METHOD OF OPERATING AN ENGINE ASSEMBLY
A method of operating a compoundable engine (10) that includes a turbine (22) having a turbine shaft (26) and an intermittent internal combustion engine (12) having an engine shaft (14). The engine shaft (14) is rotated at a first rotational speed. The turbine (22) is driven by exhaust gases of the...
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| creator | VILLENEUVE, Bruno THOMASSIN, Jean FONTAINE, Mike |
| description | A method of operating a compoundable engine (10) that includes a turbine (22) having a turbine shaft (26) and an intermittent internal combustion engine (12) having an engine shaft (14). The engine shaft (14) is rotated at a first rotational speed. The turbine (22) is driven by exhaust gases of the intermittent internal combustion engine (12) to rotate the turbine shaft (26) while the engine shaft (14) rotates independently from the turbine shaft (26). A rotatable load (L) is driven with the turbine shaft (26). A rotational speed of the engine shaft (14) is increased from the first rotational speed until the turbine shaft (26) reaches a predetermined rotational speed. After the turbine shaft (26) has reached the predetermined rotational speed, the rotational speed of the engine shaft (14) is adjusted until the turbine shaft (26) and the engine shaft (14) are drivingly engageable with each other, and the turbine shaft (26) with the engine shaft (14) are engaged such that both are in driving engagement with the rotatable load (L). |
| format | Patent |
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The engine shaft (14) is rotated at a first rotational speed. The turbine (22) is driven by exhaust gases of the intermittent internal combustion engine (12) to rotate the turbine shaft (26) while the engine shaft (14) rotates independently from the turbine shaft (26). A rotatable load (L) is driven with the turbine shaft (26). A rotational speed of the engine shaft (14) is increased from the first rotational speed until the turbine shaft (26) reaches a predetermined rotational speed. After the turbine shaft (26) has reached the predetermined rotational speed, the rotational speed of the engine shaft (14) is adjusted until the turbine shaft (26) and the engine shaft (14) are drivingly engageable with each other, and the turbine shaft (26) with the engine shaft (14) are engaged such that both are in driving engagement with the rotatable load (L).</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 ; COMBUSTION ENGINES IN GENERAL ; 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 ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2022</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=20220727&DB=EPODOC&CC=EP&NR=3456939B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220727&DB=EPODOC&CC=EP&NR=3456939B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VILLENEUVE, Bruno</creatorcontrib><creatorcontrib>THOMASSIN, Jean</creatorcontrib><creatorcontrib>FONTAINE, Mike</creatorcontrib><title>METHOD OF OPERATING AN ENGINE ASSEMBLY</title><description>A method of operating a compoundable engine (10) that includes a turbine (22) having a turbine shaft (26) and an intermittent internal combustion engine (12) having an engine shaft (14). The engine shaft (14) is rotated at a first rotational speed. The turbine (22) is driven by exhaust gases of the intermittent internal combustion engine (12) to rotate the turbine shaft (26) while the engine shaft (14) rotates independently from the turbine shaft (26). A rotatable load (L) is driven with the turbine shaft (26). A rotational speed of the engine shaft (14) is increased from the first rotational speed until the turbine shaft (26) reaches a predetermined rotational speed. After the turbine shaft (26) has reached the predetermined rotational speed, the rotational speed of the engine shaft (14) is adjusted until the turbine shaft (26) and the engine shaft (14) are drivingly engageable with each other, and the turbine shaft (26) with the engine shaft (14) are engaged such that both are in driving engagement with the rotatable load (L).</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>COMBUSTION ENGINES IN GENERAL</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>INTERNAL-COMBUSTION PISTON ENGINES</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFDzdQ3x8HdR8HdT8A9wDXIM8fRzV3D0U3D1c_f0c1VwDA529XXyieRhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcYmpmaWxpZOhsZEKAEAaS0jCQ</recordid><startdate>20220727</startdate><enddate>20220727</enddate><creator>VILLENEUVE, Bruno</creator><creator>THOMASSIN, Jean</creator><creator>FONTAINE, Mike</creator><scope>EVB</scope></search><sort><creationdate>20220727</creationdate><title>METHOD OF OPERATING AN ENGINE ASSEMBLY</title><author>VILLENEUVE, Bruno ; THOMASSIN, Jean ; FONTAINE, Mike</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3456939B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</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>COMBUSTION ENGINES IN GENERAL</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>INTERNAL-COMBUSTION PISTON ENGINES</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>VILLENEUVE, Bruno</creatorcontrib><creatorcontrib>THOMASSIN, Jean</creatorcontrib><creatorcontrib>FONTAINE, Mike</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VILLENEUVE, Bruno</au><au>THOMASSIN, Jean</au><au>FONTAINE, Mike</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD OF OPERATING AN ENGINE ASSEMBLY</title><date>2022-07-27</date><risdate>2022</risdate><abstract>A method of operating a compoundable engine (10) that includes a turbine (22) having a turbine shaft (26) and an intermittent internal combustion engine (12) having an engine shaft (14). The engine shaft (14) is rotated at a first rotational speed. The turbine (22) is driven by exhaust gases of the intermittent internal combustion engine (12) to rotate the turbine shaft (26) while the engine shaft (14) rotates independently from the turbine shaft (26). A rotatable load (L) is driven with the turbine shaft (26). A rotational speed of the engine shaft (14) is increased from the first rotational speed until the turbine shaft (26) reaches a predetermined rotational speed. After the turbine shaft (26) has reached the predetermined rotational speed, the rotational speed of the engine shaft (14) is adjusted until the turbine shaft (26) and the engine shaft (14) are drivingly engageable with each other, and the turbine shaft (26) with the engine shaft (14) are engaged such that both are in driving engagement with the rotatable load (L).</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 COMBUSTION ENGINES IN GENERAL 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 INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | METHOD OF OPERATING AN ENGINE ASSEMBLY |
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