发明名称 Rotating joint for gas turbine rotor of helicopter, has ribs of one of parts overlapped with sleeves of other part to form large volume decompression zone, where plates have gas injection nozzle that is opened in space defined by zones
摘要 <p>The joint (6) has a movable plate (8) movable with respect to a fixed plate (7) around a rotational axis (A). Each plate has an interface zone (30) with projected and retraction elements i.e. coaxial annular ribs (29), presenting complementary shapes. The ribs of one of the plates are overlapped with another elements i.e. adapter sleeves (26) of other plate to form a large volume decompression zone. The zones are located remote from one other without friction. The plates have a pressurized gas injection nozzle (32) that is opened in a baffle or labyrinth shaped space defined by the zones.</p>
申请公布号 FR2913479(A1) 申请公布日期 2008.09.12
申请号 FR20070001653 申请日期 2007.03.07
申请人 DE CHAMPEAUX PHILIPPE 发明人 DE CHAMPEAUX PHILIPPE
分类号 F16L27/08;B64C27/12;F02C1/02;F16J15/44 主分类号 F16L27/08
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