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Franklin Engine Company: The Franklin 2 series of American two-cylinder air-cooled horizontally opposed aircraft engines were produced in the 1930s and 1940s.
In 1975 the government of Poland bought the company and moved it to Rzeszów, first under the name PZL-Franklin and later PZL-F. The company is now called Franklin Aircraft Engines Sp. z o.o. with the address ul. Chełmińska 208 in 86-300 Grudziądz city in Poland. [4] At Aero Friedrichshafen 2016 the company had new engines on display.
Pages in category "Franklin aircraft engines" ... This list may not reflect recent changes. F. Franklin 2 series; Franklin Engine Company; Franklin O-150; Franklin O-175;
153 Series (153in 3; gasoline or diesel) 175 Series (175in 3; diesel) 182 Series (182in 3; gasoline or diesel) 344 Series (344in 3; diesel) 433 Series (200in 3; gasoline or diesel) B Series (116 or 125in 3; gasoline) E Series (460, 510, or 563in 3; gasoline or diesel) G Series (138, 149, or 160in 3; gasoline or propane) W Series (201 or 226in 3 ...
The Franklin O-805 (company designation 12AC) was an American air-cooled aircraft piston engine, designed in the mid-1940s and was to be used in radio-controlled pilotless drones that were to be guided from an accompanying control plane. Due to project requirement changes and cancellations the engine was not produced.
Introduced in 1949, it had an open tubework tail boom reminiscent of the Bell Model 30 and three seats. 47E Powered by a 200 hp (150 kW) Franklin 6V4-200-C32 engine. 47F Bell 47G 47G Combines a 200 hp (149 kW) Franklin engine with the three-seat configuration of the 47D-1 and introduced the twin saddle-bag fuel tank configuration. 47G-2
In 1930 Franklin introduced a new type of engine which ultimately produced 100 horsepower (75 kW), with one of the highest power-to-weight ratios of the time. In 1932, in response to competition amongst luxury car makers, Franklin brought out a twelve-cylinder engine. [11] Air cooled with 398 cubic inches (6.5 L), it developed 150 hp (110 kW).
The Franklin O-150 (company designation 4AC-150) was an American air-cooled aircraft engine of the late 1930s. The engine was of four-cylinder, horizontally-opposed layout and displaced 150 cu in (2 L). The power output was nominally 40 hp (30 kW).