Invention Grant
US09366150B2 Method for mounting a stator blading of a turbomachine, an engine casing and a turbomachine comprising at least one stator blading mounted on this engine casing
有权
一种用于安装涡轮机,发动机壳体和涡轮机的定子叶片的方法,包括安装在该发动机壳体上的至少一个定子叶片
- Patent Title: Method for mounting a stator blading of a turbomachine, an engine casing and a turbomachine comprising at least one stator blading mounted on this engine casing
- Patent Title (中): 一种用于安装涡轮机,发动机壳体和涡轮机的定子叶片的方法,包括安装在该发动机壳体上的至少一个定子叶片
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Application No.: US13659404Application Date: 2012-10-24
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Publication No.: US09366150B2Publication Date: 2016-06-14
- Inventor: Maurice Guy Judet , Jerome Etienne Robert Cameau , Fabrice Marcel Noel Garin , Alain Paul Madec
- 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: FR1159692 20111026
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D25/24

Abstract:
The present disclosure aims at achieving a mounting of a turbomachine stator blading while avoiding a delicate machining process of the engine casing. It also aims at simplifying the mounting as well as at reducing the costs, and at decreasing the number of item references for the engine. To achieve these objects, the turbomachine uses an extension of the engine casing. A turbomachine comprises at least one stator blading for air or gas stream flowing on the internal engine casing. The stator blading comprises a rim which is assembled on a radial extension of engine casing with an axial fastener. In a preferred embodiment of the turbomachine, the engine casing presents an annular wall provided with fingers originating axially from this wall and extending according to a curvature so that they present a radial extension tip against the rim of the stator blading.
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