发明名称 |
Aircraft cabin window assembly method |
摘要 |
A method for assembling a cabin window to a bay in a side wall of an aircraft fuselage, where the cabin window including an outer transparent element and at least one inner transparent element, includes making a non-through hole in a portion of the side wall. The outer transparent element includes a first part having a diameter greater than that of the bay and which is shaped to co-operate with the portion of the side wall to block the outer transparent element in the bay both laterally and longitudinally. A second part of the outer transparent element has a groove that projects into the fuselage. The outer transparent element and the at least one inner transparent element are welded to the fuselage using a strap which presses a seal against at least the fuselage and the inner wall of the groove.
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申请公布号 |
US8371531(B2) |
申请公布日期 |
2013.02.12 |
申请号 |
US20080521819 |
申请日期 |
2008.01.03 |
申请人 |
AIRBUS OPERATIONS SAS;GALLANT GUILLAUME;AGUERA DAMIEN;BERNADET PHILIPPE |
发明人 |
GALLANT GUILLAUME;AGUERA DAMIEN;BERNADET PHILIPPE |
分类号 |
B64C1/14 |
主分类号 |
B64C1/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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