X-Virus-Scanned: clean according to Sophos on Logan.com From: "Charlie England" Received: from mail-pf0-f176.google.com ([209.85.192.176] verified) by logan.com (CommuniGate Pro SMTP 6.2c1) with ESMTPS id 9594137 for flyrotary@lancaironline.net; Tue, 21 Mar 2017 16:54:20 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.192.176; envelope-from=ceengland7@gmail.com Received: by mail-pf0-f176.google.com with SMTP id o190so2990506pfo.0 for ; Tue, 21 Mar 2017 13:54:19 -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=ihc7LWlgf7cOidkhPWbFZjdxXGCZdB9GbE0QWHlF3B4=; b=ig1lBm1MLpVW+ii9HeML1c9gLpG6O2LfkqmhCFu66+ld8Ggomi9PqChm4Z1eOfB9iu OKrV+XkLWkLw3sinMasYBpxuFiDIQv24zt/k8F2TTfAKPJr4raeW4xuP5sdIC3xQDonT dMMUHhx8TqFXcIBkmi0v+4W2P+mA0595SoDFkFmSxiR7M4Pskxl+iAQH205GvMnBwXt7 NcNokxcq5dy/WKAaN6ZmjBi7botMAWrHjgar3E1Sx7USk7ul+nOEDsnmMgv4PXRBsjty U+C0CfpGYD4nRGSdM/iz86mfuIpvdrzQKlwPgqyCYN+L6zH1974krzXKO9tHx7sgOst2 XgCg== 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=ihc7LWlgf7cOidkhPWbFZjdxXGCZdB9GbE0QWHlF3B4=; b=e9nwJ2CxIInmJPcrxtgi0v8JBAbkADt3mP1kjcViKzGoXLNB59EG4aMCzqYEM/Tgml c9vHoq4P+8MVRqutK4p8gOgSh6elRh5Qg+bXc5CN55gQA22qC9veP5Y/GSFT7eYncBYg zurSi96EI8ooWDxYan3/zDDLrBtXdQBDJ/Q0hteFDDED/gN5atQZoyyKiuLW4veGATdv LV6QFpXqK/gtRpTYoHLMMAgG4ScLF3z4ZWPZPPyJGkGrpzFwHnXjEC+Jzxv71dbrWEHU qsdfso82i2Eu5wthvYvWv3Qwccdv+t/oX5RSW1OsDAKuFGDOzRrQqzgiIN0YvFlFfSB3 F0Wg== X-Gm-Message-State: AFeK/H1ztG/aDFJTkBOYQ4j6j04c6X4qDfpv5mc4m2e9Jzh97pKjFOVxzrUWPr2tDnbscQ== X-Received: by 10.98.213.130 with SMTP id d124mr42994764pfg.172.1490129641439; Tue, 21 Mar 2017 13:54:01 -0700 (PDT) Return-Path: Received: from ?IPv6:2602:306:25fb:1599:a476:6fca:5659:407? ([2602:306:25fb:1599:a476:6fca:5659:407]) by smtp.googlemail.com with ESMTPSA id c28sm41260170pfj.77.2017.03.21.13.53.59 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Tue, 21 Mar 2017 13:54:00 -0700 (PDT) Subject: Re: [FlyRotary] Re: fuel system peer review To: Rotary motors in aircraft References: Message-ID: Date: Tue, 21 Mar 2017 15:55:54 -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="------------58A1A578CBF45D9496069219" This is a multi-part message in MIME format. --------------58A1A578CBF45D9496069219 Content-Type: text/plain; charset=utf-8; format=flowed Content-Transfer-Encoding: 7bit I did consider it, but that would mean 3 xfer pumps instead of 1+backup. I'd still need a pair of injection pumps. In the same vein, I considered the little turbine style in-tank pumps for that purpose, but then I'd need a positive shutoff valve for the aux tanks. I also considered them for injection pumps (lighter, smaller, lower power consumption) but they're actually harder to mount with any configuration flexibility and I'd again need a separate positive cutoff (gerotor pumps are positive cutoff when not running). Thanks, Charlie On 3/21/2017 10:33 AM, Ernest Christley wrote: > At the point you're at, what would be the downside to simply putting a > pump in each tank, and using a rotary switch to select? Having the > main tank with the return wired in with the ignition, so that it is > always running to avoid the return overfilling the tank. > > On Mar 20, 2017 5:26 PM, 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 --------------58A1A578CBF45D9496069219 Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: 8bit
I did consider it, but that would mean 3 xfer pumps instead of 1+backup. I'd still need a pair of injection pumps. In the same vein, I considered the little turbine style in-tank pumps for that purpose, but then I'd need a positive shutoff valve for the aux tanks. I also considered them for injection pumps (lighter, smaller, lower power consumption) but they're actually harder to mount with any configuration flexibility and I'd again need a separate positive cutoff (gerotor pumps are positive cutoff when not running).

Thanks,

Charlie

On 3/21/2017 10:33 AM, Ernest Christley wrote:
At the point you're at, what would be the downside to simply putting a pump in each tank, and using a rotary switch to select?  Having the main tank with the return wired in with the ignition, so that it is always running to avoid the return overfilling the tank.

On Mar 20, 2017 5:26 PM, 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

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