发明名称 |
Noise reducing connection assembly for aircraft turbine housings |
摘要 |
In an aircraft turbine, an assembly consisting of an air inlet structure, a air blower housing (22) and a connecting part (36), is fitted in such a way as to reduce noise including in the junction area between the structure and the housing. The connecting part (36) is fastened onto a rear section (20'), not provided with a honeycomb core, of the internal wall (20) of the air inlet structure. A honeycomb structure (44) is fitted inside the air blower housing (22). The space inside the rear section (20') houses a forward extension (44') of the honeycomb structure (44), or a different honeycomb structure.
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申请公布号 |
US6123170(A) |
申请公布日期 |
2000.09.26 |
申请号 |
US19980132902 |
申请日期 |
1998.08.12 |
申请人 |
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE |
发明人 |
PORTE, ALAIN;ANDRE, ROBERT |
分类号 |
F01D25/24;F02C7/045;F04D29/66;(IPC1-7):B64D33/02;F02K11/00 |
主分类号 |
F01D25/24 |
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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