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user9253
Joined: 28 Mar 2008 Posts: 1924 Location: Riley TWP Michigan
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Posted: Sun Feb 24, 2019 5:20 pm Post subject: ENDURANCE BUS ALTERNATIVE |
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If the main purpose of the Endurance Bus is to reduce pilot workload in case the
alternator fails, then there is an alternative solution. Arrange the switches in
order of importance and color code them. When the alternator fails, the pilot
finishes his coffee, then starts shutting off switches on the far right and
works his way to the left. Several switches could be shut off with one motion
of the hand. A physical barrier or open space could separate essential
switches from non-essential ones. The advantage of this architecture is a
simplified electrical system, only one bus, no diodes, and yes, even reduced
pilot workload. She will not have to remember which loads are connected to
which bus. Some loads could be essential or not depending on the flight
conditions. Just turn them on or off as needed.
_ What about the backup-electrical-current path that the E-Bus relay
provides? No problem, just install a 40 amp automotive relay (disabled
during starting) in parallel with the battery contactor. The master switch
would have 3 positions: down-off, center-relay, up-contactor.
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_________________ Joe Gores |
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henador_titzoff(at)yahoo. Guest
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Posted: Mon Feb 25, 2019 4:53 am Post subject: ENDURANCE BUS ALTERNATIVE |
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Joe,
Your description of one common bus with multiple switches to select singular on and offs is brilliant! It assumes that one has plenty of time to determine what to turn on and off, but it's typically true in light emergencies such as an alternator failure. I'm not sure what you mean by the "backup-electrical-current" path that the E-bus relay provides. Can you please explain it?
I'm not saying that the E-bus concept is a failure. It's being used successfully today in many experimentals and when certain failure modes occur, I'm sure it validates itself. From a pilot's point of view, it's a much simpler interface, and simplicity is good in dire emergencies.
Henador Titzoff
On Sunday, February 24, 2019, 8:37:01 PM EST, user9253 <fransew(at)gmail.com> wrote:
--> AeroElectric-List message posted by: "user9253" <fransew(at)gmail.com (fransew(at)gmail.com)>
If the main purpose of the Endurance Bus is to reduce pilot workload in case the
alternator fails, then there is an alternative solution. Arrange the switches in
order of importance and color code them. When the alternator fails, the pilot
finishes his coffee, then starts shutting off switches on the far right and
works his way to the left. Several switches could be shut off with one motion
of the hand. A physical barrier or open space could separate essential
switches from non-essential ones. The advantage of this architecture is a
simplified electrical system, only one bus, no diodes, and yes, even reduced
pilot workload. She will not have to remember which loads are connected to
which bus. Some loads could be essential or not depending on the flight
conditions. Just turn them on or off as needed.
_ What about the backup-electrical-current path that the E-Bus relay
provides? No problem, just install a 40 amp automotive relay (disabled
during starting) in parallel with the battery contactor. The master switch
would have 3 positions: down-off, center-relay, up-contactor.
--------
Joe Gores
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user9253
Joined: 28 Mar 2008 Posts: 1924 Location: Riley TWP Michigan
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Posted: Mon Feb 25, 2019 7:28 am Post subject: Re: ENDURANCE BUS ALTERNATIVE |
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Thanks for your reply Henador. Most of Bob's "Z" figures have an Endurance
Bus which can receive electrical power from the battery via two possible paths.
Using Z-13/8 as an example, the normal path is from the battery, through the
battery contactor and though a diode to the Endurance Bus. The alternate
current path is from the battery bus, through the E-Bus relay to the Endurance
Bus. There is certainly nothing wrong with Bob's architecture. In fact, many
builders are better off using one of his proven wiring diagrams instead of
designing their own. Some builder architecture has a hidden flaw that only
becomes apparent under certain conditions. The more complicated the
electrical architecture is, the greater the chance of pilot error when the mind
goes blank in in a emergency.
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