AIRCRAFT ELECTRICAL ENERGY SUPPLY NETWORK
The invention concerns an electrical energy supply network (1) of an aircraft equipped with a plurality of electrical loads (C1, C2) to be supplied, the supply network (1) comprising at least two generators (2, 3) of a turbogenerator of the aircraft, each suitable for providing an electrical energy...
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Main Authors | , , |
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Format | Patent |
Language | Chinese English |
Published |
21.12.2021
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Subjects | |
Online Access | Get full text |
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Summary: | The invention concerns an electrical energy supply network (1) of an aircraft equipped with a plurality of electrical loads (C1, C2) to be supplied, the supply network (1) comprising at least two generators (2, 3) of a turbogenerator of the aircraft, each suitable for providing an electrical energy source, at least one stator associated with a rectifier (20a, 20b, 20c; 30a, 30b, 30c), characterised in that the stators of the generators (2, 3) are mounted in parallel on at least two distribution buses (4, 5) designed to supply the plurality of electrical loads (C1, C2), and in that it comprises contactors (100) suitable for electrically connecting or disconnecting the distribution buses (4, 5) from each other.
本发明涉及一种用于飞行器的电能供应网络(1),该电能供应网络具有多个待供电的电负载(C1,C2),所述电能供应网络(1)包括飞行器的涡轮发电机的至少两个发电机(2,3),每个发电机适于提供电能源,至少一个定子与整流器(20a,20b,20c;30a、30b、30c)关联,其特征在于,发电机(2,3)的定子并联安装在至少两条配电总线(4,5)上,所述配电总线被设计为向多个电负载(C1,C2)供电,并且在于,所述电能供应网络包括将配电总线(4,5)彼此电连接或断开的接触器(100)。 |
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Bibliography: | Application Number: CN202080035701 |