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In 1905, Continental Motors was born with the introduction of a four-cylinder, four stroke cycle L-head engine operated by a single camshaft. In August 1929, the Continental Motors Company formed the Continental Aircraft Engine Company as a subsidiary to develop and produce its aircraft engines. [1] A Continental engine in a 1948 Divco delivery ...
In late 1948, Cessna began sales of the 170, with a metal fuselage and tail and fabric-covered constant-chord wings. These earliest 170s were four-seat versions of the popular 140 with a more powerful 145 hp (108 kW) Continental C145-2 and an extra interconnected fuel tank in one wing for a total of 36 gallons in three tanks. Like the 140, they ...
The wing is metal instead of composite and the aircraft is equipped with a Teledyne Continental Motors FADEC-controlled engine mounted on a metal space frame instead of the Europa's Rotax 912 engine mounted on the fiberglass fuselage. The landing gear is also of a different design. [3] The Liberty was designed by Ivan Shaw, who also created the ...
The Continental O-190 (Company designations C75 and C85) is a series of engines made by Continental Motors beginning in the 1940s. Of flat-four configuration, the engines produced 75 hp (56 kW) or 85 hp (63 kW) respectively. [1] The two variants shared the same bore, stroke and compression ratio.
After the war, Continental introduced its own R-975 version for aircraft, the R9-A. Though it was basically similar to other R-975 engines, and its compression ratio and supercharger gear ratio were unchanged from the R-975E-3, other improvements in the R9-A allowed it to achieve 525 hp (391 kW) for takeoff, [ 12 ] surpassing any Wright version.
The 130 hp (97 kW) O-240 was a new engine design derived from the six-cylinder Continental O-360 and introduced in 1971. It is generally similar in overall dimensions to the Continental O-200, but with a higher 8.5:1 compression ratio, designed to run on 100/130 avgas. The O-240 delivers 30% more power than the O-200 while it weighs only 12% more.