An aircraft (199, 400, 3127, 385, 450), comprising: a fuselage (102, 402, 263, 3140, 386); a wing (404); an engine (106, 406, 2601) connected to the wing (404); a set of liquid hydrogen tanks (108, 408, 2260, 381, 431); a discharge port (2860, 4304) located on the tail wing (410, 386) on the fuselage (102, 402, 263, 3140, 386); a conduit system (3801) connecting the liquid hydrogen tank (108, 408, 2260, 381, 431) to the discharge port (2860, 4304); and a controller. The controller is configured to control the conduit system (3801) to release gaseous hydrogen (3811) in the set of liquid hydrogen tanks (108, 408, 2260, 3881, 431) to travel through the conduit system (3801) and exit at the exhaust port (2860, 4304) in response to a pressure in the set of liquid hydrogen tanks (108, 408, 2260, 3881, 431) being greater than a particular tolerance.
一种飞机(199,400,3127,3855,4502),包括:机身(102,402,2630,3140,3862);机翼(404);发动机(106,406,2601),连接到机翼(404);一组液氢罐(108,408,2602,3810,4310);排出口(2860,4304),位于在机身(102,402,2630,3140,3862)上的尾翼(410,3861)上;导管系统(3801),将液氢罐(108,408,2602,3810,4310)连接至排出口(2860,4304);以及控制器。控制器配置为响应于一组液氢罐(108,408,2602,3810,4310)中的压力大于特定公差,控制导管系统(3801)释放一组液氢罐(108,408,2602,3810,4310)中的气态氢(3811)以行进通过导管系统(3801)并且在排出口(2860,4304)处离开。
Aircraft, hydrogen recirculation system and method for recirculating hydrogen
飞机、氢再循环系统及用于再循环氢的方法
2025-02-21
Patent
Electronic Resource
Chinese
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