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  2. Continental Aerospace Technologies - Wikipedia

    en.wikipedia.org/wiki/Continental_Aerospace...

    In 1929, the company introduced its first aircraft engine, [3] a seven-cylinder radial designated as the A-70, with a displacement of 543.91 cu in (8.91L) that produced 170 hp (127 kW). In August 1929, the Continental Motors Company formed the Continental Aircraft Engine Company as a subsidiary to develop and produce its aircraft engines. [4]

  3. Continental O-470 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-470

    The Continental O-470 engine is a family of carbureted and fuel-injected six-cylinder, horizontally opposed, air-cooled aircraft engines that were developed especially for use in light aircraft by Continental Motors. Engines designated "IO" are fuel-injected. [1] [2] The family also includes the E165, E185, E225 and the E260 engines, and ...

  4. Category:Continental aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Continental...

    Pages in category "Continental aircraft engines" The following 24 pages are in this category, out of 24 total. ... Continental O-526; R. Continental R-670; T.

  5. Continental Motors Company - Wikipedia

    en.wikipedia.org/wiki/Continental_Motors_Company

    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 ...

  6. Continental XI-1430 - Wikipedia

    en.wikipedia.org/wiki/Continental_XI-1430

    This one-cylinder engine was designated "Hyper No. 2", and became the test bed for developing the cylinders that would become the Continental O-1430 ("O" for "opposed") engine. It would require a ten-year development period which changed the layout to first an upright V-12 engine and later, an inverted V-12 engine, before becoming reliable ...

  7. Continental O-300 - Wikipedia

    en.wikipedia.org/wiki/Continental_O-300

    The GO-300 employs a reduction gearbox, so that the engine turns at 3200 rpm to produce a propeller rpm of 2400. The GO-300 produces 175 hp (130 kW) whereas the ungeared O-300 produces 145 hp (108 kW). [1] The GO-300 engine has a TBO (Time Between Overhaul) of 1200 hours, while 1800 hours is the standard for ungeared O-300 engines.

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