USA

Wright Cyclone R 2600 Aircraft Engine Technical Details Working volume-29.8 liters Compression ratio-6.4 Weight-595 kg Diameter-1400 mm Cylinder diameter-174.6 mm Take-off power – 1400 hp Wright Cyclone R 2600 Aircraft Engine In 1909, the world-famous pioneers of aviation, the American brothers Wilbur and Orville Wright, founded the company for the production of aircraft engines. Initially, …

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Allison V-1710 Aircraft Engine Technical Specifications Working volume-28 l Compression ratio-6.5 Weight-650 kg Length-744 mm Height-928 mm Cylinder diameter-139.7 mm Take-off power – 1165 hp Allison V-1710 Aircraft Engine Details The first aircraft engine for the US Army Air Force was developed by Allison in 1924. It was an experimental 24-cylinder air-cooled engine with an …

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Bell R-63 Fighter Aircraft Technical Specifications Crew – 1 person Engine – Allison V-1710-93 Power-1500 hp Wingspan-11.68 m Wing area – 23.04 sq. m Empty aircraft weight-2569 kg Maximum take-off weight-4763 kg Maximum speed-657 km / h Practical ceiling – 13,106 m Maximum range-3540 km Armament – 1×37 mm cannon and 4×12. 7 mm Browning …

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