发明名称 Pressure-difference warning system used for e.g. aircraft door, has acoustic signal device adapted to output acoustic signal if measured pressure difference exceeds specifiable threshold value
摘要 A pressure sensor (4) is adapted to measure pressure difference between the primary and secondary spatial regions. An energy supply device (14) is adapted to provide energy to operate a pressure difference warning system (2). An acoustic signal device (12) is adapted to output an acoustic signal if measured pressure difference exceeds specifiable threshold value. Independent claims are also included for the following: (A) a door with a pressure-difference warning system; (B) an aircraft with a pressure-difference warning system; (C) a method of generating an acoustic signal as a pressure-difference warning signal; (D) a computer-readable storage medium; and (E) a program element for generating an acoustic signal as a pressure-difference warning signal.
申请公布号 DE102005002544(A1) 申请公布日期 2006.07.27
申请号 DE20051002544 申请日期 2005.01.19
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 HELLWIG, ROBERT
分类号 G08B21/18;B64D45/00 主分类号 G08B21/18
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