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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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