| 发明名称 |
FUEL TRANSFER SYSTEM FOR AIRCRAFT |
| 摘要 |
<p>Fuel Transfer System for Aircraft Parallel transfer pump (92,94) operate to transfer fuel from auxiliary tanks (52,60,66) to the main tank (10). A pressure sensor (106) in the pump discharge line in combination with tank level rate means (86,88,90) sequences pumps (92,92) and transfer valves (100,102) if required, and confirms successful transfer or alarms when unsuccessful.</p> |
| 申请公布号 |
CA1324367(C) |
申请公布日期 |
1993.11.16 |
| 申请号 |
CA19890613143 |
申请日期 |
1989.09.26 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SECCHIAROLI, LAWRENCE N.;CRESISKI, RAYMOND C., JR.;WILSON, THOMAS P. |
| 分类号 |
F02C7/22;B64C17/10;B64D37/00;B64D37/02;(IPC1-7):B64D37/00 |
主分类号 |
F02C7/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
