Return-Path: Received: from smtp5.gateway.net ([208.230.117.249]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 26 Aug 2000 16:43:52 -0400 Received: from oemcomputer (1Cust204.tnt1.coeur-dalene.id.da.uu.net [63.27.107.204]) by smtp5.gateway.net (8.9.3/8.9.3) with SMTP id QAA00434 for ; Sat, 26 Aug 2000 16:50:27 -0400 (EDT) Message-ID: <000c01c00fa0$c8a03360$cc6b1b3f@oemcomputer> Reply-To: "dfs" Reply-To: lancair.list@olsusa.com From: "dfs" To: "Lancair List" Subject: Re: Circuit Breakers for Hydraulic Pump Relays and run-away trim Date: Sat, 26 Aug 2000 14:00:46 -0700 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> A simple method of creating a run-away-proof trim system is to use what the Human Factors wonks at Rockwell referred to as a (excuse me) "Dead Man Switch" (DMS). This is a spring-loaded switch that in it's normal un-actuated position, removes ALL power to a critical circuit or control system. This is in addition to any other control actuation, like a trim switch. In the case of a trim circuit, the DMS could be a small push-button or trigger switch on the stick grip that needed to be squeezed to allow the trim control to function. This wouldn't impose very much additional work-load on the pilot (probably become second nature in no time at all) and would allow almost instant reaction time to kill the trim system by merely releasing the switch. Further, a potential run-away condition could be recognized as soon as the DMS was actuated, since the trim would start running before the trim toggle switch was touched. If a run-away condition was detected, just keeping your finger off the DMS until you pulled the breaker makes it a non-event. If ALL power to the trim circuit is removed by the DMS (similar to pulling the breaker) it can't continue to run away. Also, during normal operations, inadvertantly depressing the DMS without diddling the trim switch would be of no consequence unless a run-away failure condition existed. This concept was used in the rear cockpit of the B-1 where a built-in, computer controlled aircraft test system could actually turn various systems under test on and off, and which could include the movment of control surfaces. To run these tests, (ground tests only, active tests were locked out in flight) a test person had to manually hold the DMS actuated while potentially dangerous (to other personnel) tests were running. To kill the system if necessary, the test guy just released the switch. Simple, neat and effective. Dan Schaefer >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>