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    • 8. 发明授权
    • Process and device for quickly reducing pressure in an installation, in
particular a hydrogen-cooled generator
    • 用于快速降低安装中的压力的​​工艺和装置,特别是氢冷发电机
    • US6086333A
    • 2000-07-11
    • US48
    • 1998-01-23
    • Joachim KrutzfeldtRudolf Von Musil
    • Joachim KrutzfeldtRudolf Von Musil
    • H02K9/08H02K9/24F04F5/48F04B23/08
    • H02K9/24
    • A method and device for quick pressure relief in a hydrogen-cooled generator system. The hydrogen-cooled generator system at least includes a first and second housing part and a hydrogen seal that separates the first housing part from the interior of the second housing part. In the normal state, the first housing part contains a hydrogen atmosphere at overpressure that is separated from the interior of the second housing part by the hydrogen seal. The quick pressure relief method includes the steps of lowering the pressure of the overpressure hydrogen in the first housing part through a quick discharge line upon failure of the hydrogen seal, and exhausting gas from the interior of the second housing part through a bleed line that is connected to the quick discharge line. The quick pressure relief device includes a quick discharge line for relieving pressure from the first housing part upon a failure of the hydrogen seal, and a bleed line fluidically connected to the quick discharge line and to the interior of the second housing part.
    • PCT No.PCT / DE96 / 01284第 371日期1998年1月23日 102(e)日期1998年1月23日PCT提交1996年7月15日PCT公布。 出版物WO97 / 05686 日期1997年2月13日在冷却发电机系统中快速释压的方法和装置。 氢冷却发电机系统至少包括第一和第二壳体部分和将第一壳体部分与第二壳体部分的内部分离的氢气密封件。 在正常状态下,第一壳体部分包含超压的氢气氛,其通过氢气密封与第二壳体部分的内部分离。 快速压力释放方法包括以下步骤:在氢气密封失效时通过快速排出管线降低第一壳体部分中的超压氢气的压力,并且通过排放管线从第二壳体部件的内部排出气体, 连接到快速放电线。 快速卸压装置包括用于在氢气密封故障时从第一壳体部分释放压力的快速排放管线和与流体连接到快速排放管线和第二壳体部分内部的排出管线。
    • 10. 发明授权
    • Drive disconnect for oil-cooled electrical generator
    • 油冷发电机驱动断开
    • US5418412A
    • 1995-05-23
    • US196702
    • 1994-02-15
    • Stephen F. Brucker
    • Stephen F. Brucker
    • H02K7/00H02K9/19H02K9/24H02K7/10H02K23/68
    • H02K9/24H02K7/003H02K9/19
    • An electric generator of the type that is oil-cooled and generally used in aircraft includes a fluid brake assembly. The fluid brake assembly includes a fluid brake rotor which is generally in the form of a fan or impeller which is connected to the drive shaft of the generator. Under normal conditions with the cooling oil withdrawn from the housing of the generator by the scavenge system, the fluid brake rotor freely turns with the shaft. When the oil scavenge system becomes incapacitated, the generator becomes "flooded" and the fluid brake rotor acts as pump to try to pump the oil, creating a torque load on the drive shaft. This load is preferably greater than the shear strength of the shaft, causing the shaft to shear and disconnecting the generator from the aircraft engine. By shearing the drive shaft, the operation of the main engine is unaffected by the flooding of the generator, and serious failure of the aircraft engine is avoided.
    • 通常用于飞机的油冷却型发电机包括流体制动组件。 流体制动组件包括流体制动转子,其通常为与发电机的驱动轴连接的风扇或叶轮的形式。 在正常条件下,通过清扫系统从发电机壳体中抽出的冷却油,流体制动转子与轴自由转动。 当油清除系统变得无法实现时,发电机变得“淹没”,并且流体制动转子作为泵来试图泵送油,从而在驱动轴上产生转矩负载。 该负载优选地大于轴的剪切强度,导致轴剪切并将发电机与飞机发动机断开连接。 通过剪切驱动轴,主发动机的操作不受发电机的溢流的影响,并且避免了飞机发动机的严重故障。