeroElectric-List: Any know is there a typical faliure mode for Soild State Relays Any know is there a typical failure mode for Solid State Relays? Like do they typically fail OPEN ??? or do they Typical fail CLOSED (just like sometimes of a typical mechanical relay that the points weld together or the spring fails ?) I am considering using solid state relays to replace mechanical relays but do not know if the ssr has a failure mode worse than them. I have attached one relay I found thus far to possibly replace a hydraulic motor contactor for a landing gear pump. Thanks in advance and HAPPY HOLIDAYS ! ------------------------------------------------------------------------- ------- No virus found in this message. Checked by AVG - www.avg.com p>


    Message 14


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    Time: 09:52:17 PM PST US
    From: Jeff Luckey <jluckey@pacbell.net>
    Subject: Re: Any know is there a typical faliure mode for Soild
    State Relays they sure are pricey - $130 ea. @ Mouser, ouch!=0A=0A=0A=0A________________ ________________=0A From: "berkut13@berkut13.com" <berkut13@berkut13.com> =0ATo: aeroelectric-list@matronics.com =0ASent: Sunday, December 22, 2013 8 :59 PM=0ASubject: Re: AeroElectric-List: Any know is there a typical faliur e mode for Soild State Relays=0A =0A=0A=0A =0AThat=99s what I did...l ess weight, less space, less environmental issues, =0Acleaner operation (no contact bounce), etc. =0A=C2-=0Ahttp://www.berkut13.com/berkut50.htm#SSR =0A=C2-=0AIf you hydraulic system is anything like mine, you should also be used the =0Asnap action hydraulic pressure switches.=0A=C2-=0AGood luc k,=0AJames=0ABerkut/Race 13=0Awww.berkut13.com=0AFacebook: Berkut13=0A=C2 -=C2-=0AFrom: Jeffrey Skiba =0ASent: Sunday, December 22, 2013 10:27 AM =0ATo: aeroelectric-list@matronics.com =0ASubject: AeroElectric-List: Any k now is there a typical faliure mode =0Afor Soild State Relays=0A=C2- Any =0Aknow is there a typical failure mode for Solid State =0ARelays?=0A =C2 -=0ALike =0Ado they typically fail OPEN ??? or do they Typical fail CLOSE D (just like =0Asometimes of a typical mechanical relay that the points wel d together or the =0Aspring fails ?)=0A =C2-=0AI =0Aam considering using solid state relays to replace mechanical relays but do not =0Aknow if the s sr has a failure mode worse than them. =0A =C2-=0AI =0Ahave attached one relay I found thus far to possibly replace a hydraulic motor =0Acontactor f or a landing gear pump.=0A =C2-=0AThanks =0Ain advance and HAPPY HOLIDAYS !=0A________________________________=0A =0ANo virus found in this =0Amess -======================== ============




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