Mailing List flyrotary@lancaironline.net Message #56288
From: Al Wick <alwick@juno.com>
Subject: Re: [FlyRotary] In-tank pumps
Date: Wed, 17 Aug 2011 10:40:40 -0700
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
<how does it
<avoid a negative pressure when the fuel level gets near the bottom of the tank?
 
It doesn't. Actually, GM takes advantage of that and designs inlet so that you'll run out of fuel at home instead of on the road. Pretty interesting.
 
I mention the oem design because I'd like to save a few lives. Fewer crashes. I hope a few guys will be open minded. Test their ideas instead of speculate. Compare results to OEM method.
 
If we broke down fuel design into individual components. Like self priming, pressure drop at inlet, effect of contaminants, etc. Then did the simple tests to prove which is superior, it would be enlightening.
 
-al wick
----- Original Message -----
Sent: Wednesday, August 17, 2011 8:40 AM
Subject: [FlyRotary] In-tank pumps

Al Wick wrote:

> What's the best fuel design to prevent vapor lock? Copy any auto mfg
> method. They all use the same method because it's SOOO effective. OEM
> fuel designs minimize every REAL risk we have in our aircraft. They use
> self cleaning filters that have around 10 or 20 times more surface area
> than stupid in line filters. They minimize pressure drop at pump inlet
> by using large coarse filters there. Submerged pumps. Every car mfg uses
> the same system. Do you know how rare that is? They do it because the
> wet design with self cleaning filters eliminates all historical failures.
> I recently converted my sys to automotive style. Details at bottom of page:
> http://www.maddyhome.com/canardpages/pages/alwick/index_files/Page467.htm


Can you explain something to me on this point?  Considering that the in-tank pump has a positive volume, how does it
avoid a negative pressure when the fuel level gets near the bottom of the tank?  I ask, because most airplanes tend to
have very flat tanks, and fuel often gets left on the ground for weight and balance reasons.  Pulling that last few
gallons off the bottom of the tank can be VERY important.  Putting the pump in the tank is going to result in pulling
fuel uphill at some point unless you have a flat pump.

I'm going to go out on a limb and say you're wrong.  Manufacturers all use the in-tank system because it simplifies
design and assembly.  They all use pre-assmebled console "clusters", and many other pre-assembled components for the
same reason.  It is not rare at all.  In-tank pumps are not a safety issue.  It's an economic one.

The best design for avoiding vapor lock is going to be the one that puts the most pressure ahead of the pumps.  Whether
this is done by putting the fuel as high above the pumps as possible, pressurizing the tank, or magical pixie dust,
positive pressure at the pump inlet is the only answer.  The in-tank pump only marginally solves the problem and is a
maintenance nightmare.

But, to each his/her own.  You build it.  You fly it.

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