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.
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 (133mm × 127mm) the displacement was 757 cu in (12.4 L), power ranged from 200hp to 350hp (150kW - 260kW). The engine features steel cylinders with aluminum-alloy cylinder heads. An R-755E variant was developed for use in helicopters.
It was the first modern radial engine to use a battery ignition.
Variants
L-4
Produced 225 horsepower (168kW) at 2,000 rpm, dual battery
L-4M
Dual magneto
L-4MA
Dual magneto, for use in autogyros
L-4MA7
Similar to R-755A3, for use in autogyros
L-4MB
Rated at 225hp (168kW) at 2,000 rpm.
L-4MBB
Rated at 225hp (168kW) at 2,000 rpm.
R-755-7
Rated at 225hp (168kW) at 2,000 rpm.
R-755-9
Rated at 225hp (168kW) at 2,000 rpm. Military version of the L-4MB.
R-755-A
Replaced the R-755-9. Rated at 300hp (220kW) at 2,200 rpm. Increased compression ratio to 6:1.
R-755A1
The base-line direct drive production version. Equivalent to the L-4MB.
↑Mingos, Howard, ed. (1942). The Aircraft Year Book for 1942(PDF). New York, New York: Aeronautical Chamber of Commerce of America. pp.362–364. Retrieved 13 October 2026.
12Aircraft Engine Listing. Washington, D.C.: Civil Aeronautics Administration, U.S. Department of Commerce. 15 May 1950. pp.11, 13. Retrieved 13 October 2026.
12Mingos, Howard, ed. (1946). The Aircraft Year Book for 1946(PDF). New York, New York: Lancair Publishers. p.392. Retrieved 13 October 2026.