发明名称 |
Closed loop control system for controlling an air discharge out of an aircraft body |
摘要 |
The flow volume of used air to be discharged from an aircraft cabin is controlled in a valve control system in which each outflow valve has at least two slave controllers responsive to any one of at least two master controllers in a closed loop control system. For this purpose the slave controllers and the master controllers are interconnected by an intermeshed conductor network including a plurality of conductor sections interconnected by electrical conductor junctions or optical conductor couplers forming interfaces between the conductor sections to provide a redundant number of communication paths to keep the system operable even if failures or faults occur.
|
申请公布号 |
US5934614(A) |
申请公布日期 |
1999.08.10 |
申请号 |
US19970891519 |
申请日期 |
1997.07.11 |
申请人 |
DAIMLERCHRYSLER AEROSPACE AIRBUS GMBH |
发明人 |
MUELLER, WOLFGANG;KLEIN, BERND |
分类号 |
B64D13/04;(IPC1-7):B64D13/04 |
主分类号 |
B64D13/04 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|