Premixing injector for gas turbine engines

dc.contributor.assigneeVirginia Tech Intellectual Properties, Inc.en
dc.contributor.assigneeElectric Jet, LLCen
dc.contributor.inventorO'Brien, Walter F. Jr.en
dc.contributor.inventorHomitz, Josephen
dc.contributor.inventorSykes, David M.en
dc.contributor.inventorVandsburger, Urien
dc.contributor.inventorLePera, Stephen D.en
dc.date.accessed2016-08-19en
dc.date.accessioned2016-08-24T17:55:02Zen
dc.date.available2016-08-24T17:55:02Zen
dc.date.filed2007-06-01en
dc.date.issued2011-01-18en
dc.description.abstractA premixing injector for use in gas turbine engines assists in the lean premixed injection of a gaseous fuel/air mixture into the combustor of a gas turbine. The premixing injector is designed to mix fuel and air at high velocities to eliminate the occurrence of flashback of the combustion flame from the reaction zone into the premixing injector. The premixing injector includes choked gas ports, which allow the fuel supply to be decoupled from any type of combustion instability which may arise in the combustor of the gas turbine and internal passages to provide regenerative cooling to the device.en
dc.format.mimetypeapplication/pdfen
dc.identifier.applicationnumber11757210en
dc.identifier.patentnumber7870736en
dc.identifier.urihttp://hdl.handle.net/10919/72657en
dc.identifier.urlhttp://pimg-fpiw.uspto.gov/fdd/36/707/078/0.pdfen
dc.language.isoen_USen
dc.publisherUnited States Patent and Trademark Officeen
dc.subject.cpcF23D14/08en
dc.subject.cpcF23D14/58en
dc.subject.cpcF23D14/64en
dc.subject.cpcF23D14/82en
dc.subject.cpcF23R3/286en
dc.subject.cpcF23C2900/9901en
dc.subject.cpcF23D2209/10en
dc.subject.cpcF23D2900/14021en
dc.subject.uspc239/533.2en
dc.subject.uspcother60/737en
dc.subject.uspcother60/740en
dc.titlePremixing injector for gas turbine enginesen
dc.typePatenten
dc.type.dcmitypeTexten
dc.type.patenttypeutilityen

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