A propulsion system includes a fuel cell assembly having a fuel cell defining an outlet positioned to remove an output product from the fuel cell and fuel cell assembly operating conditions; a turbine including a compressor section, a combustion section, and a turbine section arranged in a serial flow sequence, the combustion section configured to receive an aviation fuel flow from the aircraft fuel supply, and further configured to receive an output product from the fuel cell; and a controller comprising a memory and one or more processors, the memory storing instructions that, when executed by the one or more processors, cause the propulsion system to perform operations comprising: receiving data indicative of an in-flight flameout within the combustion section; modifying fuel cell assembly operating conditions in response to receiving data indicative of in-flight flameout within the combustion section; and initiating a reignition of the combustion section.
一种推进系统,包括:燃料电池组件,燃料电池组件具有燃料电池,燃料电池限定定位成从燃料电池中移除输出产物的出口和燃料电池组件操作条件;涡轮机,涡轮机包括以串行流动顺序布置的压缩机区段、燃烧区段和涡轮区段,燃烧区段被构造为接收来自飞行器燃料供应部的航空燃料流,并且进一步被构造为接收来自燃料电池的输出产物;以及控制器,控制器包括存储器和一个或多个处理器,存储器存储指令,指令在由一个或多个处理器执行时,使推进系统进行包括以下的操作:接收指示燃烧区段内的飞行中熄火的数据;响应于接收到指示燃烧区段内的飞行中熄火的数据,修改燃料电池组件操作条件;以及发起燃烧区段的重新点燃。
REIGNITION OF PROPULSION SYSTEM WITH FUEL CELL
具有燃料电池的推进系统的重新点燃
2023-05-05
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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