Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.229]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with SMTP id AAA10624 for ; Tue, 13 Oct 1998 07:50:22 -0400 Message-Id: <3.0.3.32.19981013074941.00ae72d4@olsusa.com> Date: Tue, 13 Oct 1998 07:49:41 -0400 To: lancair.list@olsusa.com From: (by way of Marvin Kaye ) Subject: Re:Fuel level sensors X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Jim Frantz wrote about float switches not being good because they are affected by G-loads and turbulence causing the float to probably sink. Actually that isn't the case. The same centripetal force acting on the float as acting on the surrounding fluid not only canceling any effect but multiplying the buoyancy of the float by the increase in 'g'. So if it floats, it'll float even better under higher g's. If it sinks, it'll sink harder under g's. In fact the The better way to think of it is simply by comparing densities (which is unaffected by gravity because it's MASS divided by volume). I've got 3 float switches in my tank (Matteson is the mfgr - same as in Aircraft Spruce) the lowest (at about the half mark) to turn on pumps, the middle to turn off pumps and the highest to signal a light. I also have a both wing tanks plumbed through a fuel flow transducer feeding a panel gage so that I will know if flow to the header tank isn't nominal. I'm planning to use the VM-1000 system to warn of low fuel should a pump or relay fail. The Lancair Avionics people did the design and put a nice little relay and harness package together. But I didn't think about what I would do if a relay fails and I get the warning but I only have a few gallons left. I'll have to think that failure mode through. Thanks for the warnings. Ed de Chazal Rochester Michigan