kontiki99
Electrical
- Feb 16, 2006
- 510
All,
I'm trying to understand typical voltage stability, noise and "spike voltage" characteristics typically found on GA aircraft 14V and 28V engine driven rectified alternator power systems.
Maybe the characteristics of an old 1940s automobile would do?
I'm looking into suitability of DO-160 testing and the basis for aircraft owner concerns about voltage spikes and the need for avionics bus master switches.
Thanks
My posts reflect my personal views and are not in any way endorsed or approved by any organization I'm professionally affiliated with.
I'm trying to understand typical voltage stability, noise and "spike voltage" characteristics typically found on GA aircraft 14V and 28V engine driven rectified alternator power systems.
Maybe the characteristics of an old 1940s automobile would do?
I'm looking into suitability of DO-160 testing and the basis for aircraft owner concerns about voltage spikes and the need for avionics bus master switches.
Thanks
My posts reflect my personal views and are not in any way endorsed or approved by any organization I'm professionally affiliated with.