AIRCRAFT POWER SYSTEM AND METHOD FOR CONTROLLING AIRCRAFT SYSTEM

AIRCRAFT POWER SYSTEM AND METHOD FOR CONTROLLING AIRCRAFT SYSTEM

PROBLEM TO BE SOLVED: To provide a system and a method for controlling an aircraft power. SOLUTION: This system according to one embodiment comprises an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric mo...

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Hauptverfasser: TOY DAVID K, GROAT J EVERETT, WHITE JEFFREY J
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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creator TOY DAVID K
GROAT J EVERETT
WHITE JEFFREY J
description PROBLEM TO BE SOLVED: To provide a system and a method for controlling an aircraft power. SOLUTION: This system according to one embodiment comprises an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to change the output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes. Indivisual control modes correspond to an operation mode of aircraft and a non-zero output level of the electric motor. In further embodiment, the motor controller can be substituted for each other, e.g, when one motor controller mal-functions. COPYRIGHT: (C)2008,JPO&INPIT
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SOLUTION: This system according to one embodiment comprises an electric motor, an aircraft load coupled to the electric motor and powered by the electric motor, and a motor controller coupled to the electric motor to change the output of the electric motor. The motor controller is changeable among a fixed number of preset controller modes. Indivisual control modes correspond to an operation mode of aircraft and a non-zero output level of the electric motor. In further embodiment, the motor controller can be substituted for each other, e.g, when one motor controller mal-functions. 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subjects AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title AIRCRAFT POWER SYSTEM AND METHOD FOR CONTROLLING AIRCRAFT SYSTEM
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