DEVICE AND A METHOD FOR FEEDING A ROCKET ENGINE PROPULSION CHAMBER
    1.
    发明申请
    DEVICE AND A METHOD FOR FEEDING A ROCKET ENGINE PROPULSION CHAMBER 审中-公开
    装置和一种用于喂送发动机推进室的方法

    公开(公告)号:US20140283499A1

    公开(公告)日:2014-09-25

    申请号:US13904584

    申请日:2013-05-29

    Applicant: SNECMA

    CPC classification number: F02K9/44 F02K9/46 F02K9/605

    Abstract: The invention relates to a device and a method for feeding a propulsion chamber 5 of a rocket engine 1 with at least with a first propellant. The device comprises at least a first tank 2 for containing said first propellant, a first feed circuit 4 connected to the first tank 2, and a first electric pump 10 within said first tank 2 in order to pump said first propellant through the first feed circuit 4. In the method, the first propellant is pumped through the first feed circuit 4 from the first tank 2 by at least said first electric pump 10 that is immersed in the first propellant within the first tank 2.

    Abstract translation: 本发明涉及一种用于至少与第一推进剂一起供给火箭发动机1的推进室5的装置和方法。 该装置至少包括用于容纳所述第一推进剂的第一罐2,连接到第一罐2的第一进料回路4和在所述第一罐2内的第一电泵10,以便通过第一进料回路泵送第一推进剂 在该方法中,第一推进剂通过至少浸入第一罐2中的第一推进剂的第一电动泵10从第一罐2泵送通过第一进料回路4。

    DEVICE AND A METHOD FOR FEEDING A ROCKET ENGINE PROPULSION CHAMBER
    2.
    发明申请
    DEVICE AND A METHOD FOR FEEDING A ROCKET ENGINE PROPULSION CHAMBER 审中-公开
    装置和一种用于喂送发动机推进室的方法

    公开(公告)号:US20160237951A1

    公开(公告)日:2016-08-18

    申请号:US15141431

    申请日:2016-04-28

    Applicant: SNECMA

    Abstract: The invention relates to a device and a method for feeding a propulsion chamber of a rocket engine with at least with a first propellant. The device comprises at least a first tank for containing the first propellant, a first feed circuit connected to the first tank, and a first electric pump within the first tank in order to pump the first propellant through the first feed circuit. In the method, the first propellant is pumped through the first feed circuit from the first tank by at least the first electric pump that is immersed in the first propellant within the first tank.

    Abstract translation: 本发明涉及一种用于至少与第一推进剂一起供给火箭发动机的推进室的装置和方法。 该装置至少包括用于容纳第一推进剂的第一罐,连接到第一罐的第一进料回路和第一罐内的第一电泵,以便通过第一进料回路泵送第一推进剂。 在该方法中,第一推进剂通过至少浸没在第一罐内的第一推进剂中的第一电动泵从第一罐泵送通过第一进料回路。

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