INTELLIGENT INTEGRATED PROPULSION CONTROL SYSTEM AND METHOD
Control systems and methods for an aircraft propulsion system are disclosed in which the propulsion control system (140) is integrated to intelligently control aircraft propulsion and minimize transient effects from the power demands of other aircraft subsystems (120, 130, 152)
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creator | BURNS, DONALD W ZELLER, ROBERT J |
description | Control systems and methods for an aircraft propulsion system are disclosed in which the propulsion control system (140) is integrated to intelligently control aircraft propulsion and minimize transient effects from the power demands of other aircraft subsystems (120, 130, 152) |
format | Patent |
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language | eng ; fre |
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source | esp@cenet |
subjects | AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
title | INTELLIGENT INTEGRATED PROPULSION CONTROL SYSTEM AND METHOD |
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