发明名称 |
WINDOW OF AN AIRCRAFT |
摘要 |
An aircraft includes a fuselage including a plurality of frame members disposed at predetermined intervals in a longitudinal direction of the fuselage and a plurality of stringers extending substantially linearly in the longitudinal direction. The fuselage defines an aircraft interior. A compartment is located in the interior of the fuselage. The compartment defines an interior area. A first one window assembly is mounted to an upper portion of the fuselage for introducing daylight into the interior area. The first window assembly is flanked by adjacent frame members of the plurality of frame members and adjacent stringers of the plurality of stringers. The first window assembly includes a window pane, an inner cover and a retainer. The inner cover introduces daylight from the window pane into the interior area. The retainer secures the window pane and the inner cover to the fuselage. |
申请公布号 |
EP2996938(A4) |
申请公布日期 |
2017.03.01 |
申请号 |
EP20140797229 |
申请日期 |
2014.05.14 |
申请人 |
Honda Patents & Technologies North America, LLC |
发明人 |
FUJINO, Michimasa;HOMMA, Yasuhiro |
分类号 |
B64C1/14;E06B5/12;E06B9/24 |
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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