| 摘要 |
PROBLEM TO BE SOLVED: To provide a propelling assembly more durable to oil leakage over an entire starter. SOLUTION: The present invention refers to a gas turbine engine which comprises a gear housing AGB 12 mechanically connected with an engine shaft for driving auxiliary machines and the air starter 10, 10' mounted on the housing, wherein the starter and housing enclosures are in communication such that lubrication oil of the starter is distributed from the AGB housing. The engine is characterized in that an oil enclosure of the starter 10, 10' is pressurized by an air source independently from the AGB housing. Advantageously, the compressed air is taken from a compression enclosure of an engine bearing. COPYRIGHT: (C)2008,JPO&INPIT
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