Hybrid control system across multiple operating modes
A lever for adjusting an output of a hybrid power device of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts an output of the hybrid power device between at least two modes of operation. In a first subset of positions within the overal...
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| creator | CURRIER PAUL SANTA CRUZ XAVIER GEORGE ANDERSON RICHARD PAUL WILSON GREGG SPITZER, DAVID, N |
| description | A lever for adjusting an output of a hybrid power device of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts an output of the hybrid power device between at least two modes of operation. In a first subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, output first electrical energy from a motor/generator driven by the mechanical output of the engine, and drive a propulsion mechanism by the mechanical output of the engine. In a second subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, receive second electrical energy at the motor/generator, drive the mechanical output through the motor/generator using the second electrical energy, and drive the propulsion mechanism through the mechanical output.
用于调节飞行器的混电动力装置的输出的杆包括配置为在整体位置范围内移动的杆。杆的移动在至少两种操作模式之间调节混电动力装置的输出。在整体位 |
| format | Patent |
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用于调节飞行器的混电动力装置的输出的杆包括配置为在整体位置范围内移动的杆。杆的移动在至少两种操作模式之间调节混电动力装置的输出。在整体位</description><language>chi ; eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2024</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=20240920&DB=EPODOC&CC=CN&NR=118679098A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240920&DB=EPODOC&CC=CN&NR=118679098A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CURRIER PAUL</creatorcontrib><creatorcontrib>SANTA CRUZ XAVIER GEORGE</creatorcontrib><creatorcontrib>ANDERSON RICHARD PAUL</creatorcontrib><creatorcontrib>WILSON GREGG</creatorcontrib><creatorcontrib>SPITZER, DAVID, N</creatorcontrib><title>Hybrid control system across multiple operating modes</title><description>A lever for adjusting an output of a hybrid power device of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts an output of the hybrid power device between at least two modes of operation. In a first subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, output first electrical energy from a motor/generator driven by the mechanical output of the engine, and drive a propulsion mechanism by the mechanical output of the engine. In a second subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, receive second electrical energy at the motor/generator, drive the mechanical output through the motor/generator using the second electrical energy, and drive the propulsion mechanism through the mechanical output.
用于调节飞行器的混电动力装置的输出的杆包括配置为在整体位置范围内移动的杆。杆的移动在至少两种操作模式之间调节混电动力装置的输出。在整体位</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDD1qEwqykxRSM7PKynKz1EoriwuSc1VSEwuyi8uVsgtzSnJLMhJVcgvSC1KLMnMS1fIzU9JLeZhYE1LzClO5YXS3AyKbq4hzh66qQX58anFBYnJqXmpJfHOfoaGFmbmlgaWFo7GxKgBAKsvLd4</recordid><startdate>20240920</startdate><enddate>20240920</enddate><creator>CURRIER PAUL</creator><creator>SANTA CRUZ XAVIER GEORGE</creator><creator>ANDERSON RICHARD PAUL</creator><creator>WILSON GREGG</creator><creator>SPITZER, DAVID, N</creator><scope>EVB</scope></search><sort><creationdate>20240920</creationdate><title>Hybrid control system across multiple operating modes</title><author>CURRIER PAUL ; SANTA CRUZ XAVIER GEORGE ; ANDERSON RICHARD PAUL ; WILSON GREGG ; SPITZER, DAVID, N</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN118679098A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2024</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>CURRIER PAUL</creatorcontrib><creatorcontrib>SANTA CRUZ XAVIER GEORGE</creatorcontrib><creatorcontrib>ANDERSON RICHARD PAUL</creatorcontrib><creatorcontrib>WILSON GREGG</creatorcontrib><creatorcontrib>SPITZER, DAVID, N</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CURRIER PAUL</au><au>SANTA CRUZ XAVIER GEORGE</au><au>ANDERSON RICHARD PAUL</au><au>WILSON GREGG</au><au>SPITZER, DAVID, N</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Hybrid control system across multiple operating modes</title><date>2024-09-20</date><risdate>2024</risdate><abstract>A lever for adjusting an output of a hybrid power device of an aircraft includes a lever configured to move over an overall range of positions. Movement of the lever adjusts an output of the hybrid power device between at least two modes of operation. In a first subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, output first electrical energy from a motor/generator driven by the mechanical output of the engine, and drive a propulsion mechanism by the mechanical output of the engine. In a second subset of positions within the overall range of positions, the hybrid power device is configured to operate an engine having a mechanical output, receive second electrical energy at the motor/generator, drive the mechanical output through the motor/generator using the second electrical energy, and drive the propulsion mechanism through the mechanical output.
用于调节飞行器的混电动力装置的输出的杆包括配置为在整体位置范围内移动的杆。杆的移动在至少两种操作模式之间调节混电动力装置的输出。在整体位</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Hybrid control system across multiple operating modes |
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