Return-Path: Received: from [65.54.168.111] (HELO hotmail.com) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 725509 for flyrotary@lancaironline.net; Fri, 11 Feb 2005 17:05:48 -0500 Received-SPF: pass receiver=logan.com; client-ip=65.54.168.111; envelope-from=lors01@msn.com Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Fri, 11 Feb 2005 14:05:01 -0800 Message-ID: Received: from 4.174.6.71 by BAY3-DAV7.phx.gbl with DAV; Fri, 11 Feb 2005 22:04:08 +0000 X-Originating-IP: [4.174.6.71] X-Originating-Email: [lors01@msn.com] X-Sender: lors01@msn.com From: "Tracy Crook" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Heating the Fuel Date: Fri, 11 Feb 2005 17:04:05 -0500 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0073_01C5105B.B192BF60" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: MSN 9 X-MimeOLE: Produced By MSN MimeOLE V9.10.0009.2900 Seal-Send-Time: Fri, 11 Feb 2005 17:04:05 -0500 X-OriginalArrivalTime: 11 Feb 2005 22:05:01.0855 (UTC) FILETIME=[BBDE9AF0:01C51085] This is a multi-part message in MIME format. ------=_NextPart_000_0073_01C5105B.B192BF60 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable > >The problem with boiling the fuel is that most of it will then escape = out=20 >the vent before it can re-condense. I'm sure this will more than = offset=20 >any fuel gains from drag-free cooling. Even moderately raising the = temp=20 >(and vapor pressure) will probably cause excessive evaporative loss = of the=20 >fuel. We have to face the fact the fuel is not an acceptable coolant = for=20 >this application. That's OK, there is still Evans or water and the = rest=20 >of the wing surface to be used. > Look up "heat pipe" using Google. The returned vapor will quickly condense in the cool tank. = The=20 only way it will not condense is if the tank, and it's entire = contents,=20 reach the boiling point of the fuel. Until the entire tank and the fuel in it warm up to the = boiling=20 point, all of the vapor will condense on the walls and on the surface = of=20 the fuel in the tank. As long as most of the vapors are condensing, = the=20 fuel properties will not change. This is why you need to monitor the fuel tank temperature if = you=20 are planning to use the fuel as coolant. If you dump too much heat = into the=20 tank, it will become warm enough to vaporize the fuel. You probably = would=20 not want the tank to become much hotter than, say, 140 F, I would = guess. Bill Dube Good reference on the heat pipe Bill. The 140 Deg figure is about = what my seat of the pants guess was. I figured 120 as a safe margin. = If my instrumentation and methodology was good during my test (must = repeat it to be sure) then there is a possibility "fuel cooling" will be = useful.=20 The basic numbers so far: I got 2 degrees of oil cooling with something like 20 - 30 GPH of = fuel flow through heat exchanger. Temperature rise in the tank was on the order of .1 degrees (lets say = it was .2 for sake of argument) We need about 40 degrees of oil cooling, about 20 times what I got in = the experiment. Also means we need 20x the fuel flow or about 500 GPH = (8 1/3 GPM). Assuming this means a temp rise in the tank of 20 x .2 or 4 degrees, = that implies that there is a huge margin of safety here. And this was = only using one of the two tanks. If it was required, I'd be happy to = utilize both tanks. I will be the first to admit that this sounds too good to be true. I = must repeat the experiment to verify the basic numbers. Tracy ------=_NextPart_000_0073_01C5105B.B192BF60 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
 

>
>The problem with boiling the fuel is that most of = it will=20 then escape out
>the vent before it can re-condense.  I'm = sure=20 this will more than offset
>any fuel gains from drag-free=20 cooling.  Even moderately raising the temp
>(and vapor = pressure)=20 will probably cause excessive evaporative loss of the =
>fuel.  We=20 have to face the fact the fuel is not an acceptable coolant for =
>this=20 application.  That's OK, there is still Evans or water and the = rest=20
>of the wing surface to be=20 used.
>

         = Look up=20 "heat pipe" using=20 Google.

         The = returned=20 vapor will quickly condense in the cool tank. The
only way it will = not=20 condense is if the tank, and it's entire contents,
reach the = boiling point=20 of the fuel.

         = Until the=20 entire tank and the fuel in it warm up to the boiling
point, all = of the=20 vapor will condense on the walls and on the surface of
the fuel in = the=20 tank. As long as most of the vapors are condensing, the
fuel = properties=20 will not = change.

         This=20 is why you need to monitor the fuel tank temperature if you
are = planning=20 to use the fuel as coolant. If you dump too much heat into the =
tank, it=20 will become warm enough to vaporize the fuel. You probably would =
not want=20 the tank to become much hotter than, say, 140 F, I would = guess.
Bill Dube

Good reference on the heat pipe Bill.  The 140 Deg = figure is=20 about what my seat of the pants guess was.   I figured 120 = as a safe=20 margin.   If my instrumentation and methodology was good = during my=20 test (must repeat it to be sure) then there is a = possibility "fuel=20 cooling" will be useful. 
 
The basic numbers so far:
 
 I got 2 degrees of oil cooling with something like 20 - 30 = GPH of=20 fuel flow through heat exchanger.
 
 Temperature rise in the tank was on the order of .1 degrees = (lets=20 say it was .2 for sake of argument)
 
We need about 40 degrees of oil cooling, about 20 times what I = got in the=20 experiment.  Also means we need 20x the fuel flow or about 500 = GPH (8 1/3=20 GPM).
 
Assuming this means a temp rise in the tank of 20 x .2  = or 4=20 degrees, that implies that there is a huge margin of safety = here.  =20 And this was only using one of the two tanks.  If it was = required, I'd be=20 happy to utilize both tanks.
 
I will be the first to admit that this sounds too good to be = true. =20 I must repeat the experiment to verify the basic numbers.
 
Tracy
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