发明名称 Blowout latch
摘要 <p>A blowout latch (10) for releasably securing and aircraft panel (12) to an aircraft structure (18). The blowout latch (10) includes a housing (26), a bolt (28), and a handle (30). The housing includes a bias section (40) that has a plate (84), a block (86) adjacent the plate, a bias section (40) such as at least one coil spring (88) havingopposing ends (92, 94), a roller mount (96), and a roller pin (98). A trigger (32) is carried on the handle and is selectively engageable with the bolt to manually open the latch. The roller amount has a roller mount base. One end of the coil spring contacts the roller mount base. The opposing end of the coil spring contacts the block. The roller pin is rotably mounted to the roller mount. The bolt is rotatably mounted to the housing moveable between a latched and an unlatched position and is used to engage the aircraft structure. The bolt has a secured position. The bolt is held in its secured position by the coil spring which biases the roller pin against the bolt. The handle is rotably mounted to the bolt and is moveable between a latched position and an unlatched position, without the use of a tool. The handle provides an indicator when the blowout latch is in an open position. <IMAGE></p>
申请公布号 EP1197619(A1) 申请公布日期 2002.04.17
申请号 EP20010308636 申请日期 2001.10.10
申请人 HARTWELL CORPORATION 发明人 JACKSON, FRANK T.
分类号 B64D29/06;E05B15/04;E05B51/02;E05C3/08;(IPC1-7):E05B65/10;B64C1/14;E05C19/12 主分类号 B64D29/06
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