发明名称 |
Device and method for starting of a helicopter turbine, using an electrical energy source comprising supplementary discharging means |
摘要 |
The device has a starter (6) powered with electrical energy from an electricity network (8). Discharge members (10) i.e. supercapacitors, are incorporated in the electricity network and grouped into a module. The members of the module are grouped by a dozen, and have individual capacitance in the order of 3000 farads for a unit voltage of about 2.7 voltage direct current (Vdc). The members are connected in series to make the module suitable for use on a network having a voltage of about 28 Vdc. The members partially form an accessory that is removably mounted in the electricity network. An independent claim is also included for a method of starting a turbine engine of a helicopter. |
申请公布号 |
EP2264297(A1) |
申请公布日期 |
2010.12.22 |
申请号 |
EP20100005723 |
申请日期 |
2010.06.02 |
申请人 |
EUROCOPTER |
发明人 |
GAZZINO, MARC;LANCELEVEE, PIERRE-BERTRAND |
分类号 |
F02C7/26;F02C7/268;H02J7/34 |
主分类号 |
F02C7/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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