SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN
Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver...
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| creator | RUHAN, Desmond MARTIN, Andrew ZIOLKOWSKI, Craig ABLER, Todd |
| description | Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver angle of a throttle (270, 410) controller in response to the first control signal, comparing (530) the throttle (270, 410) resolver angle to a threshold throttle (270, 410) angle, and generating (540) a pilot warning in response to the first control signal and the throttle (270, 410) resolver angle exceeding the threshold throttle (270, 410) angle. |
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An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver angle of a throttle (270, 410) controller in response to the first control signal, comparing (530) the throttle (270, 410) resolver angle to a threshold throttle (270, 410) angle, and generating (540) a pilot warning in response to the first control signal and the throttle (270, 410) resolver angle exceeding the threshold throttle (270, 410) angle.</description><language>eng ; fre ; ger</language><subject>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</subject><creationdate>2021</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=20211013&DB=EPODOC&CC=EP&NR=3892544A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211013&DB=EPODOC&CC=EP&NR=3892544A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>RUHAN, Desmond</creatorcontrib><creatorcontrib>MARTIN, Andrew</creatorcontrib><creatorcontrib>ZIOLKOWSKI, Craig</creatorcontrib><creatorcontrib>ABLER, Todd</creatorcontrib><title>SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN</title><description>Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver angle of a throttle (270, 410) controller in response to the first control signal, comparing (530) the throttle (270, 410) resolver angle to a threshold throttle (270, 410) angle, and generating (540) a pilot warning in response to the first control signal and the throttle (270, 410) resolver angle exceeding the threshold throttle (270, 410) angle.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAIjgwOcfVVcPRzUfB1DfHwd1EI8VcICHINc_ULUQj18_QLcfVzcXVRcPQMcg5ydAtRcPVz9_RzVQj2CA1x8Q_342FgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxhaWRqYmJo6GxkQoAQBujiqB</recordid><startdate>20211013</startdate><enddate>20211013</enddate><creator>RUHAN, Desmond</creator><creator>MARTIN, Andrew</creator><creator>ZIOLKOWSKI, Craig</creator><creator>ABLER, Todd</creator><scope>EVB</scope></search><sort><creationdate>20211013</creationdate><title>SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN</title><author>RUHAN, Desmond ; MARTIN, Andrew ; ZIOLKOWSKI, Craig ; ABLER, Todd</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3892544A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>RUHAN, Desmond</creatorcontrib><creatorcontrib>MARTIN, Andrew</creatorcontrib><creatorcontrib>ZIOLKOWSKI, Craig</creatorcontrib><creatorcontrib>ABLER, Todd</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>RUHAN, Desmond</au><au>MARTIN, Andrew</au><au>ZIOLKOWSKI, Craig</au><au>ABLER, Todd</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN</title><date>2021-10-13</date><risdate>2021</risdate><abstract>Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver angle of a throttle (270, 410) controller in response to the first control signal, comparing (530) the throttle (270, 410) resolver angle to a threshold throttle (270, 410) angle, and generating (540) a pilot warning in response to the first control signal and the throttle (270, 410) resolver angle exceeding the threshold throttle (270, 410) angle.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| 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 | SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN |
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