emuyshondt
Well Known Member
I'm helping a friend build an RV6A. I believe the plans call out for a 12V electrical system. However there seem to be a number of components that use a 24V supply. Is there an advantage to implementing one voltage level over the other? If we build a 12V system per plans, is it acceptable to use some sort of DC to DC converter to supply those devices that require 24V? For example, we are looking at a 24V used heated Pitot tube. There may be other components that require one or the other voltage level. In case it makes a difference, we intend the plane to be certified for IFR even if we don't intend on flying in severe weather conditions.
I'd appreciate any thoughts on this subject. While we have engineering degrees to understand the flow of electrons, we don't know what the trade-offs are in terms of availability of components, safety, and practicality in an aviation environment.
Henry
I'd appreciate any thoughts on this subject. While we have engineering degrees to understand the flow of electrons, we don't know what the trade-offs are in terms of availability of components, safety, and practicality in an aviation environment.
Henry