GrumpyOldCrewChief
Airman 1st Class
OK, folks, here comes a real esoteric request. I have been researching this question for a loooong time, and have not found a definitive answer. The The Me-261 was powered by the legendarily wretched (underdeveloped, arguably) DB paired motor units. On most of the aircraft that shared the use of this style motor, the inboard banks of cylinders exited their exhausts out of the cowling downwards, under the center of the motor. Some paired the manifolds into a single output manifold, some did not. But on the Adolfine, the struts and wheels for the MLG were placed right in line with that "usual" location. That situation would lead to all kinds of problems. I have not found a reliable reference anywhere that shows where that center pair of cylinder banks dumped their exhaust. Technically, there is no reason not to run a manifold to any other location, just to get it safely out of the cowling, but simplicity and lightness are Holy Grails in any aircraft design. Most drawings, I realize, are somebody's "best guess", and so can't be relied on. None of the photos I have layed eyes on so far show any clear detail of the underside of the engines. (see samples) Anybody got any real information? I already have all kinds of speculation. After all, I am a grumpy old crew chief, and an A&P mechanic...