发明名称 PRESSURE SENSOR AND ROCKET ENGINE INCORPORATING SAME
摘要 .The invention concerns a pressure sensor (2) comprising a pressure detecting element (21) designed to receive a pressure to be measured and to detect same, and a printed circuit (22) connected to the pressure detecting element (21) for electrical connection. The invention is characterised in that the electric connection comprises at least a flexible conductive blade (29) whereof one first end (290) is connected, directly or indirectly, to the printed circuit (22) and a second end (291) is simply supported on a corresponding contact (213) of the pressure detecting element (21). In order to ensure proper electric contact, the support surface (294) of the second end of the or each flexible conductive blade (29) on the corresponding electric contact (213a) is smooth.
申请公布号 WO02061384(A1) 申请公布日期 2002.08.08
申请号 WO2002FR00340 申请日期 2002.01.29
申请人 SNECMA PROPULSION SOLIDE;AVISSE, JEAN-BERNARD 发明人 AVISSE, JEAN-BERNARD
分类号 G01L9/04;F02K9/60;F02K9/96;G01L9/00;G01L19/00 主分类号 G01L9/04
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