| 发明名称 |
NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT |
| 摘要 |
An aircraft may include at least one secondary power system requiring secondary power, at least two main engines, and at least three non-propulsive utility power (NPUP) generation systems. The NPUP generation systems may each be configured to provide full-time secondary power during operation of the aircraft. The NPUP generation systems may be configured to provide at least a portion of the secondary power required by the secondary power system. |
| 申请公布号 |
US2015151847(A1) |
申请公布日期 |
2015.06.04 |
| 申请号 |
US201314096106 |
申请日期 |
2013.12.04 |
| 申请人 |
The Boeing Company |
发明人 |
Krug David S.;Karimi Kamiar J.;Currier Thomas F.;Bayliss Andrew J.;Roe George M.;Liffring Mark E.;Lesyna Mark W.;Severns Christopher M.;Johnson Andrew |
| 分类号 |
B64D41/00;B64D15/04;B64D13/00;B60R16/03;H02J9/06 |
主分类号 |
B64D41/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft, comprising:
at least one secondary power system requiring secondary power; at least two main engines; and at least three non-propulsive utility power (NPUP) generation systems that are each configured to provide full-time secondary power during operation of the aircraft, wherein the at least three NPUP generation systems are configured to provide at least a portion of the secondary power required by the at least one secondary power system. |
| 地址 |
Chicago IL US |
