THERMOELECTRIC GENERATOR ON AN AIRCRAFT BLEED SYSTEM
摘要
<p>A device for producing electrical power. A thermoelectric device is coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air.</p>
申请公布号
WO2011071602(A2)
申请公布日期
2011.06.16
申请号
WO2010US53622
申请日期
2010.10.21
申请人
THE BOEING COMPANY;GAO, LIJUN;SHENGYI, LIU;CHIEN, CHIN-HSI
