发明名称 |
Stopper rotation braking device for e.g. jet engine, has braking unit that cooperates by elastic fixing with cylindrical teeth of boss of casing of turbomachine, where unit is integrated in rotation with stopper by shape cooperation unit |
摘要 |
<p>The device has a braking unit (28) that is carried by a stopper (10) and cooperates by elastic fixing with cylindrical teeth (30) of a boss (16) of a casing (18) of a turbomachine. The unit (28) is integrated in rotation with the stopper by using a shape cooperation unit. The unit (28) comprises tongues curved in circular arc around an axis (24) and applied on a bottom of an annular edge (22). The tongues are connected with each other by a flat transversal median part which extends along the bottom of an outer annular groove (32) of the stopper. An independent claim is also included for a turbomachine such as jet engine and turbo-prop of aircraft, comprising a device for braking rotation of two elements screwed with each other.</p> |
申请公布号 |
FR2888900(A1) |
申请公布日期 |
2007.01.26 |
申请号 |
FR20050007748 |
申请日期 |
2005.07.21 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION SNECMA SOCIETE ANONYME |
发明人 |
BROMANN ALAIN;DEBENEIX PIERRE |
分类号 |
F16B39/32;F02C7/00;F16B41/00 |
主分类号 |
F16B39/32 |
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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