| 发明名称 |
Disassembling turbomachinery compressors |
| 摘要 |
A turbomachine compressor comprising a rotor 43 including a removable end part 45, in the form of a unitary bladed disc, can be withdrawn and replaced in one unit. High and low pressure shaft assemblies (54 and ) 46 are formed by separable parts to enable these operations to be performed without having to dismantle the entire machine. <IMAGE>
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| 申请公布号 |
GB2283535(A) |
申请公布日期 |
1995.05.10 |
| 申请号 |
GB19940022067 |
申请日期 |
1994.11.02 |
| 申请人 |
* SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION S N E C M A |
发明人 |
JACKY SERGE * NAUDET |
| 分类号 |
F01D5/06;F01D25/28;F04D29/32;(IPC1-7):F04D29/60;F04D29/04 |
主分类号 |
F01D5/06 |
| 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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