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1.发明授权公开(公告)号：US08757542B2
公开(公告)日：2014-06-24
申请号：US13176846
申请日：2011-07-06
IPC分类号： B64D35/00
CPC分类号： B64D27/24 , B60L3/0046 , B60L3/0061 , B60L11/005 , B60L11/123 , B60L11/14 , B60L11/1853 , B60L2210/20 , B60L2240/36 , B60L2250/10 , B64C27/04 , B64C27/14 , B64D2027/026 , Y02T10/6217 , Y02T10/7005 , Y02T10/7022 , Y02T10/705 , Y02T10/7077 , Y02T10/725 , Y02T50/44 , Y02T50/64
摘要： A hybrid power plant (5) for an aircraft (1) comprises at least: a hybrid drive system (37) having a main on-board electricity network (16) and an auxiliary electricity network (34); and a selective adaptation interface (38) arranged to enable electrical energy to be exchanged selectively between the main and auxiliary electricity networks (16; 34). At least one engine and a hybrid drive auxiliary electrical machine (7, 31) are mechanically connected to a transmission (8); said machine (7) being electrically connected to at least one auxiliary electrical bus (36) in parallel with at least one auxiliary device for delivering electric charge.
摘要翻译： 一种用于飞机（1）的混合动力装置（5）至少包括：具有主车载电力网络（16）和辅助电力网络（34）的混合动力驱动系统（37）。 以及布置成使得能够在主电力网络和辅助电力网络（16; 34）之间有选择地交换电能的选择性适配接口（38）。 至少一个发动机和混合驱动辅助电机（7,31）机械连接到变速器（8）; 所述机器（7）与至少一个用于传送电荷的辅助装置并联地与至少一个辅助电气总线（36）电连接。
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2.发明申请公开(公告)号：US20120025032A1
公开(公告)日：2012-02-02
申请号：US13176846
申请日：2011-07-06
CPC分类号： B64D27/24 , B60L3/0046 , B60L3/0061 , B60L11/005 , B60L11/123 , B60L11/14 , B60L11/1853 , B60L2210/20 , B60L2240/36 , B60L2250/10 , B64C27/04 , B64C27/14 , B64D2027/026 , Y02T10/6217 , Y02T10/7005 , Y02T10/7022 , Y02T10/705 , Y02T10/7077 , Y02T10/725 , Y02T50/44 , Y02T50/64
摘要： A hybrid power plant (5) for an aircraft (1) comprises at least: a hybrid drive system (37) having a main on-board electricity network (16) and an auxiliary electricity network (34); and a selective adaptation interface (38) arranged to enable electrical energy to be exchanged selectively between the main and auxiliary electricity networks (16; 34). At least one engine and a hybrid drive auxiliary electrical machine (7, 31) are mechanically connected to a transmission (8); said machine (7) being electrically connected to at least one auxiliary electrical bus (36) in parallel with at least one auxiliary device for delivering electric charge.
摘要翻译： 一种用于飞机（1）的混合动力装置（5）至少包括：具有主车载电力网络（16）和辅助电力网络（34）的混合动力驱动系统（37）。 以及布置成使得能够在主电力网络和辅助电力网络（16; 34）之间有选择地交换电能的选择性适配接口（38）。 至少一个发动机和混合驱动辅助电机（7,31）机械连接到变速器（8）; 所述机器（7）与至少一个用于传送电荷的辅助装置并联地与至少一个辅助电气总线（36）电连接。
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