| 发明名称 |
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM SELECTIVELY POWERED BY THREE BLEED REPORTS |
| 摘要 |
An engine compressor bleed system of an engine for an aircraft is provided including a plurality of compressor pressure ports configured to supply bleed air to satisfy a cooling load for at least a first stage of a flight profile of an aircraft. A first pressure port of the plurality of compressor pressure ports is configured to provide bleed air having a pressure at least equal to a cabin pressure of an aircraft and a temperature that does not exceed a predetermined threshold. |
| 申请公布号 |
US2015307183(A1) |
申请公布日期 |
2015.10.29 |
| 申请号 |
US201514755929 |
申请日期 |
2015.06.30 |
| 申请人 |
Hamilton Sundstrand Corporation |
发明人 |
Bruno Louis J.;Zywiak Thomas M. |
| 分类号 |
B64C21/06;B64D13/08 |
主分类号 |
B64C21/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An engine compressor bleed system of an engine for an aircraft is provided, comprising:
a plurality of compressor pressure ports configured to supply bleed air to satisfy a cooling load for at least a first stage of a flight profile of an aircraft, wherein a first pressure port of the plurality of compressor pressure ports is configured to provide bleed air having a pressure at least equal to a cabin pressure of an aircraft and a temperature that does not exceed a predetermined threshold. |
| 地址 |
Windsor Locks CT US |
