发明名称 Anchoring lock for aircraft seat feet
摘要 The heavy monobloc lock (1) for anchoring an aircraft seat foot in a sectioned slide fixed to the floor comprises a longitudinal web plate (8). Transversely on a longitudinal edge, the web plate has longitudinal spaced pairs of oppositely positioned runners (13). These runners project laterally and their faces (14) constitute support surfaces which engage in the slide. A first transversely projecting part (16) of the web plate is fixed rigidly to the foot. A second part enables rigid but removable fixing to a locking flange (5). A third part in the shape of a swivel pin, with a transverse axis, takes a longitudinal locking plunger (6). The first projecting part is in the middle of the web plate between the second part which is to the rear and the third part at the front.
申请公布号 FR2735443(A1) 申请公布日期 1996.12.20
申请号 FR19950007085 申请日期 1995.06.14
申请人 SOCIETE INDUSTRIELLE ET COMMERCIALE DE MATERIEL AERONAUTIQUE 发明人 BEDOUCH PIERRE FRANCOIS
分类号 B64D11/06;(IPC1-7):B64D11/06 主分类号 B64D11/06
代理机构 代理人
主权项
地址