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
- A preserved Jacobs R-755 is on display at the Arkansas Air Museum.[3]
- A Jacobs R-755 is on public display at the Aerospace Museum of California
- A preserved Jacobs R-755 is on display at Super T Aviation Academy in Medicine Hat, Canada.
- A restored Jacobs R-755A is on display at the House of Whitley.
External links
Notes and References
- Book: Gunston. Bill. World encyclopaedia of aero engines. 1989. P. Stephens. Wellingborough. 1-85260-163-9. 85. Fully rev. 2nd.
- 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.
- http://www.arkairmuseum.org/engines/engine-jacobs755.php Arkansas Air Museum - Jacobs R-755