公开(公告)号：US09995247B2

公开(公告)日：2018-06-12

申请号：US14875897

申请日：2015-10-06

Applicant: SPIRIT AEROSYSTEMS, INC.

Inventor： Rahbar Nasserrafi ,  Craig Clasper ,  Micheal A. Walker ,  Gerald E. Hicks ,  Linda Cadwell Stancin

IPC: B32B15/00 ,  C25D7/00 ,  F02K1/82 ,  C25D3/04 ,  C25D3/12 ,  C25D3/38 ,  C25D3/54 ,  C25D3/56 ,  C25D3/58 ,  C23C26/00 ,  F02K1/72

CPC classification number: F02K1/822 ,  B32B15/00 ,  B32B2305/024 ,  C23C4/073 ,  C23C4/11 ,  C23C4/129 ,  C23C4/131 ,  C23C24/04 ,  C23C26/00 ,  C23C28/321 ,  C23C28/3455 ,  C25D3/04 ,  C25D3/12 ,  C25D3/38 ,  C25D3/54 ,  C25D3/56 ,  C25D3/562 ,  C25D3/58 ,  C25D7/00 ,  F02K1/72 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2300/172 ,  F05D2300/177 ,  F05D2300/5024 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/675

Abstract: An aircraft thrust reverser inner wall and method of manufacturing the same. The aircraft thrust reverser inner wall may include a face sheet, a perforated back sheet, and a core sandwiched between the face sheet and the perforated back sheet. The face sheet may have an inner face sheet surface and an outer face sheet surface, and the core may have an inner core surface, an outer core surface, and a plurality of cell walls extending therebetween. An electro-depositable material may be applied, via electrodeposition, in a substantially continuous layer over the outer core surface, the cell walls, and the outer face sheet surface, thus bonding the face sheet and core together. The perforated back sheet may be attached to the core at the outer core surface, and a conductive coating may be applied to the inner face sheet surface.