DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY
This control device for a propulsion system, which comprises means for computing a blade-pitch setpoint for at least one propeller of the propulsion system, the computing means using a predictive model of the performance of the propeller that takes into account at least one flight speed so as to ada...
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creator | GIANNAKAKIS, Panagiotis YESILCIMEN, Henri BINDER, Anthony |
description | This control device for a propulsion system, which comprises means for computing a blade-pitch setpoint for at least one propeller of the propulsion system, the computing means using a predictive model of the performance of the propeller that takes into account at least one flight speed so as to adapt a blade-pitch angle setpoint, is characterized in that the predictive model of the performance of the propeller is configured to use polar curves implemented in the form of a mathematical law. |
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fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINE PLANTS IN GENERAL ; HEATING ; HELICOPTERS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2024</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&date=20241009&DB=EPODOC&CC=EP&NR=4441339A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241009&DB=EPODOC&CC=EP&NR=4441339A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GIANNAKAKIS, Panagiotis</creatorcontrib><creatorcontrib>YESILCIMEN, Henri</creatorcontrib><creatorcontrib>BINDER, Anthony</creatorcontrib><title>DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY</title><description>This control device for a propulsion system, which comprises means for computing a blade-pitch setpoint for at least one propeller of the propulsion system, the computing means using a predictive model of the performance of the propeller that takes into account at least one flight speed so as to adapt a blade-pitch angle setpoint, is characterized in that the predictive model of the performance of the propeller is configured to use polar curves implemented in the form of a mathematical law.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PERFORMING OPERATIONS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyrEKwjAQgOEsDqK-w72AQ2kXxzNem4OY1MtFcSpF4iRaqO-PCD6A088H_9KcDnRmS9BGAUyJk3Lo4MLqQKjLHpVjgNhCL7En70nSV0gSA2Zlix40yz4e0ToOJNe1WdzHx1w2v64MtKTWbcv0Gso8jbfyLO-B-qZpqrreYVX_sXwAbgovUA</recordid><startdate>20241009</startdate><enddate>20241009</enddate><creator>GIANNAKAKIS, Panagiotis</creator><creator>YESILCIMEN, Henri</creator><creator>BINDER, Anthony</creator><scope>EVB</scope></search><sort><creationdate>20241009</creationdate><title>DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY</title><author>GIANNAKAKIS, Panagiotis ; YESILCIMEN, Henri ; BINDER, Anthony</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4441339A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PERFORMING OPERATIONS</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>GIANNAKAKIS, Panagiotis</creatorcontrib><creatorcontrib>YESILCIMEN, Henri</creatorcontrib><creatorcontrib>BINDER, Anthony</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GIANNAKAKIS, Panagiotis</au><au>YESILCIMEN, Henri</au><au>BINDER, Anthony</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY</title><date>2024-10-09</date><risdate>2024</risdate><abstract>This control device for a propulsion system, which comprises means for computing a blade-pitch setpoint for at least one propeller of the propulsion system, the computing means using a predictive model of the performance of the propeller that takes into account at least one flight speed so as to adapt a blade-pitch angle setpoint, is characterized in that the predictive model of the performance of the propeller is configured to use polar curves implemented in the form of a mathematical law.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS |
title | DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY |
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