发明名称 |
AIRCRAFT ENGINE STRUT WITH INTEGRATED SENSOR COMPONENT |
摘要 |
An engine strut for providing fan hub frame structural support and monitoring an air flow within an aircraft engine includes an airfoil coupled to the aircraft engine and has a first portion and a second portion. The first portion is positioned upstream of the second portion with respect to the air flow. A shield is coupled to the engine and positioned between the first portion and the second portion. The shield includes a first side spaced from the first portion and defining a first flow path with the first portion. The shield further includes a second side spaced from the second portion and defining a second flow path with the second portion. At least one sensor is coupled to the aircraft engine and positioned in flow communication with the second flow path. |
申请公布号 |
EP3063380(A1) |
申请公布日期 |
2016.09.07 |
申请号 |
EP20140861158 |
申请日期 |
2014.10.29 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
TAN, CHIONG, SIEW;PRITCHARD, BYRON, ANDREW;OTTA, SHOURYA, PRAKASH |
分类号 |
F01D17/08;F01D5/14;F01D21/00;F01D25/16;F02C7/05;F02C7/20 |
主分类号 |
F01D17/08 |
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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