发明名称 |
MONOLITHIC THRUST REVERSER COMPONENTS |
摘要 |
<p>An aircraft engine nacelle (10) includes a pivot-door type thrust reverser. The thrust reverser (22) includes a monolithic fan duct barrel (24) with an annular wall (50) that includes a forward section (46), a door section (54), and an aft section (48). The wall (50) has a honeycomb-sandwich type structure with an interiorface sheet (60) and a backing sheet (62) radially separated by a first cellular core (66). An outer sheet (64) associated with the aft section (48) of the wall (50) is radially separated from the backing sheet (62) by a second cellular core (68). A plurality of pivoting doors (26,28) mate with a plurality of door openings (56,58) in the door section (54) of the annular wall (50). Each door (26,28) has honeycomb-sandwich type structure similar to that of the annular wall (50), wherein each door (26,28) has an interior face sheet (74) separated from a backing sheet (76) by a first cellular core (80), and an outer sheet (78) separated from the backing sheet (76) by a second cellular core (82).</p> |
申请公布号 |
WO2008111992(A2) |
申请公布日期 |
2008.09.18 |
申请号 |
WO2007US73355 |
申请日期 |
2007.07.12 |
申请人 |
SPRITT AEROSYSTEMS, INC.;STERNBERGER, JOE, E.;SAWYER, CHRISTOPHER |
发明人 |
STERNBERGER, JOE, E.;SAWYER, CHRISTOPHER |
分类号 |
B64D27/16 |
主分类号 |
B64D27/16 |
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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