Digital aviation power supply vehicle control device
The utility model discloses a digital aviation power supply vehicle control device, which comprises an engine, a power generator, a control panel, a control circuit, a rectifying module and multi-path AC/DC output power supplies, and is characterized in that the digital aviation power supply vehicle...
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| creator | WANG JINGDONG JIANG RENSHU ZHENG HAISHENG WANG SHENWEI |
| description | The utility model discloses a digital aviation power supply vehicle control device, which comprises an engine, a power generator, a control panel, a control circuit, a rectifying module and multi-path AC/DC output power supplies, and is characterized in that the digital aviation power supply vehicle control device is provided with a digital controller, wherein a CPU, a switching value input interface module, an analog sampling input interface module, a relay output interface module, a CAN bus communication interface module, an operating state storage module and a digital display module are arranged on a circuit board of the digital controller, each module is connected with the CPU, the switching value input interface module is connected with the control panel, the CAN bus communication interface module is connected with a CAN bus of the engine ECU, the analog sampling input interface module is connected with the control circuit, the control circuit is respectively connected with the engine, the power generator and the rectifying module, and the rectifying module is connected with the multi-path AC/DC output power supplies respectively. The digital aviation power supply vehicle control device has the advantages of accurate reading, fast operating speed, good visuality and the like. |
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The digital aviation power supply vehicle control device has the advantages of accurate reading, fast operating speed, good visuality and the like.</description><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL</subject><subject>CONTROLLING</subject><subject>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</subject><subject>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBxyUzPLEnMUUgsy0wsyczPUyjIL08tUiguLSjIqVQoS83ITM5JVUjOzyspys9RSEkty0xO5WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8c5-RgYmxsaGJoYmoaHGRCkCALZBLd8</recordid><startdate>20150513</startdate><enddate>20150513</enddate><creator>WANG JINGDONG</creator><creator>JIANG RENSHU</creator><creator>ZHENG HAISHENG</creator><creator>WANG SHENWEI</creator><scope>EVB</scope></search><sort><creationdate>20150513</creationdate><title>Digital aviation power supply vehicle control device</title><author>WANG JINGDONG ; JIANG RENSHU ; ZHENG HAISHENG ; WANG SHENWEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN204331414UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</creationdate><topic>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</topic><topic>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><toplevel>online_resources</toplevel><creatorcontrib>WANG JINGDONG</creatorcontrib><creatorcontrib>JIANG RENSHU</creatorcontrib><creatorcontrib>ZHENG HAISHENG</creatorcontrib><creatorcontrib>WANG SHENWEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WANG JINGDONG</au><au>JIANG RENSHU</au><au>ZHENG HAISHENG</au><au>WANG SHENWEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Digital aviation power supply vehicle control device</title><date>2015-05-13</date><risdate>2015</risdate><abstract>The utility model discloses a digital aviation power supply vehicle control device, which comprises an engine, a power generator, a control panel, a control circuit, a rectifying module and multi-path AC/DC output power supplies, and is characterized in that the digital aviation power supply vehicle control device is provided with a digital controller, wherein a CPU, a switching value input interface module, an analog sampling input interface module, a relay output interface module, a CAN bus communication interface module, an operating state storage module and a digital display module are arranged on a circuit board of the digital controller, each module is connected with the CPU, the switching value input interface module is connected with the control panel, the CAN bus communication interface module is connected with a CAN bus of the engine ECU, the analog sampling input interface module is connected with the control circuit, the control circuit is respectively connected with the engine, the power generator and the rectifying module, and the rectifying module is connected with the multi-path AC/DC output power supplies respectively. The digital aviation power supply vehicle control device has the advantages of accurate reading, fast operating speed, good visuality and the like.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING |
| title | Digital aviation power supply vehicle control device |
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