Sheet metal turbine or compressor static shroud

F - Mech Eng,Light,Heat,Weapons – 01 – D

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Details

F01D 9/04 (2006.01) F01D 11/08 (2006.01) F01D 25/24 (2006.01) F04D 29/16 (2006.01) F04D 29/58 (2006.01)

Patent

CA 2503149

A static shroud (1) for ducting an axial gas flow past an array of blades (2) rotating about an axis, made of a sheet of metal bent to form a contiguous shroud body having a substantially uniform sheet thickness and a uniform axial profile, initiating with an upstream flange (3) flowing into a tip clearance portion (4) and terminating in a downstream flange (5).

L'invention concerne un cordage statique (1) destiné à canaliser un écoulement gazeux axial au-delà d'un jeu de pales (2) tournant autour d'un axe. Le cordage statique est constitué d'une feuille métallique courbée pour former un corps de cordage contigu présentant une épaisseur de la feuille sensiblement uniforme et un profil axial uniforme, qui commence en bride amont (3), s'étend de manière à former une partie avec jeu à l'extrémité (4) et se termine en bride aval (5).

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