发明名称 |
Structural housing of a turbomachine |
摘要 |
<p>The casing has a central hub, an intermediate shroud and an external ring concentric about an axial direction. The ring and the shroud are connected via links, and the shroud and the central hub are connected by a series of radially fastened hollow arms. The series of arms comprises a main arm (110) and a secondary arm, where each main arm is arranged in the continuation of a link. Each main arm has a mass greater than that of the secondary arm arranged at a distance from the links, and has a narrowed wall thickness over full height of the main arm. An independent claim is also included for a turbine engine comprising a structural casing.</p> |
申请公布号 |
EP1770246(A2) |
申请公布日期 |
2007.04.04 |
申请号 |
EP20060076712 |
申请日期 |
2006.09.12 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" |
发明人 |
GIRARD, NICOLAS;CAMERIANO, LAURENT |
分类号 |
F01D25/24;F01D5/14;F01D9/04;F01D9/06;F01D25/16 |
主分类号 |
F01D25/24 |
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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