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  2. Pratt & Whitney R-2180-A Twin Hornet - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_R-2180-A...

    The Pratt & Whitney R-2180-A Twin Hornet was a radial engine developed in the United States by Pratt & Whitney. It had two rows of seven cylinders each. It had two rows of seven cylinders each. Applications

  3. Pratt & Whitney R-2180 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_R-2180

    Pratt & Whitney R-2180 was the designation for two closely related radial engines developed in the United States by Pratt & Whitney.They had two rows of seven cylinders each.

  4. Category:Pratt & Whitney aircraft engines - Wikipedia

    en.wikipedia.org/wiki/Category:Pratt_&_Whitney...

    Pratt & Whitney R-1535 Twin Wasp Junior; Pratt & Whitney R-1690 Hornet; Pratt & Whitney R-1830 Twin Wasp; Pratt & Whitney R-1860 Hornet B; Pratt & Whitney R-2000 Twin Wasp; Pratt & Whitney R-2060 Yellow Jacket; Pratt & Whitney R-2180-A Twin Hornet; Pratt & Whitney R-2180-E Twin Wasp E; Pratt & Whitney R-2270; Pratt & Whitney R-2800 Double Wasp

  5. Pratt & Whitney Wasp series - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Wasp_series

    The Pratt & Whitney Wasp was the civilian name of a family of air-cooled radial piston engines developed in the 1920s, 1930s and 1940s. [1]The Pratt & Whitney Aircraft Company (P&W) was founded in 1925 by Frederick B. Rentschler, who had previously been the President of Wright Aeronautical.

  6. Category:Aircraft air-cooled radial piston engines - Wikipedia

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

    Pratt & Whitney R-1535 Twin Wasp Junior; Pratt & Whitney R-1690 Hornet; Pratt & Whitney R-1830 Twin Wasp; Pratt & Whitney R-1860 Hornet B; Pratt & Whitney R-2000 Twin Wasp; Pratt & Whitney R-2180-A Twin Hornet; Pratt & Whitney R-2180-E Twin Wasp E; Pratt & Whitney R-2270; Pratt & Whitney R-2800 Double Wasp; Pratt & Whitney R-4360 Wasp Major

  7. Pratt & Whitney JT8D - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_JT8D

    The JT8D is an axial-flow front turbofan engine incorporating a two-spool design. There are two coaxially-mounted independent rotating assemblies: one rotating assembly for the low pressure compressor (LPC) which consists of the first six stages (i.e. six pairs of rotating and stator blades, including the first two stages which are for the bypass turbofan), driven by the second (downstream ...

  8. File:Pratt & Whitney R-2180 Twin Wasp Hornet radial engine ...

    en.wikipedia.org/wiki/File:Pratt_&_Whitney_R...

    The R-2180 “Twin Hornet’ was well along in the development stages when two issues surfaced that caused termination of the engine program. The first was realization that Pratt & Whltney's engineering had too many projects under development to provide each with the required attention necessary and Pratt & Whitney‘s company president ...

  9. Pratt & Whitney R-1860 Hornet B - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_R-1860...

    The Twin Wasp was by far the more powerful engine though, even in its early versions it produced 800 bhp to the Hornet B's 575 bhp. Having more cylinders per the same displacement also creates a smoother engine, since the individual pistons are smaller and lighter, and the stroke is shorter, which reduces the vibration of reciprocation, and ...

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