发明名称 |
AIR INPUT DEVICE FOR A TURBOPROP ENGINE |
摘要 |
An air intake layout for a turboprop. A nacelle surrounding an intake section of the turboprop behind the fan propeller can be moved away from the main part of the nacelle and can be divided into two parts that may be extracted so as to leave full access to the panel leading to equipment in a central compartment, whereas the panel was partially covered by the air intake leading edge. |
申请公布号 |
EP1626900(A1) |
申请公布日期 |
2006.02.22 |
申请号 |
EP20030740678 |
申请日期 |
2003.04.28 |
申请人 |
SNECMA |
发明人 |
CHAUMERET, MICHEL;MAZEAUD, GEORGES |
分类号 |
B64D29/00 |
主分类号 |
B64D29/00 |
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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