| 发明名称 |
INNER COWL STRUCTURE FOR AIRCRAFT TURBINE ENGINE |
| 摘要 |
An inner cowl structure for circumscribing at least a portion of a jet engine extending from an aircraft includes an apron configured to mount directly to the engine independent of the pylon and overly an upper portion of the jet engine, and an inner body configured to circumscribe a portion of the jet engine not circumscribed by the apron. |
| 申请公布号 |
US2014319269(A1) |
申请公布日期 |
2014.10.30 |
| 申请号 |
US201313862941 |
申请日期 |
2013.04.15 |
| 申请人 |
MRA Systems, Inc. |
发明人 |
Scarr Antony Brett;Weir Thomas Joseph;Woolley Allen Madsen;Janzon Carol Marie |
| 分类号 |
F04D29/40;B64D29/02;B64D29/06 |
主分类号 |
F04D29/40 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An inner cowl structure for circumscribing at least a portion of a jet engine having at least one engine mount coupled to an engine pylon extending from an aircraft wing, the inner cowl structure comprising:
an apron configured to mount directly to the engine independent of the pylon and overly an upper portion of the jet engine; and an inner body configured to circumscribe a portion of the jet engine not circumscribed by the apron; wherein the inner cowl body is coupled to the apron such that the resulting combination of the coupled apron and inner cowl body defines a hoop structure that is structurally independent of the pylon and completely circumscribes at least a portion of the jet engine. |
| 地址 |
US |
