发明名称 |
DOOR ANTI-HIJACKING LATCH/LOCK MECHANISM WITH PNEUMATIC DECOMPRESSION OVERRIDE |
摘要 |
<p>An aircraft door having an electrically operated latching device (601) engaged only when electrical power is applied. Latch logic permits release by actuation of a switch (603) on the pilot's panel, by loss electrical power (602) , by a knob on the control cabin side (605) OR by a key from outside the control cabin (604). The aircraft door controlled by the electrically operated latching device (601) further includes a decompression override mechanism (606).</p> |
申请公布号 |
WO8401404(A1) |
申请公布日期 |
1984.04.12 |
申请号 |
WO1982US01387 |
申请日期 |
1982.09.30 |
申请人 |
THE BOEING COMPANY |
发明人 |
CHURCH, ROYCE, FRANKLIN;MCCAFFREY, DONALD, BRIAN;PLUDE, LEO, WALTER |
分类号 |
B64C1/14;B64D45/00;E05B47/00;E05B51/02;(IPC1-7):05C1/06;64C1/14 |
主分类号 |
B64C1/14 |
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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