发明名称 CONTENITORE PER LIQUIDI, IN PARTICOLARE SERBATOIO PER OLIO, CON MEZZI PER LO SFIATAMENTO DEL CONTENITORE, TENENDO CONTO DI POSIZIONI E CONDIZIONI DI VOLO ESTREMI
摘要 <p>A liquid reservoir, such as an oil tank, for use in missiles or aircraft which are subjected to extreme flight attitudes. The reservoir has a wall rotationally symmetrical about the longitudinal axis of the reservoir, and the liquid content of the reservoir is rotated about the longitudinal axis to provide, by centrifugal force, a central space within the reservoir which is essentially free of liquid. Air is vented from the reservoir through a fixed vent located within the central space created when the liquid content is rotated.</p>
申请公布号 IT1142120(B) 申请公布日期 1986.10.08
申请号 IT19810025657 申请日期 1981.12.17
申请人 MTU MOTOREN UND TURBINEN UNION MUENCHEN GMBH 发明人 SCHWEIKL LUDWIG;KRAUSS OLAF
分类号 B64D37/02;B64D37/06;B64D37/22;F01D25/18;F16N39/00;(IPC1-7):F16K/ 主分类号 B64D37/02
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