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发明公开
EP2559882A1 Ignition system for a gas turbine combustor 审中-公开
Zündungssystemfüreine Gasturbinen-Brennkammer

Ignition system for a gas turbine combustor
摘要：
A combustor ignition system (40) includes an igniter assembly (42) adapted for installation at least partially inside a combustor (10). A first ignition lead (46) is electrically connected to the igniter assembly (42) and includes a terminal end (62) remote from the igniter assembly (42). A second ignition lead (48) is electrically connected to the first ignition lead (46). The combustor ignition system (40) further includes means for releasably connecting the first and second ignition leads (46, 48).
摘要（中）：

燃烧器点火系统（40）包括适于至少部分地安装在燃烧器（10）内部的点火器组件（42）。 第一点火引线（46）电连接到点火器组件（42）并且包括远离点火器组件（42）的终端（62）。 第二点火引线（48）电连接到第一点火引线（46）。 燃烧器点火系统（40）还包括用于可释放地连接第一和第二点火线（46,48）的装置。

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