CONFIGURATION OF LANDING GEAR ASSEMBLIES FOR AN AIRCRAFT
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United States of America Patent
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Issued Date -
Sep 24, 2020
app pub date -
Feb 24, 2020
filing date -
Feb 28, 2019
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Abstract
An aircraft having a retractable landing gear assembly configured to support some of the weight of the aircraft via one or more wheels, and another retractable non-wheeled landing gear assembly or device configured to support some of the weight of the aircraft via one or more “low-friction” supports such as an air cushion is disclosed. The aircraft may have a maximum take-off weight between 100 and 150 tonnes. There may be two main landing gears each carrying two wheels, a nose landing gear, and a central non-wheeled landing gear providing the low friction vertical support when the aircraft is moving on the ground/operating surface.
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