公开(公告)号：WO2014182616A2

公开(公告)日：2014-11-13

申请号：PCT/US2014036791

申请日：2014-05-05

Applicant: SIKORSKY AIRCRAFT CORP

Inventor： SIMONETTI JOSEPH LAWRENCE ,  BYSTRY MARK DENTON ,  DEVITA MICHAEL JOSEPH ,  TARASCIO MATTHEW J ,  STRAUSS MICHAEL PETER ,  REEVE HAYDEN M ,  DESAI NIRANJAN ,  ST ROCK BRIAN ,  LENTS CHARLES E ,  ZEIDNER LAWRENCE E ,  SMILEY ALFRED RUSSELL

IPC: F02C9/48

CPC classification number: B64D31/12 ,  B64D27/02 ,  B64D41/00 ,  B64D2027/026 ,  B64D2221/00 ,  B64F5/00 ,  Y02T50/44 ,  Y02T50/64 ,  Y02T90/44

Abstract: Embodiments are directed to selecting, by a computing device comprising a processor, the size of at least one prime mover associated with an aircraft to satisfy a baseline power requirement for operation of the aircraft during a steady state load condition, selecting at least one power source configuration to supplement power provided by the at least one prime mover during a transient load condition associated with the operation of the aircraft, and selecting, by the computing device, a parameter of the at least one power source configuration to provide a total power in an amount that is greater than a threshold during the transient condition.

Abstract translation: 实施例涉及通过包括处理器的计算设备选择与飞行器相关联的至少一个原动机的尺寸，以满足在稳定状态负载条件期间飞行器的操作的基准功率需求，选择至少一个电源 配置以在与飞行器的操作相关联的瞬态负载条件期间补充由至少一个原动机提供的功率，以及由计算设备选择所述至少一个电源配置的参数以提供总功率 在瞬态条件下大于阈值的量。