SUPPLEMENTARY AIR ASSEMBLY FOR AN ENGINE
An internal combustion engine (2) includes a crankcase (4) including a crankshaft and at least one cylinder (6; 61, 62, 63, 64) coupled to the crankcase. The at least one cylinder has an intake port (14) and defines an internal combustion chamber (10). The engine further includes a throttle body ass...
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| creator | MCKOSKEY, G., Jay |
| description | An internal combustion engine (2) includes a crankcase (4) including a crankshaft and at least one cylinder (6; 61, 62, 63, 64) coupled to the crankcase. The at least one cylinder has an intake port (14) and defines an internal combustion chamber (10). The engine further includes a throttle body assembly (20) with a throttle valve (22) coupled to the intake port of the at least one cylinder and a throttle plate (26). Additionally, the engine includes a supplementary air inlet (42) fluidly coupled to the intake port and spaced apart from the throttle valve. The supplementary air inlet is configured to receive a flow of air from a location downstream of the throttle plate when the throttle plate is in a fully closed position and the flow of air is directed into the combustion chamber through the intake port for combustion therein.
L'invention concerne un moteur à combustion interne (2) comprenant un carter (4) de vilebrequin comprenant un vilebrequin et au moins un cylindre (6 ; 61, 62, 63, 64) couplé au carter de vilebrequin. Ledit cylindre possède un orifice d'admission (14) et délimite une chambre de combustion interne (10). Le moteur comprend en outre un ensemble corps de papillon (20) ayant un papillon des gaz (22) couplée à l'orifice d'admission dudit cylindre et au papillon (26). En outre, le moteur comprend une entrée d'air supplémentaire (42) en connexion fluidique avec l'orifice d'admission et espacée du papillon des gaz. L'entrée d'air supplémentaire est conçue pour recevoir un écoulement d'air depuis un emplacement situé en aval du papillon lorsque celui-ci est dans une position complètement fermée et l'écoulement d'air est dirigé dans la chambre de combustion à travers l'orifice d'admission pour y alimenter la combustion. |
| format | Patent |
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L'invention concerne un moteur à combustion interne (2) comprenant un carter (4) de vilebrequin comprenant un vilebrequin et au moins un cylindre (6 ; 61, 62, 63, 64) couplé au carter de vilebrequin. Ledit cylindre possède un orifice d'admission (14) et délimite une chambre de combustion interne (10). Le moteur comprend en outre un ensemble corps de papillon (20) ayant un papillon des gaz (22) couplée à l'orifice d'admission dudit cylindre et au papillon (26). En outre, le moteur comprend une entrée d'air supplémentaire (42) en connexion fluidique avec l'orifice d'admission et espacée du papillon des gaz. L'entrée d'air supplémentaire est conçue pour recevoir un écoulement d'air depuis un emplacement situé en aval du papillon lorsque celui-ci est dans une position complètement fermée et l'écoulement d'air est dirigé dans la chambre de combustion à travers l'orifice d'admission pour y alimenter la combustion.</description><language>eng ; fre</language><subject>BLASTING ; COMBUSTION ENGINES ; COMBUSTION ENGINES IN GENERAL ; CONTROLLING COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INTERNAL-COMBUSTION PISTON ENGINES ; LIGHTING ; MECHANICAL ENGINEERING ; SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF ; 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=20160915&DB=EPODOC&CC=WO&NR=2016144630A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160915&DB=EPODOC&CC=WO&NR=2016144630A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MCKOSKEY, G., Jay</creatorcontrib><title>SUPPLEMENTARY AIR ASSEMBLY FOR AN ENGINE</title><description>An internal combustion engine (2) includes a crankcase (4) including a crankshaft and at least one cylinder (6; 61, 62, 63, 64) coupled to the crankcase. The at least one cylinder has an intake port (14) and defines an internal combustion chamber (10). The engine further includes a throttle body assembly (20) with a throttle valve (22) coupled to the intake port of the at least one cylinder and a throttle plate (26). Additionally, the engine includes a supplementary air inlet (42) fluidly coupled to the intake port and spaced apart from the throttle valve. The supplementary air inlet is configured to receive a flow of air from a location downstream of the throttle plate when the throttle plate is in a fully closed position and the flow of air is directed into the combustion chamber through the intake port for combustion therein.
L'invention concerne un moteur à combustion interne (2) comprenant un carter (4) de vilebrequin comprenant un vilebrequin et au moins un cylindre (6 ; 61, 62, 63, 64) couplé au carter de vilebrequin. Ledit cylindre possède un orifice d'admission (14) et délimite une chambre de combustion interne (10). Le moteur comprend en outre un ensemble corps de papillon (20) ayant un papillon des gaz (22) couplée à l'orifice d'admission dudit cylindre et au papillon (26). En outre, le moteur comprend une entrée d'air supplémentaire (42) en connexion fluidique avec l'orifice d'admission et espacée du papillon des gaz. L'entrée d'air supplémentaire est conçue pour recevoir un écoulement d'air depuis un emplacement situé en aval du papillon lorsque celui-ci est dans une position complètement fermée et l'écoulement d'air est dirigé dans la chambre de combustion à travers l'orifice d'admission pour y alimenter la combustion.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION ENGINES IN GENERAL</subject><subject>CONTROLLING COMBUSTION ENGINES</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>SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAIDg0I8HH1dfULcQyKVHD0DFJwDA529XXyiVRw8wdy_BRc_dw9_Vx5GFjTEnOKU3mhNDeDsptriLOHbmpBfnxqcUFicmpeakl8uL-RgaGZoYmJmbGBo6ExcaoAnSkk9g</recordid><startdate>20160915</startdate><enddate>20160915</enddate><creator>MCKOSKEY, G., Jay</creator><scope>EVB</scope></search><sort><creationdate>20160915</creationdate><title>SUPPLEMENTARY AIR ASSEMBLY FOR AN ENGINE</title><author>MCKOSKEY, G., Jay</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2016144630A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2016</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION ENGINES IN GENERAL</topic><topic>CONTROLLING COMBUSTION ENGINES</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>SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>MCKOSKEY, G., Jay</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MCKOSKEY, G., Jay</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SUPPLEMENTARY AIR ASSEMBLY FOR AN ENGINE</title><date>2016-09-15</date><risdate>2016</risdate><abstract>An internal combustion engine (2) includes a crankcase (4) including a crankshaft and at least one cylinder (6; 61, 62, 63, 64) coupled to the crankcase. The at least one cylinder has an intake port (14) and defines an internal combustion chamber (10). The engine further includes a throttle body assembly (20) with a throttle valve (22) coupled to the intake port of the at least one cylinder and a throttle plate (26). Additionally, the engine includes a supplementary air inlet (42) fluidly coupled to the intake port and spaced apart from the throttle valve. The supplementary air inlet is configured to receive a flow of air from a location downstream of the throttle plate when the throttle plate is in a fully closed position and the flow of air is directed into the combustion chamber through the intake port for combustion therein.
L'invention concerne un moteur à combustion interne (2) comprenant un carter (4) de vilebrequin comprenant un vilebrequin et au moins un cylindre (6 ; 61, 62, 63, 64) couplé au carter de vilebrequin. Ledit cylindre possède un orifice d'admission (14) et délimite une chambre de combustion interne (10). Le moteur comprend en outre un ensemble corps de papillon (20) ayant un papillon des gaz (22) couplée à l'orifice d'admission dudit cylindre et au papillon (26). En outre, le moteur comprend une entrée d'air supplémentaire (42) en connexion fluidique avec l'orifice d'admission et espacée du papillon des gaz. L'entrée d'air supplémentaire est conçue pour recevoir un écoulement d'air depuis un emplacement situé en aval du papillon lorsque celui-ci est dans une position complètement fermée et l'écoulement d'air est dirigé dans la chambre de combustion à travers l'orifice d'admission pour y alimenter la combustion.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL CONTROLLING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MECHANICAL ENGINEERING SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF WEAPONS |
| title | SUPPLEMENTARY AIR ASSEMBLY FOR AN ENGINE |
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