Aircraft for use with unit for reducing wheel friction forces during take-off run, has rolling resistance reduction device, whose performance weight load is equal to or greater than product of rolling friction coefficient at take-off run

摘要

The aircraft has a device for rolling resistance reduction, whose performance weight load is equal to or greater than the product of the rolling friction coefficient at the take-off run of the aircraft, without influence of a system and characteristic or operating speed of the take-off run. The maximum installed capacity of a motor assembly of the device for rolling resistance reduction based on the operating weight of the aircraft is provided. An independent claim is included for a method for operating an aircraft during take-off run.