发明名称 |
Retention assembly for a propeller blade |
摘要 |
<p>A retention assembly (32) for a propeller blade (30) includes an inner ring (40) that is conformally shaped to a bore (41) of an annular loop (38), the annular loop (38) being associated with a root portion (36) of the propeller blade (30); a base (44) that is configured to be immediately adjacent the annular loop (38); an outer ring (42) that includes an extended tapered portion (72) which decreases in radial thickness from an inboard end (74) to an outboard end (76); and an adhesive that adhesively connects complementary surfaces of the outer ring (42) and the annular loop (38). Also, a propeller blade assembly (22) includes a propeller blade (30) having a blade portion (34) and a root portion (36) and the retention assembly (32) configured to be attached to the propeller blade (30).</p> |
申请公布号 |
EP2862799(A1) |
申请公布日期 |
2015.04.22 |
申请号 |
EP20140188983 |
申请日期 |
2014.10.15 |
申请人 |
HAMILTON SUNDSTRAND CORPORATION |
发明人 |
NAGLE, DAVID P.;CARVALHO, PAUL A. |
分类号 |
B64C11/26;B64C11/06;F01D5/30 |
主分类号 |
B64C11/26 |
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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