VansAirForceForums  
Home > VansAirForceForums

- POSTING RULES
- Donate yearly (please).
- Advertise in here!

- Today's Posts | Insert Pics

  #1  
Old 03-06-2015, 06:56 AM
Mich48041 Mich48041 is offline
 
Join Date: Apr 2008
Location: Riley TWP MI
Posts: 3,068
Default Fuel System Peer Review

I hope it is alright to post here, even though the aircraft not a Van's, but is a Thurston-TA-16 with a LS1 fuel injected engine. VansAirforce is where all of the most knowledgeable people hang out. A friend of mine is building the TA16, which is at the stage where it is starting to look like an airplane. Below is a diagram of his fuel system which is already installed. I drew the filter and pressure regulator separately, but they are actually combined in one unit. The tank in the center holds about a quart. My friend calls it an accumulator, but I think that it is just a large-volume 4-way "T". I have concerns about the consequences of a pressure regulator failing. Is there a problem with turning on both solenoid valves but only one fuel pump? Comments, suggestions and criticism are welcome. PDF Version - ExpressSch Version
__________________
Joe Gores
RV-12 Flying
Reply With Quote
  #2  
Old 03-09-2015, 04:11 AM
rmartingt's Avatar
rmartingt rmartingt is offline
 
Join Date: Nov 2006
Location: Savannah, GA
Posts: 1,029
Default

IMHO that systems seems needlessly complicated. Solenoid valves for selecting the tank? Why the "accumulator" tank? Why no filters before the pumps?

I assume an LS1 uses electronic ignition, so why not piggyback off the same setup used by EFII? See the last page here. Forget the solenoid valves and just use a manual duplex fuel valve.

Edit: Also make sure the fuel return goes all the way back to the tank. Don't just tee it back in.
__________________
RV-7ER - finishing kit and systems installation
There are two kinds of fool in the world. The first says "this is old, and therefore good"; the second says "this is new, and therefore better".

Last edited by rmartingt : 03-09-2015 at 06:57 AM. Reason: Addition
Reply With Quote
  #3  
Old 03-09-2015, 05:42 AM
Jesse's Avatar
Jesse Jesse is offline
 
Join Date: May 2005
Location: X35 - Ocala, FL
Posts: 3,679
Default

I agree with rmartingt. I wouldn't be a fan of the solenoid valves. I think the EFII setup should work perfect for that installation as well.

In response to the single pump on with both valves on, this should work since there are 2 pressure regulators and the check valves.
__________________
Jesse Saint
Reply With Quote
  #4  
Old 03-09-2015, 08:17 AM
Mich48041 Mich48041 is offline
 
Join Date: Apr 2008
Location: Riley TWP MI
Posts: 3,068
Default

The owner of this project lives about 45 minutes away from me. I have just recently visited his project for the first time and the fuel system was already installed in the fuselage. It would be difficult to install return lines to the fuel tanks in the wings that are already built (but not yet attached to the fuselage). I agree with you guys that a manual fuel valve is less likely to fail than a solenoid valve. The solenoid valves do allow remote control without long fuel lines or the need to find room to install a manual selector valve within easy reach.
"Why the "accumulator" tank" That is the same question I asked. I see no useful purpose of that tank except perhaps to help cool the fuel. But I do not know if it has enough area to accomplish that. Do you guys think that the fuel will get too warm without returning to the wing tanks? I will forward your comments to my friend.
__________________
Joe Gores
RV-12 Flying
Reply With Quote
  #5  
Old 03-09-2015, 08:31 AM
Jesse's Avatar
Jesse Jesse is offline
 
Join Date: May 2005
Location: X35 - Ocala, FL
Posts: 3,679
Default

The purpose of the "header" tank is almost certainly to keep the fuel cool. I would probably recommend that it be at least 2 gallons to avoid overheating the fuel. I had a vapor problem on an engine with no header with the fuel return going to a T in the line just on the engine side of the fuel selector. The fuel just kept getting hotter and hotter, as it cycled into the engine compartment, until it vaporized in the fuel pump and the engine wanted to quit in flight. Not a fun experience. We added fuel returns to the tanks and a stacked fuel selector and the problem was solved. That's certainly the best option. He could get a bung that rivets with proseal into the tank and then a threaded fitting in the bung and you have a return. That would definitely be my recommendation.
__________________
Jesse Saint
Reply With Quote
  #6  
Old 03-09-2015, 10:06 AM
DanH's Avatar
DanH DanH is offline
 
Join Date: Oct 2005
Location: 08A
Posts: 9,477
Default

Quote:
Originally Posted by Mich48041 View Post
I have just recently visited his project for the first time and the fuel system was already installed....
Joe, make enough TC calls, and this won't be the last time you hear that wail from a builder.

Quote:
I agree with you guys that a manual fuel valve is less likely to fail than a solenoid valve.
Don't need any valve. Fuel is not going to flow uphill (from a wing tank to a high pusher engine pylon) all by itself. Without 'em you can simplify and add lightness.

Ditch the solenoid valves. Run return lines to the tanks. Put the filters before the pumps. Move the check valves. Now it's simply "both pumps on for takeoff", and if one unports or runs dry it makes no difference.

__________________
Dan Horton
RV-8 SS
Barrett IO-390
Reply With Quote
  #7  
Old 03-09-2015, 10:09 AM
rv6ejguy's Avatar
rv6ejguy rv6ejguy is offline
 
Join Date: Mar 2005
Location: Calgary, Canada
Posts: 5,745
Default

Duplex fuel valve, return lines to the tanks a very good idea to avoid hot start and vapor lock issues, filters before the pumps, use Walbro pumps mounted right on the floor (they re-prime much better and don't make metal like some other brands), they have built in check valves. Ditch the header tank and solenoid valves. Regs should ideally be on exit of 2nd fuel rail (again to purge out hot fuel as soon as pumps run).

If you have a sender access cover in metal tanks, you can use Earls Stat-O-Seals to mount the return fittings without the goop.
__________________

Ross Farnham, Calgary, Alberta
Turbo Subaru EJ22, SDS EFI, Marcotte M-300, IVO, Shorai- RV6A C-GVZX flying from CYBW since 2003- 441.0 hrs. on the Hobbs,
RV10 95% built- Sold 2016
http://www.sdsefi.com/aircraft.html
http://sdsefi.com/cpi2.htm


Reply With Quote
  #8  
Old 03-09-2015, 10:16 AM
N62XS N62XS is offline
 
Join Date: Jan 2005
Location: Hazlehurst, GA
Posts: 1,359
Default KISS

Keep it super simple. If the builder wants an eternal repair/tinker project, embrace complexity. If the builder wants to fly and enjoy the fruits of his labor, keep it super simple.
__________________

IHN,

2020 Dues Paid

Robby Knox

THEM: Why do you always carry a knife?

ME: I can't open a bag of chips with my Glock!
Reply With Quote
  #9  
Old 03-10-2015, 09:32 AM
Mich48041 Mich48041 is offline
 
Join Date: Apr 2008
Location: Riley TWP MI
Posts: 3,068
Default

Thanks for all of the comments and suggestions. I will pass them along to the builder.
__________________
Joe Gores
RV-12 Flying
Reply With Quote
Reply


Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT -6. The time now is 04:33 AM.


The VAFForums come to you courtesy Delta Romeo, LLC. By viewing and participating in them you agree to build your plane using standardized methods and practices and to fly it safely and in accordance with the laws governing the country you are located in.