| 摘要 |
An aircraft spherical bearing assembly (100, 200) comprises a first part (102, 202) which is in sliding contact with an intermediate part (104, 106, 204, 206) for sliding therebetween to form a spherical joint. A second slip path is provided between the intermediate component (104, 106, 204, 206) and an outer component (110, 112, 208) which can be selectively actuated when the force through the first slip path exceeds a predetermined level.
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