| 发明名称 |
DUAL VALVE GAS PRESSURE EQUALIZATION SYSTEM AND METHOD |
| 摘要 |
An aircraft gas transport system including a high pressure gas supply line having a supply valve, and an equilibrium gas line joined at junctions with the high pressure gas supply line upstream and downstream from the supply valve, and in flow communication with the high pressure gas supply line, the equilibrium gas line having an equilibrium valve and a flow restrictor, the equilibrium valve having an exit orifice and the flow restrictor being offset from the exit orifice of the equilibrium valve. |
| 申请公布号 |
US2016368609(A1) |
申请公布日期 |
2016.12.22 |
| 申请号 |
US201514743112 |
申请日期 |
2015.06.18 |
| 申请人 |
The Boeing Company |
发明人 |
Schmidt Kevin |
| 分类号 |
B64D13/02;F17D1/20;F15D1/06;F17D1/02 |
主分类号 |
B64D13/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft gas transport system comprising:
a high pressure gas supply line having a supply valve; and an equilibrium gas line joined at junctions with the high pressure gas supply line upstream and downstream from the supply valve, and in flow communication with the high pressure gas supply line, the equilibrium gas line having an equilibrium valve and a flow restrictor, the equilibrium valve having an exit orifice and the flow restrictor being offset from the exit orifice of the equilibrium valve. |
| 地址 |
Chicago IL US |
