Avionics Master
Posted: Mon Jul 06, 2009 1:25 pm
To fit a relay, or not to fit a relay : that is the question.
All (permit) aircraft wiring diagrams I've ever seen seem to just have a switch from the main bus to the avionics bus, so that the avionics can be isolated for startup to avoid the nasties involved in the operation of the starter (and, to a lesser extent, turning on the generator).
I've discovered that some certified aircraft use a relay, and not just to handle a heavier load than the switch could cope with.
It appears the relay is normally closed (connected) and switching the avionics master switch to OFF actually energises the relay, DISconnecting the avionics!
The idea is if the avionics master switch breaks then the relay remains closed/connected, feeding the avionics with power.
Don't know about anybody else, but I've seen far more problems with relays than I ever have with switches: more external connections to fail, dirty contacts inside, cooked coils, sticky pivots, to name but a few. To put a less reliable piece of kit (relay) in to guard against failure of a more reliable piece (switch) seems barmy.
Also makes me wonder about the "starting an engine on a cold winter day" situation. Turn the key, starter turns about fast enough to start the engine but the voltage fluctuates so avionics relay clicks in and out. This would not only feed 'dirty' power to the avionics (the very thing the avionics master is supposed to prevent!), but the flicking of the relay coil and contacts is going to make that power feed even 'dirtier'.
Think I may have just answered my own question, but what do people recommend:
- a relay installation as described above
- a more conventional use of a relay just to offset sheer current requirements of a complex avionics stack (2 x radios, GPS, xponder, intercom, TCAS etc)
- a nice meaty (10-20 amp?) switch doing the whole job.
All (permit) aircraft wiring diagrams I've ever seen seem to just have a switch from the main bus to the avionics bus, so that the avionics can be isolated for startup to avoid the nasties involved in the operation of the starter (and, to a lesser extent, turning on the generator).
I've discovered that some certified aircraft use a relay, and not just to handle a heavier load than the switch could cope with.
It appears the relay is normally closed (connected) and switching the avionics master switch to OFF actually energises the relay, DISconnecting the avionics!
The idea is if the avionics master switch breaks then the relay remains closed/connected, feeding the avionics with power.
Don't know about anybody else, but I've seen far more problems with relays than I ever have with switches: more external connections to fail, dirty contacts inside, cooked coils, sticky pivots, to name but a few. To put a less reliable piece of kit (relay) in to guard against failure of a more reliable piece (switch) seems barmy.
Also makes me wonder about the "starting an engine on a cold winter day" situation. Turn the key, starter turns about fast enough to start the engine but the voltage fluctuates so avionics relay clicks in and out. This would not only feed 'dirty' power to the avionics (the very thing the avionics master is supposed to prevent!), but the flicking of the relay coil and contacts is going to make that power feed even 'dirtier'.
Think I may have just answered my own question, but what do people recommend:
- a relay installation as described above
- a more conventional use of a relay just to offset sheer current requirements of a complex avionics stack (2 x radios, GPS, xponder, intercom, TCAS etc)
- a nice meaty (10-20 amp?) switch doing the whole job.