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公开(公告)号：US20160201553A1
公开(公告)日：2016-07-14
申请号：US15076829
申请日：2016-03-22
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Anthony C. Jones , Victor Pascu
CPC classification number: F02B37/10 , F02B33/40 , F02B39/04 , F02B39/06 , F02B39/08 , F02B53/14 , F02B63/04 , F02M35/10157 , F02M35/10268 , Y02T10/144
Abstract: A supercharge compound configuration of a forced induction intake and/or breather system for an internal combustion engine is provided. The system may be configured to improve the power output of an internal combustion engine when considered against similar internal combustion engines with conventional forced induction systems. The supercharge compound configuration may comprise a turbine that may be driven by the exhaust of the internal combustion engine. The turbine may also be operatively and/or directly coupled to a gearbox and/or a compressor.
Abstract translation: 提供了一种用于内燃机的强制进气和/或通气系统的增压复合结构。 该系统可以被配置为当考虑到具有常规强制诱导系统的类似内燃机时，提高内燃机的功率输出。 增压复合构造可以包括可由内燃机的排气驱动的涡轮机。 涡轮机还可以可操作地和/或直接地联接到齿轮箱和/或压缩机。
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公开(公告)号：US08662445B2
公开(公告)日：2014-03-04
申请号：US13953164
申请日：2013-07-29
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Anthony C. Jones , Todd A. Spierling , Gregory L. DeFrancesco
CPC classification number: B64D41/00 , B64C13/40 , B64C13/42 , B64D2221/00
Abstract: A hybrid power distribution system for an aircraft generates hydraulic power from one of a plurality of power sources based on which power source provides energy most efficiently. Power sources includes an electric power distribution bus that distributes electrical energy onboard the aircraft, a pneumatic distribution channel that distributes pneumatic energy onboard the aircraft, and mechanical power provided by one or more engines associated with the aircraft.
Abstract translation: 用于飞机的混合动力配电系统基于哪个电源最有效地提供能量从多个电源之一产生液压动力。 电源包括分配飞机上的电能的电力分配总线，在飞机上分配气动能量的气动分配通道以及由与飞机相关联的一个或多个发动机提供的机械动力。
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公开(公告)号：US20130306790A1
公开(公告)日：2013-11-21
申请号：US13953164
申请日：2013-07-29
Applicant: Hamilton Sundstrand Corporation
Inventor： Louis J. Bruno , Anthony C. Jones , Todd A. Spierling , Gregory L. DeFrancesco
IPC: B64D41/00
CPC classification number: B64D41/00 , B64C13/40 , B64C13/42 , B64D2221/00
Abstract: A hybrid power distribution system for an aircraft generates hydraulic power from one of a plurality of power sources based on which power source provides energy most efficiently. Power sources includes an electric power distribution bus that distributes electrical energy onboard the aircraft, a pneumatic distribution channel that distributes pneumatic energy onboard the aircraft, and mechanical power provided by one or more engines associated with the aircraft.
Abstract translation: 用于飞机的混合动力配电系统基于哪个电源最有效地提供能量从多个电源之一产生液压动力。 电源包括分配飞机上的电能的电力分配总线，在飞机上分配气动能量的气动分配通道以及由与飞机相关联的一个或多个发动机提供的机械动力。
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