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Power speed reduction units for general aviation: Simplified gear design piston-powered, propeller-driven general aviation aircrafts


Article Information

Title: Power speed reduction units for general aviation: Simplified gear design piston-powered, propeller-driven general aviation aircrafts

Authors: Luca Piancastelli, Stefano Cassani

Journal: ARPN Journal of Engineering and Applied Sciences

HEC Recognition History
Category From To
Y 2023-07-01 2024-09-30
Y 2022-07-01 2023-06-30
Y 2021-07-01 2022-06-30
X 2020-07-01 2021-06-30

Publisher: Khyber Medical College, Peshawar

Country: Pakistan

Year: 2017

Volume: 12

Issue: 3

Language: English

Categories

Abstract

The power speed reduction unit (PSRU) is the device that is loaded by the piston engine and the thruster. The thruster, a propeller of a fan, acts on the PSRU to extract the required power at the optimum speed for the aerial vehicle. Inertia, thrust and vibrations load the PRSU. PSRU has been the problem of the years before WWII. These problems periodically come back from common design errors or from the introduction of new technologies. For historical reasons, FAR and JAR do not allow the use of belt and chain transmissions in PRSUs for aircrafts. However, recent advances in timing belts make it possible to manufacture lubrication free PRSUs. Multi-Groove-V belts have also been used successfully in helicopters and homebuilt aircrafts. Belt PRSU are critical in design and they will be fully analyzed in another paper. This third paper deals with the general problem of designing the PRSU gear drives on a general aviation aircraft [1-2].


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