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    • 1. 发明授权
    • Gas turbine, particularly an aircraft engine
    • 燃气轮机,特别是飞机发动机
    • US07495354B2
    • 2009-02-24
    • US10582917
    • 2004-11-20
    • Hubert Herrmann
    • Hubert Herrmann
    • F02K11/00
    • F02C7/268F01D15/10F02C3/113F05D2220/50
    • A gas turbine, particularly an aircraft engine includes at least one compressor. The gas turbine comprises at least one stator, at least one rotor and at least one generator (19) for generating electrical energy. An engine rotor has a rotor shaft (11) and rotor disks (12, 13, 14), which are driven by the rotor shaft (11) and which have rotating rotor blades (15). A stator has a housing (17) and fixed guide vanes (18). A generator (19) has at least one stator (21) and at least one rotor (20). The electrical energy generated by the generator (19) preferably serves to operate at least one attachment or one auxiliary unit of the gas turbine. According to the invention, the generator (19) is integrated in the interior of the gas turbine in such a manner that each rotor (20) of the generator is allocated to the compressor rotor and the stator (21) of the generator is allocated to the compressor stator, whereby kinetic energy of the rotor is convertible into electrical energy by the generator (19).
    • 燃气轮机,特别是飞机发动机包括至少一个压缩机。 燃气轮机包括至少一个定子,至少一个转子和用于产生电能的至少一个发电机(19)。 发动机转子具有转子轴(11)和由转子轴(11)驱动并具有旋转的转子叶片(15)的转子盘(12,13,14)。 定子具有壳体(17)和固定导叶(18)。 发电机(19)具有至少一个定子(21)和至少一个转子(20)。 由发电机(19)产生的电能优选用于操作燃气轮机的至少一个附件或一个辅助单元。 根据本发明,发电机(19)以这样的方式集成在燃气涡轮机的内部,使得发电机的每个转子(20)被分配给压缩机转子,并且发电机的定子(21)被分配给 压缩机定子,由此由发电机(19)将转子的动能转换成电能。
    • 3. 发明申请
    • Gas turbine, particularly an aircraft engine
    • 燃气轮机,特别是飞机发动机
    • US20070152534A1
    • 2007-07-05
    • US10582917
    • 2004-11-20
    • Hubert Herrmann
    • Hubert Herrmann
    • F01D15/10H02K17/42
    • F02C7/268F01D15/10F02C3/113F05D2220/50
    • The invention relates to a gas turbine, particularly an aircraft engine. The gas turbine comprises at least one stator, at least one rotor and at least one generator (19) for generating electrical energy. A rotor has a rotor shaft (11) and rotor disks (12, 13, 14), which are driven by the rotor shaft (11) and which have rotating rotor blades (15). A stator has a housing (17) and fixed guide vanes (18). A generator (19) has at least one stator (21) and at least one rotor (20). The electrical energy generated by the generator (19) preferably serves to operate at least one attachment device or one auxiliary unit of the gas turbine. According to the invention, the generator (19) is integrated in the interior of the gas turbine in such a manner that the or each rotor (20) of the generator is allocated to the rotor and the or each stator (21) of the generator is allocated to the stator, whereby kinetic energy of the rotor is convertible into electrical energy by the generator (19).
    • 本发明涉及一种燃气轮机,特别是飞机发动机。 燃气轮机包括至少一个定子,至少一个转子和用于产生电能的至少一个发电机(19)。 转子具有转子轴(11)和由转子轴(11)驱动并具有旋转的转子叶片(15)的转子盘(12,13,14)。 定子具有壳体(17)和固定导叶(18)。 发电机(19)具有至少一个定子(21)和至少一个转子(20)。 由发电机(19)产生的电能优选地用于操作燃气轮机的至少一个附接装置或一个辅助装置。 根据本发明,发电机(19)以这样的方式集成在燃气轮机的内部,使得发电机的每个转子(20)被分配给发电机和发电机的每个定子(21) 被分配给定子,由此通过发电机(19)将转子的动能转化为电能。