That is very cool, PJ. You already have the flap balance tab technology you will need to relieve the ponderous hinge moment.
Dave Gardner was writing an article about the B-17 fuel system for Stunt News, but I delayed his progress by offering him some additional data which I probably never gave him. Now that someone is interested, we should finish the article.
I found a summary of the fuel system, which I may have posted here before, so if the following looks familiar, it may well be:
The B-17 fuel system resulted from the FAI rule that F2B airplanes can’t have automatic or pilot-activated engine shutoffs. This made it challenging to have all four engines reliably quit between the end of the pattern and the seven-minute F2B flight time limit. Paul’s first B-17 had four individual tanks. This system had too much variation in engine shutdown time. Would you have guessed that the four engines burn vastly different amounts of fuel as a function of position on the plane? He then went to a system having a central bladder and individual pressure regulators on each engine. Paul used this setup at the 1995 Nats. It was pretty consistent, but the time between when the left engine quit until the right engine quit was about 20 seconds. When the bladder ran out, the fuel in the manifold between the engines had sufficient head pressure to keep engines to the outside of the circle running. The engines would quit from left to right with about one lap between. Paul thought that for reliable F2B operation the engines would need to quit over a much shorter time. We decided to use pressure reducers on the engines on the right wing to attenuate the head pressure, so that all the engines would quit when the bladder pressure dropped at the end of the run. Ralph Cooney of Fourmost donated some check valves that I made into ball-and-spring 7-psi pressure reducers. These worked perfectly the first time we tried them—but seldom after that. A sideways tap on the pressure reducer knocked the ball out of its seat, after which the reducer did not reduce. I made some seemingly more reliable reducers out of Luer fittings, which Paul used at the 2001 Nats. I’d like to know of any other little pressure reducers one can buy; we haven’t been able to find any.
We tried various combinations of pressure reducers and got bizarre engine-shutdown results. I made an engine-shutdown simulation that actually explained the results and confirmed that we needed reducers on only numbers 3 and 4: one of the few cases of theory being of any help to the Bomber project.
Norm McFadden designed the regulators for combat. They proved very reliable over the years—-sufficiently so that several west coast combat flyers used them despite their small advantage for combat over a straight-through fuel feed from bladder to engine. Tony Huber makes the regulators, which are popular now with RC pylon racers. I’ll send you his phone number.
Get some of Ferocious's yellow bladder tubing and bladder end fittings.
The pressure reducers use parts available from Small Parts, http://www.smallparts.com/. Part numbers are:
W-1005009 Male Luer lock 3/32” with locking nut
Q-1005109 Female Luer 3/32” barb
W-BX-1-1/2 stainless steel ball, 3/32” diameter
I think I used the 3/32” ball, but I may have used 1/16” or 1/18”. Their part numbers are:
W-BX-1 stainless steel ball, 1/16” diameter
W-BX-2 stainless steel ball, 1/8” diameter
They are 9 cents apiece, so get some of each.
I made the springs from .005” stainless steel wire: the center strand of .015” stranded control lines.
The fuel system is still a little unreliable. I think it is unstable when the engines are running rich (the richer it gets, the richer it gets), so the engines have to run pretty close to peak RPM. Dr. Briggs and I have done some further experiments to try to fix this. I posted some of them here. I tried to make the bladder-fed engine operate at a steady four cycle. Nothing has worked so far.
What engines do you have in mind? One thing to look for is a positive gradient of crankcase pressure with RPM. The primary thing to look for is probably lightness. You really have to work to keep weight down. The bladder tube, for example, was made from two plies of .002" thick carbon prepreg.