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Szekely aircraft engines were three-cylinder radial engines built in Holland, Michigan in the 1920s and 30s. They were used to power small aircraft such as the Rearwin Junior, Taylor H-2 and American Eagle Eaglet. Often criticized for reliability issues and design flaws, many were replaced with better engines in their original airframes.
The Lawrance L-3 and L-4 were early aircraft piston engines with three radial cylinders, designed and built by the Lawrance Aero Engine Company in the early 1920s. The L-3 / L-4 series were marketed by the Wright Aeronautical Corporation as the Wright Gale after the acquisition of the Lawrance company.
Data from Compact Radial Engines General characteristics Type: Three cylinder, radial two-stroke aircraft engine Bore: 66 mm (2.60 in) Stroke: 42 mm (1.65 in) Displacement: 430 cc (20.75 cu in) Dry weight: 17 kg (37 lb) Components Valvetrain: rotary valve induction Oil system: premixed oil and fuel Cooling system: air cooled Reduction gear: none Performance Power output: 20 hp (15 kW) at 4200 ...
The LeBlond radial engines, later produced under the name Ken-Royce, were a family of 3-cylinder, 5-cylinder and 7-cylinder, air-cooled radial engines for aircraft, built in the 1930s by the LeBlond Aircraft Engine Corporation until the operation was sold to Rearwin Airplanes in 1937 and renamed Ken-Royce Engines.
At the Museo Nacional de Aeronáutica Argentina there is a three-cylinder Anzani semiradial in working order installed on a Bleriot 11. A Y three-cylinder engine is on display at the Engines hall at the same Museum; Brooklands Museum, Weybridge, U.K. has an Anzani 3-cylinder fan engine on static display.
Source: RMV, Able Experimental Aircraft Engine Co. [6] (Able Experimental Aircraft Engine Co., Altimizer, Hoverhawk ... Advanced Engine Design Spitfire 3 Cylinder;
For example, on a five-cylinder engine the firing order is 1, 3, 5, 2, 4, and back to cylinder 1. Moreover, this always leaves a one-piston gap between the piston on its combustion stroke and the piston on compression. The active stroke directly helps compress the next cylinder to fire, making the motion more uniform.
The 2si 808 is a family of in-line three cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by JLO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.