发明名称 Pressure regulator at end of aircraft fuelling pipe - comprises control cut=off and venturi-nozzle
摘要 The control cut-off (2) and venturi-nozzle (3) of predetermined venturi length are incorporated in the tank filling pipe. The one is connected to the other via a control conduit (4) which issues in the region of the narrowest restriction in the nozzle. The venturi-nozzle is made of an elastic material which permits continuous deformation, and its profile, at least in the region of the narrowest cross-section, is alterable using an adjustment device (6). This device comprises flange rings rotatable counter to each other, and with a seal between them, the one ring being connected to the filling pipe, and the other with the venturi-nozzle. USE - To regulate the pressure at the end of a fuel tank filling pipe for aircraft.
申请公布号 DE4011059(A1) 申请公布日期 1991.10.10
申请号 DE19904011059 申请日期 1990.04.05
申请人 DR.-ING. ULRICH ESTERER GMBH & CO. FAHRZEUGBAUTEN UND ANLAGEN KG, 3506 HELSA, DE 发明人 ESTERER, HAROLD, DIPL.-KAUFM., 3500 KASSEL, DE
分类号 B67D7/36 主分类号 B67D7/36
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