Single stage or multi-stage compressor for a turbocharger
The present invention relates to a turbocharger for use in an internal combustion engine, and, more particularly, to a turbocharger having a two-stage compressor. A turbocharger for an internal combustion engine has a compressor operable as a single stage or multi-stage compressor. A first compresso...
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creator | Houtz, Phillip J |
description | The present invention relates to a turbocharger for use in an internal combustion engine, and, more particularly, to a turbocharger having a two-stage compressor.
A turbocharger for an internal combustion engine has a compressor operable as a single stage or multi-stage compressor. A first compressor stage includes a first compressor wheel carried by a shaft, an axially extending first inlet and a radially extending first outlet. A second compressor stage includes a second compressor wheel carried by the shaft and axially extending second inlet and a radially extending second outlet. An interstage duct fluidly connects in series the first outlet of the first compressor with the second inlet of the second compressor. The interstage duct includes a bypass opening includes in communication with an ambient environment. A valve is positioned within the interstage duct. The valve is moveable to and between a first position to close the interstage duct and a second position to close the bypass opening. |
format | Patent |
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A turbocharger for an internal combustion engine has a compressor operable as a single stage or multi-stage compressor. A first compressor stage includes a first compressor wheel carried by a shaft, an axially extending first inlet and a radially extending first outlet. A second compressor stage includes a second compressor wheel carried by the shaft and axially extending second inlet and a radially extending second outlet. An interstage duct fluidly connects in series the first outlet of the first compressor with the second inlet of the second compressor. The interstage duct includes a bypass opening includes in communication with an ambient environment. A valve is positioned within the interstage duct. The valve is moveable to and between a first position to close the interstage duct and a second position to close the bypass opening.</description><language>eng</language><creationdate>2002</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6442936$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,780,802,885,64039</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6442936$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Houtz, Phillip J</creatorcontrib><creatorcontrib>Caterpillar Inc</creatorcontrib><title>Single stage or multi-stage compressor for a turbocharger</title><description>The present invention relates to a turbocharger for use in an internal combustion engine, and, more particularly, to a turbocharger having a two-stage compressor.
A turbocharger for an internal combustion engine has a compressor operable as a single stage or multi-stage compressor. A first compressor stage includes a first compressor wheel carried by a shaft, an axially extending first inlet and a radially extending first outlet. A second compressor stage includes a second compressor wheel carried by the shaft and axially extending second inlet and a radially extending second outlet. An interstage duct fluidly connects in series the first outlet of the first compressor with the second inlet of the second compressor. The interstage duct includes a bypass opening includes in communication with an ambient environment. A valve is positioned within the interstage duct. The valve is moveable to and between a first position to close the interstage duct and a second position to close the bypass opening.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2002</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZLAMzsxLz0lVKC5JTE9VyC9SyC3NKcnUhXCT83MLilKLi4HCaUCcqFBSWpSUn5yRWJSeWsTDwJqWmFOcyguluRkU3FxDnD10S4sLEktS80qK49OLEkGUgZmJiZGlsZkxEUoAFYEvsg</recordid><startdate>20020903</startdate><enddate>20020903</enddate><creator>Houtz, Phillip J</creator><scope>EFH</scope></search><sort><creationdate>20020903</creationdate><title>Single stage or multi-stage compressor for a turbocharger</title><author>Houtz, Phillip J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_064429363</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2002</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Houtz, Phillip J</creatorcontrib><creatorcontrib>Caterpillar Inc</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Houtz, Phillip J</au><aucorp>Caterpillar Inc</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Single stage or multi-stage compressor for a turbocharger</title><date>2002-09-03</date><risdate>2002</risdate><abstract>The present invention relates to a turbocharger for use in an internal combustion engine, and, more particularly, to a turbocharger having a two-stage compressor.
A turbocharger for an internal combustion engine has a compressor operable as a single stage or multi-stage compressor. A first compressor stage includes a first compressor wheel carried by a shaft, an axially extending first inlet and a radially extending first outlet. A second compressor stage includes a second compressor wheel carried by the shaft and axially extending second inlet and a radially extending second outlet. An interstage duct fluidly connects in series the first outlet of the first compressor with the second inlet of the second compressor. The interstage duct includes a bypass opening includes in communication with an ambient environment. A valve is positioned within the interstage duct. The valve is moveable to and between a first position to close the interstage duct and a second position to close the bypass opening.</abstract><oa>free_for_read</oa></addata></record> |
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title | Single stage or multi-stage compressor for a turbocharger |
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