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公开(公告)号：EP2296970A2
公开(公告)日：2011-03-23
申请号：EP09766033.6
申请日：2009-05-14
申请人： Snecma
IPC分类号： B64D27/24
CPC分类号： B64D27/24 , B64C2201/042 , B64D2027/026 , B64D2041/005 , B64D2211/00 , Y02T50/64 , Y02T90/36 , Y02T90/44
摘要： The invention relates to an aircraft powered by hybrid power that comprises: an outer structure (12 to 20); electric equipment (34); internal combustion propulsion means (40); and a means for supplying power to the propulsion means; characterised in that the aircraft further comprises: a plurality of converters for directly converting light energy into electric power (24), arranged on at least a portion of the outer surface of the outer structure; a means (32) for comparing the electric power generated by said converters with the instantaneous consumption of said electric equipment (34); a means (36) for recovering excess electric power if there is any; and a means (38) for supplying said propulsion means (40) with additional power from said excess electric power if there is any.
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公开(公告)号：EP2296970B1
公开(公告)日：2012-02-01
申请号：EP09766033.6
申请日：2009-05-14
申请人： Snecma
IPC分类号： B64D27/24
CPC分类号： B64D27/24 , B64C2201/042 , B64D2027/026 , B64D2041/005 , B64D2211/00 , Y02T50/64 , Y02T90/36 , Y02T90/44
摘要： The invention relates to an aircraft powered by hybrid power that comprises: an outer structure (12 to 20); electric equipment (34); internal combustion propulsion means (40); and a means for supplying power to the propulsion means; characterised in that the aircraft further comprises: a plurality of converters for directly converting light energy into electric power (24), arranged on at least a portion of the outer surface of the outer structure; a means (32) for comparing the electric power generated by said converters with the instantaneous consumption of said electric equipment (34); a means (36) for recovering excess electric power if there is any; and a means (38) for supplying said propulsion means (40) with additional power from said excess electric power if there is any.
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