SYSTEM AND METHOD FOR CONTROLLING PROPELLER-DRIVEN AIRCRAFT

A method and a system are provided for controlling a propeller-driven aircraft, the aircraft powered by at least one engine (110) having at least one propeller (120) associated therewith. At least one control input for the at least one engine (110) is received at an engine controller (210) for the a...

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Hauptverfasser: LISIO, Carmine, FORTIN, Frederic
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creator LISIO, Carmine
FORTIN, Frederic
description A method and a system are provided for controlling a propeller-driven aircraft, the aircraft powered by at least one engine (110) having at least one propeller (120) associated therewith. At least one control input for the at least one engine (110) is received at an engine controller (210) for the at least one engine (110). The engine controller (210) determines, based on the at least one control input, a setpoint for a rotational speed of the at least one propeller (120) and outputs, to a propeller controller (220) for the at least one propeller (120), a control signal comprising instructions to adjust the rotational speed of the at least one propeller (120) to the setpoint.
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At least one control input for the at least one engine (110) is received at an engine controller (210) for the at least one engine (110). The engine controller (210) determines, based on the at least one control input, a setpoint for a rotational speed of the at least one propeller (120) and outputs, to a propeller controller (220) for the at least one propeller (120), a control signal comprising instructions to adjust the rotational speed of the at least one propeller (120) to the setpoint.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; GAS-TURBINE PLANTS ; HEATING ; HELICOPTERS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2020</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20200812&amp;DB=EPODOC&amp;CC=EP&amp;NR=3693573A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20200812&amp;DB=EPODOC&amp;CC=EP&amp;NR=3693573A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LISIO, Carmine</creatorcontrib><creatorcontrib>FORTIN, Frederic</creatorcontrib><title>SYSTEM AND METHOD FOR CONTROLLING PROPELLER-DRIVEN AIRCRAFT</title><description>A method and a system are provided for controlling a propeller-driven aircraft, the aircraft powered by at least one engine (110) having at least one propeller (120) associated therewith. 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language eng ; fre ; ger
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source esp@cenet
subjects AEROPLANES
AIR INTAKES FOR JET-PROPULSION PLANTS
AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
COSMONAUTICS
GAS-TURBINE PLANTS
HEATING
HELICOPTERS
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
title SYSTEM AND METHOD FOR CONTROLLING PROPELLER-DRIVEN AIRCRAFT
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