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1. 发明申请

US20130158750A1 Energy Management On Board an Aircraft 有权
标题翻译：飞机上的能源管理
公开(公告)号：US20130158750A1
公开(公告)日：2013-06-20
申请号：US13721636
申请日：2012-12-20
申请人： THALES , LIEBHERR AEROSPACE TOULOUSE SAS
发明人： Joël BOSSON , Vincent GOMEZ
IPC分类号： B64C19/00
CPC分类号： B64C19/00 , H02J3/14 , H02J4/00
摘要： Energy management on board an aircraft includes: a plurality of thermal and electrical energy sources, a plurality of loads which are capable of being supplied with power by the various energy sources, among which at least one load is capable of being supplied with power by an electrical energy source and by a thermal energy source, and real-time management means for energy transfers from the various energy sources to the various loads as a function of the present and future energy requirement of the various loads and the present and future availability of the various sources, with the management means providing a permanent and standardized correlation between thermal and electrical energies.
摘要翻译：飞机上的能量管理包括：多个热能和电能源，能够被各种能量源供电的多个负载，其中至少一个负载能够通过电能源和热能源，以及用于从各种能源到各种负载的能量转移的实时管理手段，作为各种负载的当前和未来能量需求的函数以及当前和将来可用性各种来源，管理手段提供热能和电能之间永久和标准化的相关性。

2. 发明申请

US20170355466A1 AIR CONDITIONING SYSTEM FOR A "MORE ELECTRIC" AIRPLANE 审中-公开
公开(公告)号：US20170355466A1
公开(公告)日：2017-12-14
申请号：US15507099
申请日：2015-09-04
申请人： LIEBHERR-AEROSPACE TOULOUSE SAS
发明人： Guillaume GALZIN , Vincent GOMEZ
IPC分类号： B64D13/08 , B64D13/06
CPC分类号： B64D13/08 , B64D13/06 , B64D2013/0618 , B64D2013/0644 , B64D2013/0688 , Y02T50/44 , Y02T50/54 , Y02T50/56
摘要： An aircraft air conditioning system, powered solely using electrical energy, to draw bleed air from outside the aircraft and deliver conditioned air to the aircraft's interior, includes at most three motorized rotary machines, which include: independent first and second motorized turbocompressors, each turbocompressor includes a turbine compressor and an electric motor; and a motor compressor interconnected between the turbocompressors via an interconnection pipe. The motor compressor: generates a primary air flow, which drives a secondary air flow, allowing a breathing air flow to be cooled in a first operation phase, corresponding to a ground operation or at relatively low altitude and relatively low aircraft speed; be at shutdown or at low idle in a second phase of operation at relatively low altitude and relatively high aircraft speed; and, provide a top up breathing air flow in a third phase of operation at relatively high altitude and relatively high aircraft speed.

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