X-Virus-Scanned: clean according to Sophos on Logan.com From: "Charlie England" Received: from mail-pg0-f44.google.com ([74.125.83.44] verified) by logan.com (CommuniGate Pro SMTP 6.2c1) with ESMTPS id 9591115 for flyrotary@lancaironline.net; Mon, 20 Mar 2017 23:06:13 -0400 Received-SPF: pass receiver=logan.com; client-ip=74.125.83.44; envelope-from=ceengland7@gmail.com Received: by mail-pg0-f44.google.com with SMTP id g2so86437345pge.3 for ; Mon, 20 Mar 2017 20:06:14 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=subject:to:references:from:message-id:date:user-agent:mime-version :in-reply-to; bh=Magp7zg/ndFcLGHubbLxHUje/XdhBQuNnTThXIsX05k=; b=HlGIHualyALXiaWNmNfXlO2s3Fs4zPJ6sLpIjY9bIpqO5kNG26Mfj3FkoEb7M2En3a CS9xqHMHnlwteSyaZSOMockyu6SmhpB3aw8A6aNb46VVlBpIbhK9Rn2ZE5e93T49DvVt dLkcC5l3ZsfDKlXQfJ/gLW/P3ivo79dtZy0OII9JwGpIvhznAG99T7ZasubQjHlXamk/ jgd5Gs7pLEhp4SbFG1/XsEgbHcrIx3do5usCepgM+o259w8LFMmTo918vGwSLXtjRlrb 3XBocoVyF97Yrjv9C2MKbF5oGTGsC/wQlG5BhKzkFY7uXR6YuQHSbEODukqM1NfSCwoq qGWQ== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:subject:to:references:from:message-id:date :user-agent:mime-version:in-reply-to; bh=Magp7zg/ndFcLGHubbLxHUje/XdhBQuNnTThXIsX05k=; b=YitQ6+edoavOSH7V2b+dNQtG8KwqjzLUaBwvFtyChU/bq38kmsd9hOKLPXRN0VWEwI 4+NlP17ExpnQH5bcQlpi5UOAPVVr9+t5y9+oLSrFKKqCeIsrNrVkB28cRFrOOkjD7ll4 Je11y3r8KPYfg5GZyfHWbLR0QqifumvXn8WDvoVwq1S3JPqydmXavUn2ADD+jrCRpMA+ jQDem/I6nVHYK9m1oIxRJPAGoNVEJOircX64p7ua2fnHFuA4Q11OPxdBTZYzID1qrpOu b8yn/V6jz2DGJj54vtlEmEmeY9PEyeva3+rNrxOQ6canHesmRd59ygeEygpijDMzDveM vJMw== X-Gm-Message-State: AFeK/H1IzRtGB8e57zXD3P+cFDMjAXKcgWIIACvI6WF50fDCVL9nrRsabakCjSLuR+geqQ== X-Received: by 10.98.96.65 with SMTP id u62mr37197480pfb.219.1490065556166; Mon, 20 Mar 2017 20:05:56 -0700 (PDT) Return-Path: Received: from ?IPv6:2602:306:25fb:1599:b5a4:cc58:338e:2789? ([2602:306:25fb:1599:b5a4:cc58:338e:2789]) by smtp.googlemail.com with ESMTPSA id e16sm28375170pfb.102.2017.03.20.20.05.54 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Mon, 20 Mar 2017 20:05:55 -0700 (PDT) Subject: Re: [FlyRotary] Re: fuel system peer review To: Rotary motors in aircraft References: Message-ID: Date: Mon, 20 Mar 2017 22:07:49 -0500 User-Agent: Mozilla/5.0 (Windows NT 6.1; WOW64; rv:45.0) Gecko/20100101 Thunderbird/45.8.0 MIME-Version: 1.0 In-Reply-To: Content-Type: multipart/alternative; boundary="------------92A30932F5C0C18BA60C927A" This is a multi-part message in MIME format. --------------92A30932F5C0C18BA60C927A Content-Type: text/plain; charset=utf-8; format=flowed Content-Transfer-Encoding: 7bit Hi Andrew, I get you on the 'complicated system' issue. That's one reason I'm considering this idea. And if I had any way to set up a gravity fed sump for the aux tanks, I'd eliminate the aux tank selector valve. :-) Yeah, pumping air is the big vulnerability. If I go down this path, I'll definitely include a GEM optical sensor ahead of the transfer pump(s). I'll also do some 'pumping air' testing. One in-tank injection pump will be running during any transfer operation, so testing will determine whether air from the xfer pump will cause engine stoppage, or just a stumble. Thank you for the input. Anybody else? I'm not married to this, but I am giving it serious consideration. Charlie On 3/20/2017 8:51 PM, Andrew Martin wrote: > Charlie, I think that would work. probably better to re-route the > lines though, so fuel from Aux tanks naturally wants to go through the > regulator rather than to the fuel rail. eventually you will leave a > transfer pump on and suck air. > In effect you've got 4 efi pumps, maybe just a little bit extreme, > especially if someone turns them all on. > > Andrew > (currently replacing entire fuel system from tanks to rail. previous > just too complex and heavy. sump tank, 2 pumps & 4 valves are coming out) > > On Tue, Mar 21, 2017 at 5:26 AM, Charlie England > > wrote: > > 1st, let me define my delivery architecture. I like Tracy's idea > of feeding the engine from one tank, and transferring aux tanks to > the main tank. I understand the downside of being unable to switch > tanks, but many a/c (including turbines) supply from one tank, so > that's my choice. It avoids the need for a duplex fuel selector, > which I like. Effectively, I have 3 'aux' tanks, and I'm using the > stock (3 inlet) Van's RV fuel selector to feed redundant transfer > pumps in parallel. > > I know that most have a separate return port in their tank(s) for > regulator return. With my need for aux transfer, my original plan > was to 'T' the aux transfer line into the regulator return line, > which I'm pretty sure has been done before. > > I'm currently working on installing both injection pumps in the > fuel tank, conceptually similar to standard auto practice for the > last couple of decades: no risk of vapor lock with the added bonus > of a very clean installation. The regulator will be in the > wingroot, just outside the tank, with the manifold pressure line > running to that location for pressure control. (Deadheading fuel > to the fuel rail has been done on both cars and a/c successfully; > I believe it's an option on the new SDS system being marketed to > Lyc drivers now.) > > The recent thread on fuel pressure changes while running both > injection pumps got me thinking. If it's typical to see only a > couple of PSI change when running both pumps, has anyone > considered running the transfer line into the regulator? The > reason I'm considering this is twofold. It provides a 'final > option' for short term fuel delivery if both injection pumps are > lost, and, because the regulator is in the wingroot, I would need > to run only one fuel line to the supply tank. > > I'll be using gerotor style transfer pumps (positive displacement) > and the aux selector has an 'off' position, so backflow won't be > an issue. > > A quick & dirty sketch is attached, diagramming the idea. > > There would never be more than 2 pumps running at any time, since > transfers would only happen in cruise flight. Can anyone poke > holes in this arrangement? > > Charlie > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > > --------------92A30932F5C0C18BA60C927A Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: 8bit
Hi Andrew,

I get you on the 'complicated system' issue. That's one reason I'm considering this idea. And if I had any way to set up a gravity fed sump for the aux tanks, I'd eliminate the aux tank selector valve. :-)

Yeah, pumping air is the big vulnerability. If I go down this path, I'll definitely include a GEM optical sensor ahead of the transfer pump(s). I'll also do some 'pumping air' testing. One in-tank injection pump will be running during any transfer operation, so testing will determine whether air from the xfer pump will cause engine stoppage, or just a stumble.

Thank you for the input. Anybody else? I'm not married to this, but I am giving it serious consideration.

Charlie

On 3/20/2017 8:51 PM, Andrew Martin wrote:
Charlie, I think that would work. probably better to re-route the lines though, so fuel from Aux tanks naturally wants to go through the regulator rather than to the fuel rail. eventually you will leave a transfer pump on and suck air.
In effect you've got 4 efi pumps, maybe just a little bit extreme, especially if someone turns them all on.

Andrew
(currently replacing entire fuel system from tanks to rail. previous just too complex and heavy. sump tank, 2 pumps & 4 valves are coming out)

On Tue, Mar 21, 2017 at 5:26 AM, Charlie England <flyrotary@lancaironline.net> wrote:
1st, let me define my delivery architecture. I like Tracy's idea of feeding the engine from one tank, and transferring aux tanks to the main tank. I understand the downside of being unable to switch tanks, but many a/c (including turbines) supply from one tank, so that's my choice. It avoids the need for a duplex fuel selector, which I like. Effectively, I have 3 'aux' tanks, and I'm using the stock (3 inlet) Van's RV fuel selector to feed redundant transfer pumps in parallel. 

I know that most have a separate return port in their tank(s) for regulator return. With my need for aux transfer, my original plan was to 'T' the aux transfer line into the regulator return line, which I'm pretty sure has been done before.

I'm currently working on installing both injection pumps in the fuel tank, conceptually similar to standard auto practice for the last couple of decades: no risk of vapor lock with the added bonus of a very clean installation. The regulator will be in the wingroot, just outside the tank, with the manifold pressure line running to that location for pressure control. (Deadheading fuel to the fuel rail has been done on both cars and a/c successfully; I believe it's an option on the new SDS system being marketed to Lyc drivers now.)

The recent thread on fuel pressure changes while running both injection pumps got me thinking. If it's typical to see only a couple of PSI change when running both pumps, has anyone considered running the transfer line into the regulator? The reason I'm considering this is twofold. It provides a 'final option' for short term fuel delivery if both injection pumps are lost, and, because the regulator is in the wingroot, I would need to run only one fuel line to the supply tank.

I'll be using gerotor style transfer pumps (positive displacement) and the aux selector has an 'off' position, so backflow won't be an issue.

A quick & dirty sketch is attached, diagramming the idea.

There would never be more than 2 pumps running at any time, since transfers would only happen in cruise flight. Can anyone poke holes in this arrangement? 

Charlie

--
Homepage:  http://www.flyrotary.com/
Archive and UnSub:   http://mail.lancaironline.net:81/lists/flyrotary/List.html



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