Hey Judge,
Not to cause you more grieve for you, can you explain in detail as to why not needed, (servo failure)? If you would like you can pm me.
Thank you for sharing your thoughts... no offense taken... LOL
Jim
I have had two instances of a servo failing in flight, one was in a 2 servo per aileron planes, the other was a simple servo failing. The 2 aileron servo per aileron incident fried both servos in the left wing. It was a challenge to get it down due to how it was flying. I had a simple dual battery/switch setup which proved to be up to the challenge. The other servo failure locked up the rudder a bit off center. Lost a gear and it fried in flight. Still able to land as my power system had no issues. So at least for me, the extreme case of servo failure did not cause a power issue for me.
Beyond that, I have inquired about whether the service folks have ever seen a receiver that failed due to electrical overload (voltage or amp load). The answer was no. So seems like this is not an issue either.
Using the basic principles of Ohm's law and using the references available on the Internet to calculate wire loss/voltage drop at various voltages and loads for a specific wire run I have been able to demonstrate to my own satisfaction that a typical wire type (20 or 22 AWG) used in our planes is more than up to the task.
I have also proven to myself by doing various tests that connectors are the weakest point in the power system, which is why I try to minimize how many connections I have between the battery and the servo. I solder wires to remove connectors, or make up custom lengths.
The new receiver that is the topic of this thread solves the one major potential of a weak point in the system by providing large gauge wire directly into the receiver without any switches in between Switches are the other major weakness. I have moved to using solid state magnetically actuated switches and this new RX removes the need for any switch.
When I look at any new device I ask what problem does this solve? I then try to determine if the problem is a real one in the first place. For most of the power distribution systems I have not seen that they solve a true issue.
I use the on board voltage telemetry to track my in flight voltage. After each flight I look to see what the low voltage was (that is saved on the display on my TX). I rarely have seen more than 0.5 volts difference. That is well below the threshold that I can perceive as a change in performance of the plane.
One final thing I do sometimes is to pop that hatch as soon as I can after landing. I feel the wires and connectors. If they are no warmer than ambient, I know then that I am not losing anything by excessive resistance in the wires/etc.
So that is my thought process. It has been a proven process for me in nearly 2 decades of flying larger/complex planes.