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    TANK HAVING AN INCLINED PARTITION PROVIDED AT ITS ENDS WITH THROUGH-HOLES FOR CONTINUOUS SUPPLY OF A SUPPLY LIQUID TO A TURBINE ENGINE
    1.
    发明申请
    TANK HAVING AN INCLINED PARTITION PROVIDED AT ITS ENDS WITH THROUGH-HOLES FOR CONTINUOUS SUPPLY OF A SUPPLY LIQUID TO A TURBINE ENGINE 有权
    具有连续供应液体向涡轮发动机连续通孔的包含分段的油箱

    公开(公告)号：US20150060206A1

    公开(公告)日：2015-03-05

    申请号：US14472929

    申请日：2014-08-29

    申请人： SNECMA

    发明人： Antoine LAIGLE ,  Gilles Le Gouellec ,  Bellal Waissi

    IPC分类号： F01D25/20 ,  F01D25/18

    CPC分类号： F01D25/20 ,  F01D25/18 ,  F01M2011/0095 ,  F16N17/06

    摘要： The tank for a turbine engine comprises a partition separating a first compartment from a second compartment of the tank , the partition having a first end and a second end, the second end being closer to the bottom of the tank than the first end, the partition being inclined from the first end to the second end in the first direction and in the direction of the first outlet to the second outlet , the partition comprising at least one first Through-hole near the first end and at least one second through-hole closer to the second end than the first hole.

    摘要翻译： 用于涡轮发动机的罐包括将第一隔室与罐的第二隔室分开的隔板，隔板具有第一端和第二端，第二端比第一端更靠近罐的底部，隔板 在第一方向和第一出口的方向上从第一端向第二端倾斜到第二出口，所述隔板包括靠近第一端的至少一个第一通孔和至少一个第二通孔密封件 到第二个端头比第一个孔。

    METHOD FOR ISOLATING A COMBUSTIBLE FLUID TANK FROM A DOWNSTREAM PORTION OF A TURBOMACHINE SUPPLY SYSTEM IN CASE OF A FIRE, AND SUCH A SUPPLY SYSTEM
    2.
    发明申请
    METHOD FOR ISOLATING A COMBUSTIBLE FLUID TANK FROM A DOWNSTREAM PORTION OF A TURBOMACHINE SUPPLY SYSTEM IN CASE OF A FIRE, AND SUCH A SUPPLY SYSTEM 审中-公开
    用于从火灾案例中的涡轮机供应系统的下游部分分离可燃液体罐的方法和这样的供应系统

    公开(公告)号：US20170022906A1

    公开(公告)日：2017-01-26

    申请号：US15302571

    申请日：2015-04-07

    申请人： SNECMA

    发明人： Thomas LEPAGE ,  Antoine LAIGLE ,  Matthieu ATTALLI

    IPC分类号： F02C9/46 ,  B64D37/32 ,  F02C7/232

    CPC分类号： F02C9/46 ,  B64D37/32 ,  F01D25/20 ,  F02C7/232 ,  F05D2220/323 ,  F05D2240/35 ,  F05D2270/09 ,  Y02T50/671

    摘要： A supply system for supplying fluid to a turbomachine including a fluid tank, a downstream portion located downstream from the tank, and a cutoff valve located between the tank and the downstream portion. The cutoff valve is configured to be at least partially open when a rotational speed of a shaft of the turbomachine is higher than a first threshold and in the absence of a fire detected in the turbomachine. The cutoff valve is closed when the two following conditions are satisfied: the rotational speed of the shaft is higher than the first threshold, and the rotational speed of the shaft was lower than the first threshold when a fire was detected in the turbomachine during the flight.

    摘要翻译： 用于向包括流体箱的涡轮机供给流体的供应系统，位于罐的下游的下游部分以及位于罐和下游部分之间的截流阀。 当涡轮机的轴的旋转速度高于第一阈值并且在涡轮机中没有检测到火焰时，截止阀被构造成至少部分打开。 当满足以下两个条件时，截止阀关闭：在飞行中在涡轮机中检测到火灾时，轴的转速高于第一阈值，并且轴的转速低于第一阈值 。