发明名称 TORQUE TUBE DOOR
摘要 PROBLEM TO BE SOLVED: To provide a method of closing an opening to accommodate flap motion during a cruise portion of flight.SOLUTION: A mounted door 52 covers an opening 50 in a fuselage 44. A torque tube 78 extends through the opening and into the interior of the fuselage 44. A lower edge portion 82 of the opening 50 includes a sealing member 54. The sealing member 54 may extend around only a perimeter of the opening 50. The seal 54 provides a resilient surface for mating with the door 52. For example, the seal 54 may include a hollow structure capable of elastic deformation. The seal 54 may include a retaining part for attaching the seal to the fuselage.SELECTED DRAWING: Figure 6
申请公布号 JP2016043921(A) 申请公布日期 2016.04.04
申请号 JP20150154704 申请日期 2015.08.05
申请人 BOEING CO 发明人 MARK BLEAZARD
分类号 B64C1/14;B64C13/30 主分类号 B64C1/14
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