Systems and methods of aircraft thrust management are provided. For example, a propulsion system for an aircraft includes a fuel cell assembly including a fuel cell, a turbine, and a controller including a memory and one or more processors. The memory stores instructions that, when executed by the one or more processors, cause the propulsion system to operate, the operations including receiving data indicative of a propulsion system thrust difference and modifying an output of the fuel cell in response to receiving the data indicative of the propulsion system thrust difference. Modifying the fuel cell output may include modifying the output product, power output, or both of the fuel cell to balance thrust provided by the propulsion system.

    提供了飞行器推力管理的系统和方法。例如,用于飞行器的推进系统包括燃料电池组件,燃料电池组件包括燃料电池、涡轮机和控制器,控制器包括存储器和一个或多个处理器。存储器存储指令,该指令在由一个或多个处理器执行时使推进系统进行操作,操作包括接收指示推进系统推力差异的数据并响应于接收到指示推进系统推力差异的数据而修改燃料电池的输出。修改燃料电池输出可包括修改燃料电池的输出产物、电力输出或两者,以平衡由推进系统提供的推力。


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    Title :

    Aircraft thrust management with fuel cells


    Additional title:

    利用燃料电池的飞行器推力管理


    Contributors:

    Publication date :

    2023-07-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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