Invention Grant
- Patent Title: In-line removable heat shield for a turbomachine suspension yoke
- Patent Title (中): 用于涡轮机悬架轭的可插拔式热屏蔽
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Application No.: US14053862Application Date: 2013-10-15
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Publication No.: US09359954B2Publication Date: 2016-06-07
- Inventor: Lambert Olivier Marie Demoulin , Julien Pavillet , Guilhem Seize
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P
- Priority: FR1259833 20121015
- Main IPC: F02C7/24
- IPC: F02C7/24 ; F02C7/20 ; B64D27/26
Abstract:
A heat shield device for a yoke suspending an engine from an aircraft is provided. The device includes panels able to be fixed to the yoke, at least one of the panels extending radially in the direction of the axis of the engine, and a component configured to be fixed to the engine and including a groove shaped in such a way that the lower end of the panel can be inserted into it.
Public/Granted literature
- US20140102114A1 IN-LINE REMOVABLE HEAT SHIELD FOR A TURBOMACHINE SUSPENSION YOKE Public/Granted day:2014-04-17
Information query
IPC分类:
