Today's Message Index:
----------------------
 
     1. 10:45 AM - Re: Fusible Link for Lightspeed Ignition (Robert L. Nuckolls, III)
     2. 11:00 AM - Speaking of Lessons Learned (Robert L. Nuckolls, III)
 
 
 
Message 1
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| Subject:  | Re: Fusible Link for Lightspeed Ignition | 
      
      At 01:04 PM 3/28/2023, you wrote:
      >I am using dual lightspeed ignitions on my project. Lightspeed's 
      >instructions specify using 18ga shielded wire, the shield used as 
      >the ground return and wiring directly from the battery to a 7.5 amp 
      >panel circuit breaker. I want to use a fusible links to protect the 
      >wires from the battteries to the circuit breaker. I acquired 14 
      >gauge shielded wire. My plan was to separate the conductor from the 
      >shield, use an 18ga conductor for the fusible link and solder an 18 
      >ga ground lead to the shield. The problem I am having is separating 
      >the center wire from the shield. I end up breaking 30 to 50% of the 
      >tiny shield strands while separating the center conductor. The 
      >resulting connection is less than ideal both electrically and 
      >security wise. I'm thinking a better method would be to roll shield 
      >back over the outer insulation and use a solder sleeve with an 18ga 
      >pigtail. I have made a couple practice connections and they seem 
      >very secure, especially when the whole joint is reinforced with some 
      >additional heat shrink. Does this seem like an okay approach? It's a 
      >very important termination.
      
          I've had numerous conversations with Klaus about
          his power delivery suggestions over the years . . .
          the last being while witnessing some tests on
          his product during an inquiry as to cause of
          a LA-IV crash out in CA.
      
      https://tinyurl.com/52kbwra8
      
          This case was intently interested in the
          performance of those 'very important terminations'.
      
          The engine died in an approach to landing
          and ended up on the rocks. Both fuses feeding
          the pair of ignition systems were open.
          As it turns out, the system was DESIGNED
          to fail as explained in analysis documentation.
          The project also showed lapses in
          choice of materials and fabrication
          processes.
      
          Which brings me to this assertion: Failure
          of your ignition system(s) will most
          likely be a product of poor design and/or
          installation error. The accident cited
          above was a demonstration of BOTH of
          these effects.
      
          Klaus' recommendations are not 'wrong' . . .
          just unnecessary . . . and they ignore
          a century of lessons learned in the design
          and fabrication of reliable aircraft
          systems.
      
          Others have cited some of my writings
          on the topic of Lightspeed systems. But
          in a nutshell, the use of shielded wire
          connected directly to battery(ies) driving
          panel mounted breakers is both unnecessary
          and contrary to a 747-load of lessons
          learned.
      
          Those ignition systems will draw no more
          than 2.5A at red-line rpm. Each one would
          run happily fed by 5A fuse (from either a
          hot battery or multi-path fed engine bus)
          and 20AWG wire (for mechanical robustness,
          not current draw).  You have TWO systems,
          each of which will run the engine. They
          are pre-flight tested. If some failure takes
          out a fuse (or opens a breaker), being able
          to restore the power path is of exceedingly
          low value . . . it will just re-open due
          to the fault that caused the first event.
      
          You can confidently skip the shielded wire
          and crew-monitored circuit protection
          while exploiting benefits of legacy-
          proven design and fabrication techniques.
      
      
         Bob . . .
      
                          ////
                         (o o)
          ===========o00o=(_)=o00o========
          < Go ahead, make my day . . .   >
          < show me where I'm wrong.      >
          ================================
      
          In the interest of creative evolution
          of the-best-we-know-how-to-do based
          on physics and good practice.
      
Message 2
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| Subject:  | Speaking of Lessons Learned | 
      
      
      Electrical 'bonding' of components in aircraft
      is accomplished for some combination of three
      requirements (1) reliable connection of a
      device to power ground, (2) mitigation of
      radio frequency interference and/or (3)
      managing the effects of electro-static
      discharge (ESD).
      
      Here's a good example of failure to manage
      ESD back before we'd been schooled in
      'lessons learned' . . . 1929
      
      https://youtu.be/LR02blpCJMk
      
      Some pretty cool detective work here . . .
      
      
         Bob . . .
      
                          ////
                         (o o)
          ===========o00o=(_)=o00o========
          < Go ahead, make my day . . .   >
          < show me where I'm wrong.      >
          ================================
      
          In the interest of creative evolution
          of the-best-we-know-how-to-do based
          on physics and good practice.
      
 
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