Return-Path: Received: from [12.10.147.52] (HELO utmcmail.utmc.com) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 744179 for flyrotary@lancaironline.net; Fri, 18 Feb 2005 08:57:16 -0500 Received-SPF: none receiver=logan.com; client-ip=12.10.147.52; envelope-from=Grant.Schemmel@Aeroflex.com Received: from mcwolf.utmc.utc.com ([10.1.1.1]) by utmcmail.utmc.com with Microsoft SMTPSVC(5.0.2195.6713); Fri, 18 Feb 2005 06:56:10 -0700 Received: from pony.utmc.utc.com(172.24.100.19) by mcwolf.utmc.utc.com via csmap id a4261e44_81b2_11d9_867f_00304811acd7_13437; Fri, 18 Feb 2005 06:40:24 -0700 (MST) Received: by pony.utmc.utc.com with Internet Mail Service (5.5.2655.55) id ; Fri, 18 Feb 2005 06:56:19 -0700 Message-ID: From: "Schemmel, Grant" To: 'Rotary motors in aircraft' Subject: RE: [FlyRotary] Re: Digital Fuel Monitoring System Date: Fri, 18 Feb 2005 06:56:19 -0700 MIME-Version: 1.0 X-Mailer: Internet Mail Service (5.5.2655.55) Content-Type: multipart/alternative; boundary="----_=_NextPart_001_01C515C1.9F1B8720" Return-Path: Grant.Schemmel@Aeroflex.com X-OriginalArrivalTime: 18 Feb 2005 13:56:10.0722 (UTC) FILETIME=[9A0B2420:01C515C1] This message is in MIME format. Since your mail reader does not understand this format, some or all of this message may not be legible. ------_=_NextPart_001_01C515C1.9F1B8720 Content-Type: text/plain; charset="ISO-8859-1" Hi Ed, I wouldn't sweat the "resistor on legs" issue too much, it only becomes a vibration issue with parts that have a large mass. I work for a company that builds space grade circuit cards, and used to work on PT6 fuel controls when I worked for Hamilton Standard, so I've seen typical construction for this kind of application. If you are worried about axial leaded components, mount them close to the circuit card and put a dab of epoxy under them for bonding. On an aside, I would appreciate a photo of your board emailed direct, as my workplace blocks all jpegs. Thanks Grant Schemmel -----Original Message----- From: Ed Anderson [mailto:eanderson@carolina.rr.com] Sent: Friday, February 18, 2005 5:57 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Digital Fuel Monitoring System Geez, Finn, I was unaware that there was a "protocol" for resistor sizes on PC boards. Seriously, is there some reason (vibration?) for forcing resistors all the way to the board or is it just "esthetics?". Ed A ----- Original Message ----- From: Finn Lassen To: Rotary motors in aircraft Sent: Thursday, February 17, 2005 11:06 PM Subject: [FlyRotary] Re: Digital Fuel Monitoring System Nice. I assume those resistors are just temporary until you get hold of smaller ones that can actually rest on the PCB rather than hanging in their legs? I know it's not flight critical, but still... Finn Ed Anderson wrote: Here are a couple of photos of my homebrew digital fuel monitoring system, I have mentioned in the past (seems like I've been working on it forever). Got the PC board in today and got it mostly populated with the components. It will sit in a 2 1/4" instrument case with the LCD extending out past the boundary of the case. I plan on trying some vacuum molding of thin ABS plastic to form a attractive front cover. The front panel shows the LCD display screen as well as the push buttons for loading fuel, setting alarms and selecting which screen you wish to display. The center shaft controls the LCD backlite so it will be visible either in day or night. Hopefully, I have designed and constructed the board properly (my first microcomputer/controller board) and if so, then the software (which I have completed) will be loaded and it will be installed in the aircraft for testing. I certainly plan on having it installed for Sun & Fun. Ed ------_=_NextPart_001_01C515C1.9F1B8720 Content-Type: text/html; charset="ISO-8859-1"
Hi Ed,
 
I wouldn't sweat the "resistor on legs" issue too much, it only becomes a vibration issue with parts that have a large mass.  I work for a company that builds space grade circuit cards, and used to work on PT6 fuel controls when I worked for Hamilton Standard, so I've seen typical construction for this kind of application.  If you are worried about axial leaded components, mount them close to the circuit card and put a dab of epoxy under them for bonding.
 
On an aside, I would appreciate a photo of your board emailed direct, as my workplace blocks all jpegs.
 
Thanks
 
Grant Schemmel
-----Original Message-----
From: Ed Anderson [mailto:eanderson@carolina.rr.com]
Sent: Friday, February 18, 2005 5:57 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Digital Fuel Monitoring System

Geez, Finn, I was unaware that there was a "protocol" for resistor sizes on PC boards.  Seriously, is there some reason (vibration?) for forcing resistors all the way to the board or is it just "esthetics?".
 
Ed A
----- Original Message -----
Sent: Thursday, February 17, 2005 11:06 PM
Subject: [FlyRotary] Re: Digital Fuel Monitoring System

Nice.

I assume those resistors are just temporary until you get hold of smaller ones that can actually rest on the PCB rather than hanging in their legs? I know it's not flight critical, but still...

Finn

Ed Anderson wrote:
Here are a couple of photos of my homebrew digital fuel monitoring system, I have mentioned in the past (seems like I've been working on it forever).  Got the PC board in today and got it mostly populated with the components.  It will sit in a 2 1/4" instrument case with the LCD extending out past the boundary of the case.  I plan on trying some vacuum molding of thin ABS plastic to form a  attractive front cover.
 
The front panel shows the LCD display screen as well as the push buttons for loading fuel, setting alarms and selecting which screen you wish to display.  The center shaft controls the LCD backlite so it will be visible either in day or night.
 
Hopefully, I have designed and constructed the board properly (my first microcomputer/controller board) and if so, then the software (which I have completed)  will be loaded and it will be installed in the aircraft for testing.  I certainly plan on having it installed for Sun & Fun.
 
Ed
 
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