The invention discloses a hydrogen storage tank thermostat based on hydrogen kinetic energy engine. The hydrogen storage tank thermostat comprises a composite wing drone body, a heat transfer mechanism is arranged at the lower end of the composite wing drone body, a cold air cooling mechanism is arranged on one side of the heat transfer mechanism, and a linkage transmission mechanism is arranged on one side of the cold air cooling mechanism. The hydrogen storage tank thermostat has the beneficial effects that the hydrogen tank can be properly heated by using the heat generated by the hydrogenfuel engine, the hydrogen tank can be properly cooled by using the refrigeration effect generated by gasification of liquid hydrogen, and the heating mechanism and the cooling mechanism share one setof pipeline so that the mass of the drone can be reduced to the maximum extent; and the frosting phenomenon can be avoided through the mutual influence of the heating mechanism and the cooling mechanism, so that the hydrogen storage tank can be kept in a certain temperature interval, and the stability of the hydrogen tank is greatly improved.

    本发明公开了一种基于氢动能发动机的储氢罐恒温装置,包括复合翼无人机本体,所述复合翼无人机本体下端设有热量转移机构,所述热量转移机构一侧设有冷气降温机构,所述冷气降温机构一侧设有联动传动机构。本发明的有益效果是,可以利用氢燃料发动机自身产生的热量适当的对氢气罐加温,利用液态氢的气化产生的制冷效果可以适当的对氢气罐降温,升温机构和降温机构共用一套管路,可以最大化的降低无人机质量,通过升温机构和降温机构互相影响的作用可以避免结霜的现象发生,使储氢罐可以保持在一定温度区间内,大幅提高氢气罐的稳定性。


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    Titel :

    Hydrogen storage tank thermostat based on hydrogen kinetic energy engine


    Weitere Titelangaben:

    一种基于氢动能发动机的储氢罐恒温装置


    Beteiligte:
    LI JIE (Autor:in)

    Erscheinungsdatum :

    20.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F02M Zuführen von Brennstoff-Luft-Gemischen oder deren Bestandteilen bei Brennkraftmaschinen allgemein , SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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