Electric-based secondary power system architectures for aircraft
Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thr...
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creator | Atkey, Warren A Bernier, Alan T Bowman, Michael D Campbell, Thomas A Cruse, Jonathan M Fiterman, Charles J Meis, Charles S Ng, Casey Y. K Nozari, Farhad Zielinski, Edward |
description | Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine. |
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K ; Nozari, Farhad ; Zielinski, Edward</creator><creatorcontrib>Atkey, Warren A ; Bernier, Alan T ; Bowman, Michael D ; Campbell, Thomas A ; Cruse, Jonathan M ; Fiterman, Charles J ; Meis, Charles S ; Ng, Casey Y. K ; Nozari, Farhad ; Zielinski, Edward ; The Boeing Company</creatorcontrib><description>Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.</description><language>eng</language><creationdate>2007</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/7207521$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,776,798,881,64012</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7207521$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Atkey, Warren A</creatorcontrib><creatorcontrib>Bernier, Alan T</creatorcontrib><creatorcontrib>Bowman, Michael D</creatorcontrib><creatorcontrib>Campbell, Thomas A</creatorcontrib><creatorcontrib>Cruse, Jonathan M</creatorcontrib><creatorcontrib>Fiterman, Charles J</creatorcontrib><creatorcontrib>Meis, Charles S</creatorcontrib><creatorcontrib>Ng, Casey Y. 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K</creator><creator>Nozari, Farhad</creator><creator>Zielinski, Edward</creator><scope>EFH</scope></search><sort><creationdate>20070424</creationdate><title>Electric-based secondary power system architectures for aircraft</title><author>Atkey, Warren A ; Bernier, Alan T ; Bowman, Michael D ; Campbell, Thomas A ; Cruse, Jonathan M ; Fiterman, Charles J ; Meis, Charles S ; Ng, Casey Y. K ; Nozari, Farhad ; Zielinski, Edward</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_072075213</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2007</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Atkey, Warren A</creatorcontrib><creatorcontrib>Bernier, Alan T</creatorcontrib><creatorcontrib>Bowman, Michael D</creatorcontrib><creatorcontrib>Campbell, Thomas A</creatorcontrib><creatorcontrib>Cruse, Jonathan M</creatorcontrib><creatorcontrib>Fiterman, Charles J</creatorcontrib><creatorcontrib>Meis, Charles S</creatorcontrib><creatorcontrib>Ng, Casey Y. K</creatorcontrib><creatorcontrib>Nozari, Farhad</creatorcontrib><creatorcontrib>Zielinski, Edward</creatorcontrib><creatorcontrib>The Boeing Company</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Atkey, Warren A</au><au>Bernier, Alan T</au><au>Bowman, Michael D</au><au>Campbell, Thomas A</au><au>Cruse, Jonathan M</au><au>Fiterman, Charles J</au><au>Meis, Charles S</au><au>Ng, Casey Y. K</au><au>Nozari, Farhad</au><au>Zielinski, Edward</au><aucorp>The Boeing Company</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Electric-based secondary power system architectures for aircraft</title><date>2007-04-24</date><risdate>2007</risdate><abstract>Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet engine. The jet engine can be configured to provide propulsive thrust to the aircraft, and the electric generator can be configured to receive shaft power from the jet engine. The environmental control system can be configured to provide outside air to a passenger cabin of the aircraft in the absence of bleed air from the jet engine.</abstract><oa>free_for_read</oa></addata></record> |
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title | Electric-based secondary power system architectures for aircraft |
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