Each of these sections cooperates in a known manner to regulate the amount of fuel that is delivered to the engine, which is proportional to the amount of air that flows through the throttle body assembly, i.e., the power produced by the engine. The RSA-5AB1 servo also includes an automatic mixture control section. The major components of a conventional fuel injection servo include the airflow section, the flow metering section, and the fuel regulator section. 3 shows the RSA-7AA1 fuel injection servo, which is also sold by Precision Airmotive Corporation. 1 and 2 show the RSA-5AD1 and the RSA-5AB1 fuel injection servos, respectively, sold by Precision Airmotive Corporation. Conventional fuel injection servos are shown in FIGS. BACKGROUND OF THE INVENTIONĪ fuel injection system for an internal combustion, aircraft engine generally includes, among other components, a fuel injection servo, a flow divider, and fuel nozzles. This invention relates to a fuel injection system, and more particularly to a fuel control apparatus for an internal combustion engine. Patent and Trademark Office files or records but otherwise reserves all copyright rights whatsoever. The copyright owner has no objection to the facsimile reproduction by anyone of the patent document or the patent, as it appears in the U.S. This patent document contains information subject to copyright protection. 60/217,310, the entirety of which is hereby incorporated into the present application by reference. Provisional Application of Rivera, filed Jul. The present application claims priority to U.S.
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