Return-Path: Received: from cdihost.cdicorp.com ([207.79.152.5]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with SMTP id com for ; Fri, 28 Jul 2000 12:58:39 -0400 Received: from HQ-EDI by cdihost.cdicorp.com via smtpd (for ns1.olsusa.com [205.245.9.2]) with SMTP; 28 Jul 2000 17:05:03 UT Received: from cdim-pts-mail.cdicorp.com (CDIM-PTS-MAIL [172.17.131.3]) by hq-edi.cdicorp.com with SMTP (Microsoft Exchange Internet Mail Service Version 5.5.2650.21) id PDLSWMJF; Fri, 28 Jul 2000 13:05:01 -0400 Received: by CDIM-PTS-MAIL with Internet Mail Service (5.5.2650.21) id ; Fri, 28 Jul 2000 13:05:01 -0400 Message-ID: From: "Rumburg, William" To: "'lancair.list@olsusa.com'" Subject: Backup Electrical Power Date: Fri, 28 Jul 2000 13:04:51 -0400 X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> > The thought that backup electrical power is overly complicated or > unreliable probably scares some builders away from a modern all-electric > plane. The backup electrical system on my Lancair is uncomplicated and > reliable. It can be fully tested on the ground at any time by simply > switching it on and letting it run the connected loads for a few hours. > Whether or not you like my overall system, you may want to adopt some > features, such as the battery's location and installation method. > The entire system consists of only three components: > 1. A backup battery installed on the right side of the nose gear tunnel, > forward of the rudder pedals (check to see how much room is available in > this area on your aircraft, there's enough to accomodate at least a > medium-size battery). > The battery need not be physically large. Should backup power ever be > necessary, it will be required to operate critical loads totaling only > 5-10 amps for 2 to 3 hours at most. Even if you had enough gas onboard to > continue flying for a longer time, it would be foolish to press your > limits. > By definition the A-H (amper-hour) capacity of a battery is it's ten hour > capability at rated amperes. A 12 A-H battery, for example, will deliver > 12 amperes continuously for at least ten hours, if it's fully charged. I > installed a Concorde RG-12 as a backup four years ago, but it's no longer > manufactured (A Lifeline GPL-1300 (marine grade) is their current > equivalent). Now, I'm using a Sears Die-Hard. There are many batteries you > could choose, but I would go with a modern RG (recombident gas) sealed > lead-acid type > To install it, I first fastened a 6" length of 2" x 2" aluminum angle > (purchased at a local hardware) to the side of the nose gear tunnel > (approximately 4" above the subfloor) using 3/16 flat head aluminum pop > rivets. In order to successfully "pop" the rivets and for load spreading, > use 3/16" area washers (AN370-16) on the inside of the nose gear tunnel. > The battery then rests on the aluminum angle and is secured against the > tunnel by means of a 1" wide nylon strap (purchased at a local marine > supply and made for the purpose). The strap is supplied with two small > stainless steel brackets to allow it to wrap around the battery. Attach > the brackets to the nose gear tunnel forward and aft of the battery, again > using pop rivets and area washers. > > 2. A power diode connecting the backup battery to the main (charging) bus. > It has two functions: > a.) Provides a path for charging current from the main bus. > b.) Provides isolation for the backup battery (preventing backup > current from flowing back to the main bus). > I used a conventional silicon power diode, which has an inherent voltage > drop of approximately 0.7 V DC in the forward direction. This lowers > charging voltage to the backup battery and if your main bus voltage is > less than 14.0 V DC, the result would be less than full charge on the > backup battery (Concorde states that their testing shows that as little as > 13.5 V DC will maintain full charge on a lead-acid battery). However, as > Ed Armstrong just posted, a Schottky diode, which has a voltage drop > ranging from 0.2 V to 0.3 V (at the charging currents we would experience) > can be used, thus eliminating the possibility of undercharging the backup > battery due to low voltage. By the way, I contacted VMS and was informed > that the VMS 1000 accuracy is +/- 1% for all instruments, which equates to > 0.14 V at 14.0 V DC for the voltage instrument. > As pointed out by Jim Frantz, another possible fault would be shorting of > the diode, thus connecting the backup directly to the main bus, which > would drain it in a relatively short time. Although such an occurance was > reported by George Stevenson in the LNN several years ago, I believe this > to be a rare event provided that the diode is suitably rated. > > 3. A DPDT (double pole-double throw) switch rated at least 10A. This is > about as simple and reliable an electrical device as exists. > It has three sets of terminals. > a) The center terminal is wired to the device(s) requiring backup > power. > b) Power from the main bus is connected to one outer terminal. > c) Power from the backup battery is connected to the other outer > terminal. > Whichever position the switch is in determines whether power is fed to the > device (ignition, gyros, etc.) from the main bus or the backup battery. > Admittedly, it would be impractical to connect several devices (wires) to > a terminal. I connected directly to the switch, but you could make an > "essential" bus for connection of several devices. > > Bill Rumburg > N403WR (Sonic bOOm) > >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>