AeroElectric-List Digest Archive

Thu 05/23/13


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 09:39 AM - Re: Z13/8 all electric airplane (eschlanser)
     2. 11:19 AM - Re: Re: Z13/8 all electric airplane (Robert L. Nuckolls, III)
     3. 04:08 PM - Re: Z13/8 all electric airplane (eschlanser)
     4. 05:42 PM - Re: Re: Z13/8 all electric airplane (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 09:39:09 AM PST US
    Subject: Re: Z13/8 all electric airplane
    From: "eschlanser" <eschlanser@yahoo.com>
    Bob, Instead of a polyswitch in the PM alternator circuit, may I suggest using the Linear OVP module from PerhelionDesign.com? http://www.periheliondesign.com/lovm.htm Disclaimer: I have no connection with the company except for using the LOVP instead of crowbar OVM/RELAY combinations in both main alternator (IR) and aux alternator (SD8) circuits in my project's Z-13-8 derived electrical system. I had considered using polyswitchs. True, the LOVP module is way more expensive than polyswitches. But in return for the cost, the engineering work has been done. It has provision for an Led lite annunciator and a reset feature. I don't understand all the engineering, but it seems to me that a thermally activated polyswitch is not under the pilot's control. After cooling, wouldn't it keep trying to reset itself? I'd like to see how you would use the Perhelion LOVP in Z13/8 as I struggled with the wiring. Eric S. Z13/8 in a W-10 Tailwind/O-320 project [/quote] Actually, I've been contemplating replacement of the breaker in that drawing with a polyswitch. Given the low current demands for driving the relay coil, this would be an excellent place to incorporate a polyswitch. I'm wrestling with annunciation issues. A popped breaker is, not a great annunciator but it's not bad. If we 'hide' a tripped condition by going solid state polyfuse, then perhaps some form of OV TRIP indication is called for. I've got some ideas and will incorporate the most elegant configuration into the Z-figures that control PM alternators with the RELAY/OVM combination. Bob . . .[/quote] Read this topic online here: http://forums.matronics.com/viewtopic.php?p=401210#401210


    Message 2


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    Time: 11:19:28 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Z13/8 all electric airplane
    At 11:37 AM 5/23/2013, you wrote: > >Bob, > > Instead of a polyswitch in the PM alternator circuit, may I > suggest using the Linear OVP module from PerhelionDesign.com? > http://www.periheliondesign.com/lovm.htm That is one of many ov management options used in vehicular DC power systems . . . > I had considered using polyswitchs. True, the LOVP module is way > more expensive than polyswitches. But in return for the cost, the > engineering work has been done. It has provision for an Led lite > annunciator and a reset feature. I don't understand all the > engineering, but it seems to me that a thermally activated > polyswitch is not under the pilot's control. After cooling, > wouldn't it keep trying to reset itself? The polyswitch does not go open, only to a high resistance state which keeps drawing enough current to STAY in that high resistance state. This means that fault current that would put wiring at risk is limited to some acceptably low value. In the case OV management for the PM alternator, the NORMAL current that holds the relay closed will not drip the polyswitch. A dead short OV module connected across the relay would burn wires unless a fuse, breaker or polyswitch did not respond to limit the current. Fuses and breakers take the current to zero . . . the polyswitch takes it to some low, non-hazardous value. Either philosophy is consistent with Z-13/8 design goals. In the interim, I've once again backed off the incorporation of the polyswitch. NOT because it fails to function as advertised but because it's designed to mount to an ECB. Artful incorporation of the polyswitch into Z-13/8 PM alternator control calls for mounting it into some fabricated assembly. I looked at a surface mounted device on an ECB along with resistors to drive a 'tripped' indicator light. Too much monkey motion . . . so my track record is still intact. Since my first introduction to the realm of inrush limiters and polyfuses at LearJet in 1980, I've not discovered an elegant way to incorporate these critters into airframe system wiring. They work fine as a component INTERNAL to a black box. > I'd like to see how you would use the Perhelion LOVP in Z13/8 as I > struggled with the wiring. You use it per the installation instructions. It's wired in series with the device that you want to shut down in the event of an ov condition. The point of Z13/8 is to mitigate "struggling". The drawing is not intended to be the epitome of systems but simply an elegant solution that meets design goals for the system. There are certainly useful variations on the theme that can and should be considered if the drawing as-presented fails to meet some other design goal. Assuming you perceive a need to depart from the suggested wiring, what new or overlooked design goal needs attention? In other words, what feature of Z-13/8 drives your willingness/need to "struggle"? What changes are you considering and what is the anticipated return on investment for the change? Bob . . .


    Message 3


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    Time: 04:08:51 PM PST US
    Subject: Re: Z13/8 all electric airplane
    From: "eschlanser" <eschlanser@yahoo.com>
    Bob, Thank you for the education on the polyswitch. Once again, you cleared up an electrical design for me. Z13/8 is awesome. The only reason I changed anything in Z13/8 was due to the advertising for the LOVP. The marketing sold me on it. However, the LOVP has more wires and connections than the crowbar OV, making it more involved to incorporate. For this first timer, anything electrical is a struggle. I should have built the absolute simplest system, Z11, first. Then, I could have worked my way up to Z13/8 after getting some practical experience in the art. Attending one of your seminars and studying the AEC have been great exposure to the formal discipline of aircraft electrical science. Thanks again for so generously sharing your experience, Eric S. [/quote] Assuming you perceive a need to depart from the suggested wiring, what new or overlooked design goal needs attention? In other words, what feature of Z-13/8 drives your willingness/need to "struggle"? What changes are you considering and what is the anticipated return on investment for the change? Bob . . .[/quote] Read this topic online here: http://forums.matronics.com/viewtopic.php?p=401260#401260


    Message 4


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    Time: 05:42:05 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Z13/8 all electric airplane
    At 06:01 PM 5/23/2013, you wrote: > >Bob, > > Thank you for the education on the polyswitch. Once again, you > cleared up an electrical design for me. > > Z13/8 is awesome. The only reason I changed anything in Z13/8 was > due to the advertising for the LOVP. The marketing sold me on it. > However, the LOVP has more wires and connections than the crowbar > OV, making it more involved to incorporate. > > For this first timer, anything electrical is a struggle. I should > have built the absolute simplest system, Z11, first. Then, I could > have worked my way up to Z13/8 after getting some practical > experience in the art. > Attending one of your seminars and studying the AEC have been > great exposure to the formal discipline of aircraft electrical science. > >Thanks again for so generously sharing your experience, You're most welcome . . . it's what we do. Without a doubt, the LVOP performs as advertised. My best counsel is to set system desing goals and then work for lowest parts count, weight and cost of ownership. I fiddled with a little different technique for incorporating the Polyswitch into the PM alternator OV protection . . . even came up with a little ECB to carry a surface mount device along with the companion resistors for trip annunciation. It would have been a new product to offer . . . Problem was that it applied to a limited number of total situations for replacing a CB . . . namely the disconnect relay for a PM alternator. The 9024 4-function module is slated to replace crowbar ovm in the control of PM alternators. So to spend $resources$ to spruce up a low-volume application slated to be obsolete just didn't make sense. Getting on the List and standing your own design goals against recipes for success is the very best way to strive for the elegant solution. It's a collegial service I enjoyed during my tenures at Electro-Mech and Beech. No reason it shouldn't work here too. Bob . . . Bob . . .




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