rand robinson
kr2s
kr-2s
kr2
kr1
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KR2S

cad
The KR2S Project

Fuel System


The fuel system that resides under the seat, comprises of a 3/8" 5052-0 aluminum fuel line with AN6 fittings, two electric facet fuel pumps running in series and 2 fuel filters.  The fuel tanks in the stub wings cross feed via a 3/4" Earls Pro Lite 350 hose with Swivel Seal fittings.  This hose feeds off to the aluminum fuel line.  Only the left hand fuel tank will have a filler cap as the cross feed hose allows fuel to flow through to the right hand tank.  I figure the less management of fuel involved, the less likely there is to be an incident down the track.
5052 ally tank cutout The layout of the fuel system is straight forward.  As the fuel tanks in the AS5048 stub wings are higher than the original RAF48 which has a lower aft spar, the fuel flows out and down the 3/4" hose to the AN824 TEE which rests at floor level, 3" lower than the bottom of the tanks.  Not shown in this photo, an AN12 - AN6 reducer passes fuel to the 40 micron Proflow filter.  The two facet pumps can operate together or independently of each other which provides redundancy and thus piece of mind.  
fuel filter This is the inside of the Proflow aluminum billet fuel filter.  The replaceable 40 micron filter is easily accessed by unscrewing the T-6061 housing.
facet fuel pump I have made bases for each fuel pump to bolt to.  They are made of 3/32" plywood with 1/8" foam acting to dampen any vibration.  Two counter sunk bolts hold the pump to the base which is epoxied to the floor.  Once cured, the pump is able to be removed in the future if need be.  These facet pumps do not have anti-siphoning or check valves which means if one pump fails, the second will be able to draw fuel through it.  I anticipate flying with both pumps switched on and preflight testing them individually, much like you would do with left and right magnetos.  If a pump fails the check, it can be unbolted from the mount and replaced with a spare.
fuel cock The 3/8" fuel line passes under the main spar beside the rudder cable.  The reason I am running the line through the cockpit is because I need easy access to a simple fuel shut off valve.  I want the ability to turn the fuel off in the event of an engine fire, forced landing or an accident.  As these facet pumps do not feature check valves, switching off both fuel pumps could still see fuel flow through the line if the KR was at an unusual attitude after an accident.  eg. upside down.
reducer I decided to make my own AN12 - AN6 reducer so started with the AN929-12D end cap and drilled it before threading it for the AN816-6-6D nipple.  
reduction Here is the finished product.  More compact and less weight than screwing 3 or 4 reducers together.
AN t-piece Now inside my reducer I have inserted the primary fuel strainer which would have normally resided in each fuel tank.  However, I could not find a strainer to fit the 3/4" tank outlets.  Having it fitted here also allows for easier access for checking rather than inside sealed tanks.
AN t-piece Everything fits neatly together.