发明名称 |
TEC MIXER WITH VARIABLE THICKNESSES |
摘要 |
<p>A mixer of a bypass turbine aeroengine according to one embodiment, includes circumferential inner and outer flow surfaces in a wavy configuration to form a plurality of lobes of the mixer. The mixer has an upstream end portion of sheet metal with a first thickness and a downstream end portion of sheet metal with a second thickness less than the first thickness.</p> |
申请公布号 |
CA2826478(A1) |
申请公布日期 |
2014.03.17 |
申请号 |
CA20132826478 |
申请日期 |
2013.09.09 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
DUROCHER, ERIC;LEFEBVRE, GUY |
分类号 |
F02K1/38;F02K1/46 |
主分类号 |
F02K1/38 |
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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