| 发明名称 |
NACELLE INLET WITH EXTENDED OUTER BARREL |
| 摘要 |
A nacelle inlet is provided for an aircraft propulsion system. This nacelle inlet includes an outer barrel, a bulkhead and a plurality of supports. The outer barrel extends around an axis and along the axis to an aft end. The bulkhead is within and connected to the outer barrel. An aft portion of the outer barrel projects axially aftward from the bulkhead to the aft end. The supports are disposed around the axis and next to the bulkhead. The supports are configured to support the aft portion of the outer barrel. |
| 申请公布号 |
US2016377090(A1) |
申请公布日期 |
2016.12.29 |
| 申请号 |
US201514713680 |
申请日期 |
2015.05.15 |
| 申请人 |
Rohr, Inc. |
发明人 |
Brown Keith T.;Fowler Frank J.;Byrne Stuart J.;Stein Adam |
| 分类号 |
F04D29/52;B64D33/02;B64D29/00 |
主分类号 |
F04D29/52 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A nacelle inlet for an aircraft propulsion system, the nacelle inlet comprising:
an outer barrel extending around an axis and along the axis to an aft end; a bulkhead within and connected to the outer barrel, wherein an aft portion of the outer barrel projects aftward axially from the bulkhead to the aft end; and a plurality of supports disposed around the axis and next to the bulkhead, the supports configured to support the aft portion of the outer barrel. |
| 地址 |
Chula Vista CA US |
