PROCEDE DE PILOTAGE D'UN MOTEUR A COMBUSTION INTERNE
A method for controlling an internal combustion engine includes acquiring, at a first operating point of the engine, a value of a first characteristic parameter of the first operating point, and deducing from the value a first liquid coolant temperature setpoint in the engine and a first richness se...
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| creator | PETILLON YOHANN |
| description | A method for controlling an internal combustion engine includes acquiring, at a first operating point of the engine, a value of a first characteristic parameter of the first operating point, and deducing from the value a first liquid coolant temperature setpoint in the engine and a first richness setpoint of a mixture of air and fuel to be admitted into the engine. The method also includes acquiring, on passing a second operating point different from the first, the value of the parameter and deducing from the value, second setpoints for temperature and richness. When the second temperature setpoint is strictly lower than the first temperature setpoint, the method includes determining an additional richness to be added to the second richness setpoint, acquiring a burned gas temperature, and progressively reducing the additional richness as a function of the burned gas temperature acquired. |
| format | Patent |
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The method also includes acquiring, on passing a second operating point different from the first, the value of the parameter and deducing from the value, second setpoints for temperature and richness. When the second temperature setpoint is strictly lower than the first temperature setpoint, the method includes determining an additional richness to be added to the second richness setpoint, acquiring a burned gas temperature, and progressively reducing the additional richness as a function of the burned gas temperature acquired.</description><language>fre</language><subject>BLASTING ; COMBUSTION ENGINES ; CONTROLLING COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2016</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=20160610&DB=EPODOC&CC=FR&NR=3022591B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160610&DB=EPODOC&CC=FR&NR=3022591B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PETILLON YOHANN</creatorcontrib><title>PROCEDE DE PILOTAGE D'UN MOTEUR A COMBUSTION INTERNE</title><description>A method for controlling an internal combustion engine includes acquiring, at a first operating point of the engine, a value of a first characteristic parameter of the first operating point, and deducing from the value a first liquid coolant temperature setpoint in the engine and a first richness setpoint of a mixture of air and fuel to be admitted into the engine. The method also includes acquiring, on passing a second operating point different from the first, the value of the parameter and deducing from the value, second setpoints for temperature and richness. When the second temperature setpoint is strictly lower than the first temperature setpoint, the method includes determining an additional richness to be added to the second richness setpoint, acquiring a burned gas temperature, and progressively reducing the additional richness as a function of the burned gas temperature acquired.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAJCPJ3dnVxVQCiAE8f_xBHdyBbPdRPwdc_xDU0SMFRwdnf1yk0OMTT30_B0y_ENcjPlYeBNS0xpziVF0pzMyi4uYY4e-imFuTHpxYXJCan5qWWxLsFGRsYGZlaGjoZGhOhBABZ1Sa6</recordid><startdate>20160610</startdate><enddate>20160610</enddate><creator>PETILLON YOHANN</creator><scope>EVB</scope></search><sort><creationdate>20160610</creationdate><title>PROCEDE DE PILOTAGE D'UN MOTEUR A COMBUSTION INTERNE</title><author>PETILLON YOHANN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR3022591B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2016</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>PETILLON YOHANN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PETILLON YOHANN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>PROCEDE DE PILOTAGE D'UN MOTEUR A COMBUSTION INTERNE</title><date>2016-06-10</date><risdate>2016</risdate><abstract>A method for controlling an internal combustion engine includes acquiring, at a first operating point of the engine, a value of a first characteristic parameter of the first operating point, and deducing from the value a first liquid coolant temperature setpoint in the engine and a first richness setpoint of a mixture of air and fuel to be admitted into the engine. The method also includes acquiring, on passing a second operating point different from the first, the value of the parameter and deducing from the value, second setpoints for temperature and richness. When the second temperature setpoint is strictly lower than the first temperature setpoint, the method includes determining an additional richness to be added to the second richness setpoint, acquiring a burned gas temperature, and progressively reducing the additional richness as a function of the burned gas temperature acquired.</abstract><oa>free_for_read</oa></addata></record> |
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| language | fre |
| recordid | cdi_epo_espacenet_FR3022591B1 |
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| subjects | BLASTING COMBUSTION ENGINES CONTROLLING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | PROCEDE DE PILOTAGE D'UN MOTEUR A COMBUSTION INTERNE |
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