发明名称 Fluid ejecting device e.g. hydraulic oil extinguisher, for aircraft, has pressurization chamber provided with sock sealingly separating interior of pressurization chamber from side walls of tank
摘要 <p>The device has a piston (5) sliding in a tank along a longitudinal axis of the tank to modify a relative volume of a pressurization chamber (A) and a chamber (B). The chamber (B) is filled with fluid and has an ejection orifice closed by a distribution cap (16) so that the fluid is ejected from the tank via the orifice under translation effect of the element and opening effect of the cap. A gas generator (7) modifies pressure in the chamber (A) to provoke translation of the piston. The chamber (A) has a sock (50) sealingly separating interior of the chamber (A) from the walls.</p>
申请公布号 FR2936715(A1) 申请公布日期 2010.04.09
申请号 FR20080005467 申请日期 2008.10.03
申请人 AIRBUS FRANCE 发明人 FABRE CHRISTIAN;BIGNOLAIS ALAIN
分类号 A62C13/66;A62C3/08;B05B15/00 主分类号 A62C13/66
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