发明名称 |
System and method for forming perforations in a barrel section |
摘要 |
A drilling system may include a plurality of robotic drilling units. Each one of the robotic drilling units may include a drill end effector positioned inside a barrel section. The barrel section may be configured as a composite sandwich structure having an inner face sheet. The robotic drilling units maybe operable in synchronized movement with one another to drill a plurality of perforations into the inner face sheet using the drill end effectors in a manner providing a predetermined percent-open-area of the inner face sheet. |
申请公布号 |
US9370827(B2) |
申请公布日期 |
2016.06.21 |
申请号 |
US201314012243 |
申请日期 |
2013.08.28 |
申请人 |
The Boeing Company |
发明人 |
Zubin Claudio;Gibbings Geoffrey;Shewfelt Mathew J.;Simonovic Damjan;Ferreira Antonio M.;Boonstra David;Lauder Arnold J.;Gabriel Mark F. |
分类号 |
B23B39/14;B23B39/24;B23B39/20 |
主分类号 |
B23B39/14 |
代理机构 |
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代理人 |
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主权项 |
1. A method of fabricating an engine inlet, comprising the steps of:
providing an engine inlet inner barrel section configured as a composite sandwich structure having an inner face sheet; robotically drilling, using a plurality of synchronized robotic drilling units, a plurality of perforations in the inner face sheet after final cure of the composite sandwich structure, wherein the drilling comprises indexing a hole pattern of the perforations to one or more cell walls of a honeycomb core of the composite sandwich structure, and positioning the hole pattern such that each perforation is located at a spaced distance from the cell walls; and forming the plurality of perforations in a quantity providing a predetermined percent-open-area of the inner face sheet. |
地址 |
Chicago IL US |