LS1 aircraft fuel system
I have a few questions about the lines and return system. I've searched and come up with little info, since this probably isn't something that directly applies to automotive use.
I plan to use 1/2 inch aluminum tube from 2 separate tanks through a fuel selector valve, through a filter, through a (probably aeromotive A1000) pump to the firewall, then use braided -8 line to the rail. There will actually be two pumps arranged with split lines and check valves for redundancy, running one at a time.
Question 1: with about a 48" unpressurized line from the tank through the selector to the pump, will 1/2" line be sufficient to avoid cavitating the pump? Would a low pressure boost pump at the tank (used for starting to push fuel to the high pressure pump) be a good idea or a waste of time and money? The high pressure pump will be about 12-18 inches higher than the tank outlet.
Question 2: can I run the return line into the feed line between the high pressure pump and the fuel selector instead of all the way to the tank? I want to avoid having to use two returns and keep the return line as short as possible since it's a pain to route it through all the structure to the wing tanks.
Any comments and suggestions will be welcome.
org
a guy at the shop where i get some of my machine work was telling me about some guuy wanting to put an ls1 engine in his plane for a racing aplication. looks like more people are starting to think about this.
http://home.comcast.net/~ogoodwin/Mustang.html is my site that has pictures and info as well as links to a company converting LS1s for aircraft use.
org
Last edited by org; Jun 23, 2004 at 03:05 PM. Reason: add link


