Turbo compressor in an axial type of construction

Details Turbo compressor in an axial type of construction Turbo compressor in an axial type of construction

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 17/16 (2006.01) F04D 29/54 (2006.01)

Patent

CA 2652272

Turbo compressor in an axial type of construction, having a bladed stator and a bladed rotor, and having a longitudinally split compressor casing and a guide blade ring with adjustable guide blades, wherein the guide blades are pivotably mounted about radial axes radially within their aerofoil on an inner ring belonging to the stator. The inner ring is split, i.e. segmented, at at least two points of its circumference; furthermore, the inner ring has for each guide blade at least one bearing bush which can be inserted radially into an opening from inside.

Turbocompresseur en montage axial, comportant un stator et un rotor câblés, un boîtier de compression refendu et une couronne de pales fixes comprenant des pales réglables, lesdites pales étant montées sur paliers, à l'intérieur de leur ailette, de manière radiale, sur une bague de roulement intérieure appartenant au stator et pivotant autour d'axes radiaux. La bague intérieure est scindée, c'est-à-dire segmentée, au moins à deux endroits de son pourtour, et comprend par ailleurs, pour chaque pale fixe, au moins un coussinet pouvant être inséré, de manière radiale, de l'intérieur, dans un orifice.

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