Fire detection, suppression, reaction
This discussion of fire detection and suppression has me thinking (dangerous!) What follows is my 2 cents, and worth every penny.
I found this at Radio Shack:
http://www.radioshack.com/product/index.jsp?productId=2102788
I'm thinking of connecting one to my Dynon D180 contact inputs. I would get a warning if it opened. I was thinking the best place to put it would be on the fuel line from firewall fuel pump (IO-360). Several could be placed around the engine compartment in series if desired.
First, I think the probability of an engine fire is relatively low if in construction we use the proper materials and techniques (steel fittings, fire sleeve, non-rigid lines, pre-flight and periodic inspections, etc) It would be an interesting exercise to determine through NTSB reports how many fires (engine or electrical) have occurred in both certified and experimental aircraft. Intuitively, I think electrical fires are probably more prevalent.
Secondly, if an engine or electrical fire does occur we need to:
1) Detect
2) React
a. Confirm
b. Suppress (Remove fuel, oxygen, ignition source)
c. Land and get out
Time is our enemy here. So detection seems like a good first step. This would be followed by protection (firewall insulation, chemical suppression, smoke hood, parachute, transporter beam.....). Following protection, we have emergency procedures (fuel off, electrical off, airspeed, etc.)
To summarize we need to prevent, detect, react, and buy time. Although a firewall forward halon suppression certainly fits in here, methinks it is not the panacea. I noted in some of the installation photos that a halon fire suppression system was being fed by thin walled aluminum lines. How long would they last?
Time to stop rambling here and ramble out to the shop....
Don