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.
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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 |
代理机构 |
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