Selection Methodology of an Electric Actuator for Nose Landing Gear of a Light Weight Aircraft

Selection Methodology of an Electric Actuator for Nose Landing Gear of a Light Weight Aircraft

Landing gear system of an aircraft enables it to take off and land with safety and comfort. Because of the horizontal and vertical velocity of aircraft, upon landing, the complete aircraft undergoes different forcing functions in the form of the impact force that is absorbed by landing gears, shock...

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Bibliographic Details
Main Authors: Taimur Ali Shams, Syed Irtiza Ali Shah, Muhammad Ayaz Ahmad, Kashif Mehmood, Waseem Ahmad, Syed Tauqeer ul Islam Rizvi
Format: Article
Language:English
Published: MDPI AG 2020-12-01
Series:Applied Sciences
Subjects:
nose landing gear
retraction mechanism
electro-mechanical actuators
impact force
locking loads
Online Access:https://www.mdpi.com/2076-3417/10/23/8730

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https://www.mdpi.com/2076-3417/10/23/8730

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