DIGITAL COMMUNICATIONS BETWEEN AIRCRAFT COMPUTER AND ENGINE COMPUTER
There are described herein methods and systems for providing an engine computer with a power request having been determined by an aircraft computer. The power request is sent over a communication bus and once it reaches the engine computer, the latency due to the different update rates of the engine...
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creator | PEDRAMI, REZA SAARIO, TEUVO MARTIN, AARON |
description | There are described herein methods and systems for providing an engine computer with a power request having been determined by an aircraft computer. The power request is sent over a communication bus and once it reaches the engine computer, the latency due to the different update rates of the engine computer and the aircraft computer are compensated for.
Des méthodes et des systèmes sont décrits pour fournir un ordinateur de moteur, une demande dalimentation ayant été déterminée par un ordinateur daéronef. La demande dalimentation est envoyée au moyen dun bus de communication et, une fois quelle atteint lordinateur de moteur, la latence causée par les différents rythmes de mise à jour de lordinateur de moteur et de lordinateur daéronef est compensée. |
format | Patent |
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Des méthodes et des systèmes sont décrits pour fournir un ordinateur de moteur, une demande dalimentation ayant été déterminée par un ordinateur daéronef. La demande dalimentation est envoyée au moyen dun bus de communication et, une fois quelle atteint lordinateur de moteur, la latence causée par les différents rythmes de mise à jour de lordinateur de moteur et de lordinateur daéronef est compensée.</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</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=20240220&DB=EPODOC&CC=CA&NR=2955528C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240220&DB=EPODOC&CC=CA&NR=2955528C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PEDRAMI, REZA</creatorcontrib><creatorcontrib>SAARIO, TEUVO</creatorcontrib><creatorcontrib>MARTIN, AARON</creatorcontrib><title>DIGITAL COMMUNICATIONS BETWEEN AIRCRAFT COMPUTER AND ENGINE COMPUTER</title><description>There are described herein methods and systems for providing an engine computer with a power request having been determined by an aircraft computer. The power request is sent over a communication bus and once it reaches the engine computer, the latency due to the different update rates of the engine computer and the aircraft computer are compensated for.
Des méthodes et des systèmes sont décrits pour fournir un ordinateur de moteur, une demande dalimentation ayant été déterminée par un ordinateur daéronef. La demande dalimentation est envoyée au moyen dun bus de communication et, une fois quelle atteint lordinateur de moteur, la latence causée par les différents rythmes de mise à jour de lordinateur de moteur et de lordinateur daéronef est compensée.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBx8XT3DHH0UXD29_UN9fN0dgzx9PcLVnByDQl3dfVTcPQMcg5ydAsByQeEhrgGKTj6uSi4-rl7-rnCxXgYWNMSc4pTeaE0N4O8m2uIs4duakF-fGpxQWJyal5qSbyzo5GlqampkYWzMWEVAMVrKx0</recordid><startdate>20240220</startdate><enddate>20240220</enddate><creator>PEDRAMI, REZA</creator><creator>SAARIO, TEUVO</creator><creator>MARTIN, AARON</creator><scope>EVB</scope></search><sort><creationdate>20240220</creationdate><title>DIGITAL COMMUNICATIONS BETWEEN AIRCRAFT COMPUTER AND ENGINE COMPUTER</title><author>PEDRAMI, REZA ; SAARIO, TEUVO ; MARTIN, AARON</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2955528C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2024</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>PEDRAMI, REZA</creatorcontrib><creatorcontrib>SAARIO, TEUVO</creatorcontrib><creatorcontrib>MARTIN, AARON</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PEDRAMI, REZA</au><au>SAARIO, TEUVO</au><au>MARTIN, AARON</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DIGITAL COMMUNICATIONS BETWEEN AIRCRAFT COMPUTER AND ENGINE COMPUTER</title><date>2024-02-20</date><risdate>2024</risdate><abstract>There are described herein methods and systems for providing an engine computer with a power request having been determined by an aircraft computer. The power request is sent over a communication bus and once it reaches the engine computer, the latency due to the different update rates of the engine computer and the aircraft computer are compensated for.
Des méthodes et des systèmes sont décrits pour fournir un ordinateur de moteur, une demande dalimentation ayant été déterminée par un ordinateur daéronef. La demande dalimentation est envoyée au moyen dun bus de communication et, une fois quelle atteint lordinateur de moteur, la latence causée par les différents rythmes de mise à jour de lordinateur de moteur et de lordinateur daéronef est compensée.</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | DIGITAL COMMUNICATIONS BETWEEN AIRCRAFT COMPUTER AND ENGINE COMPUTER |
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