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F-30 Four-cylinder horizontally opposed, two-stroke, aircraft engine with a dual 38 mm diaphragm carburetors. Produces 85 hp (63 kW) at 5,500 rpm if free-air-cooled or 80 hp (60 kW) at 5,500 rpm if fan cooled. It has a factory rated time between overhaul (TBO) of 1,200 hours. Currently in production. [3] F-30E
Aftermarket port fuel injection and re-engineered cylinder heads have been the norm, although parts for the inline-six, such as aftermarket intake manifolds (from a three-carburetor setup or a single 4-barrel carburetor), exhaust headers, and hybrid cylinder heads based on Chevrolet's small-block engine are costlier than those for the small ...
In order to use existing tooling, five 250.6 cu in (4.1 L) Chrysler flathead engines (bore 3.4375 in or 87 mm, stroke 4.5 in or 114 mm) [1] were arranged around a central shaft, producing a unique 30-cylinder 21-litre (1,253 cu in) [1] engine in a relatively compact but heavy package.
The engine used three cooling fans, each directing air to one pair of opposed cylinders. The air/fuel intake used one Chevrolet-designed three-barrel carburetor per side. The original 2.94 in (74.7 mm) stroke was retained while the bore was increased to 3.56 in (90.4 mm), giving a total displacement of 175 cu in (2.9 L).
A test of a 30 cubic inch Vaux engine, built by a close associate of Bourke, gave a fuel consumption of 1.48 lb/(bhp hr), or 0.7 (lb/hr)/hp at maximum power. [6] Power to weight - The Silver Eagle was claimed to produce 25 hp from 45 lb, or a power-to-weight ratio of 0.55 hp/lb. The larger 140 cubic inch engine was good for 120 hp from 125 lb ...
The compression stroke is the second of the four stages in a four-stroke engine. In this stage, the air-fuel mixture (or air alone, in the case of a direct injection engine) is compressed to the top of the cylinder by the piston. This is the result of the piston moving upwards, reducing the volume of the chamber.
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