发明名称 Cover for aircraft engines
摘要 <p>The tarpaulin (1) has a cap-shaped section provided with a circumferential edge (11) that lies on a lining (21) of a jet engine and passes over holes in the lining. Pass-through apertures associated with the holes are provided in the edge. A trapezoidal-shaped flap (14) is formed in a region of each aperture, where one side of the flap is firmly connected with the edge. The aperture is arranged centrally in the flap. A storage pocket (15) for ball lock pins (13) is provided on the edge adjacent to each aperture.</p>
申请公布号 EP2615035(A2) 申请公布日期 2013.07.17
申请号 EP20120199167 申请日期 2012.12.21
申请人 RINCK, KLAUS 发明人 RINCK, KLAUS
分类号 B64F1/00 主分类号 B64F1/00
代理机构 代理人
主权项
地址