Jacobs R-755 Explained

The Jacobs R-755 (company designation L-4) is a seven-cylinder, air-cooled, radial engine for aircraft manufactured in the United States by the Jacobs Aircraft Engine Company.[1]

Design and development

The R-755 was first run in 1933 and was still in production in the 1970s. With a bore and stroke of 5.25 in × 5 in (133 mm × 127 mm) the displacement was 757 cu in (12.4 L), power ranged from 200 hp to 350 hp (150 kW - 260 kW). The engine features steel cylinders with aluminum-alloy cylinder heads. An R-755E variant was developed for use in helicopters.

Variants

R-755A1:The base-line direct drive production version.[2]
  • R-755A2:300 hp variant.
  • R-755A3:Similar to A1 but with Scintilla magnetoes.
  • R-755B1:De-rated version of the R-755A to drive a fixed pitch airscrew.[2]
  • R-755B2:De-rated version of the R-755A to drive a variable or controllable pitch airscrew.[2]
  • R-755E:Up-rated engine with reduction gearing.[2]
  • R-755EH:Developed to power the Jacobs Type 104 Gyrodyne.[2]
  • Applications

    Engines on display

    External links

    Notes and References

    1. Book: Gunston. Bill. World encyclopaedia of aero engines. 1989. P. Stephens. Wellingborough. 1-85260-163-9. 85. Fully rev. 2nd.
    2. Book: Bridgman, Leonard. Jane's all the World's Aircraft 1955-56. 1955. Jane's all the World's Aircraft Publishing Co. Ltd.. London. 305.
    3. http://www.arkairmuseum.org/engines/engine-jacobs755.php Arkansas Air Museum - Jacobs R-755