Crankshaft of Aircraft Two-cylinder Engine

Crankshaft of Aircraft Two-cylinder Engine

Funkční vzorek

This crankshaft is designed for a supercharged two-stroke compression-ignition opposed-piston aircraft engine. Crankshaft construction, therefore, largely reflects the requirements of high stiffness and low weight simultaneously. Semi-finished crankshaft is smith forging of material 32CrMo4. The final design is whole machined and there is used chemical-heat treatment of the exposed areas.

This crankshaft is designed for a supercharged two-stroke compression-ignition opposed-piston aircraft engine. Crankshaft construction, therefore, largely reflects the requirements of high stiffness and low weight simultaneously. Semi-finished crankshaft is smith forging of material 32CrMo4. The final design is whole machined and there is used chemical-heat treatment of the exposed areas.

crankshaft, two-cylinder engine, aircraft engine

crankshaft, two-cylinder engine, aircraft engine

Laboratoře C3 Ústavu automobilního a dopravního zařízení Fakulty strojního inženýrství Vysokého učení technického v Brně – Technická 2896/2, 616 69 Brno

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http://www.iae.fme.vutbr.cz/cs/system/files/2011_FV_Drapal_--_Klikovy_hridel_letadlovy.pdf