发明名称 |
PROPELLER FOR AN AIRCRAFT TURBINE ENGINE INCLUDING A BLADE-RETAINING RING MOUNTED AROUND A HUB |
摘要 |
A propeller for an aircraft turbine engine comprising a plurality of vanes as well as a hub having a plurality of accommodating ports receiving the bases of said vanes, each vane base being rotatably mounted in its associated accommodating port. The propeller also has at least one vane retaining ring structure in the radial direction outwardly from the hub, being cladded around the latter. |
申请公布号 |
EP2417024(A1) |
申请公布日期 |
2012.02.15 |
申请号 |
EP20100725361 |
申请日期 |
2010.04.06 |
申请人 |
AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE) |
发明人 |
LAFONT, LAURENT;PRAT, DAMIEN;DIOCHON, LIONEL |
分类号 |
B64C11/06;F01D21/04;F04D29/32 |
主分类号 |
B64C11/06 |
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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