Mailing List Message #126
From: <>
Subject: Re: Atkins parts
Date: Tue, 01 Oct 2002 20:23:31 -0400
To: Rotary motors in aircraft <>
I promised some add'l photos, so here you go.

Ed mentioned that he'd recommend keeping the flow dispersers in with the injectors.  I just noticed that the injector angle on the tb is such that the fuel stream travels in the intake air stream for about 6" before it blasts against the inner wall of the manifold... I've got to believe this is intended to help break up the fuel into the required mist before getting to the combustion chamber.  Any thoughts on this?

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