Connection system for aircraft propeller blade |
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| 申请号 | JP12709490 | 申请日 | 1990-05-18 | 公开(公告)号 | JPH0354096A | 公开(公告)日 | 1991-03-08 |
| 申请人 |
General Electric Co |
发明人 | SHIFUARATSUTO SESU FUSAIN; JIERARUDO POORU KUROGAA; ROBAATO POORU KUZACHIYOAA; | ||||
| 摘要 | PURPOSE: To improve connectability between a propeller blade support ring and a turbine surrounded by the ring, by connecting each bracket between the ring for supporting a propeller blade and the turbine surrounded by the ring with a turbine at a single point and with the ring at a pair of points. CONSTITUTION: In a simple form, two links 95, 96 are constituted to be fastened with a common anchor point 103 on a casing 24, and the links 95, 96 are fastened with a ring 22 at anchor points 107, 108. When the casing 24 expands, the point 103 moves radially outwards in the arrow 102 direction. Therefore, because links 95, 96 do not bend as a traditional bracket foot part bends, a triangle formed by the points 103, 107, 108 retains its sizes and shape. | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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