发明名称 |
Method to assemble a turbomachine |
摘要 |
<p>The method involves mating a low pressure (LP) turbine module (110) of a gas turbine engine with a low pressure shaft (101) up to a determined distance from a journal (111) integrated to a high pressure (HP) body of the engine. The shaft is centered with respect to the journal, where the centering is controlled based on the measuring distance deviations with respect to a reference on the journal. An outer ring of the journal is expanded by heating the outer surface of the journal, and the mating of the shaft is completed. An independent claim is also included for a device for the implementation of a gas turbine engine assembling method.</p> |
申请公布号 |
EP1757777(A1) |
申请公布日期 |
2007.02.28 |
申请号 |
EP20060119569 |
申请日期 |
2006.08.25 |
申请人 |
SNECMA |
发明人 |
BERGEROT, FRANCOIS;LEEDER, LAURENT;MALTERRE, JACQUES;SOUART, BERNARD;THOMAS, HUBERT |
分类号 |
F01D25/28;F02C7/20 |
主分类号 |
F01D25/28 |
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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