发明名称 |
Mission adaptive inlet |
摘要 |
A mission adaptive inlet (42) for an aircraft (40) has a rigid lip panel (56) pivotally attached to an inlet (42) of the aircraft (40). An actuation mechanism is coupled to the rigid lip panel (56) and causes the rigid lip panel (56) to pivot from a first position to a second position. A reinforced elastomer system (48) is connected the rigid lip panel and the inlet (42).
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申请公布号 |
US6089505(A) |
申请公布日期 |
2000.07.18 |
申请号 |
US19970898162 |
申请日期 |
1997.07.22 |
申请人 |
MCDONNELL DOUGLAS CORPORATION |
发明人 |
GRUENSFELDER, CYNTHIA ANN;WILLE, ROBERT HENRY |
分类号 |
B64D33/02;F02C7/042;(IPC1-7):B64B1/24;B64C1/38;B64D15/00;F02B27/00 |
主分类号 |
B64D33/02 |
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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