F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 9/04 (2006.01) F01D 17/16 (2006.01) F01D 25/24 (2006.01)
Patent
CA 2746134
A method for mounting an integral inner ring (10) of a turbocompressor stator to a guide vane ring (12) comprises the following steps: - Providing the guide vane ring (12) with an inner radius S; - Providing inner ring (10) with an outer radius R, which corresponds to the inner radius S; - Pre-tensioning inner ring (10) to an outer radius r that is smaller than the outer radius R of the untensioned inner ring (10); and - Relaxing inner ring (10) to the outer radius R.
L'invention concerne un procédé de montage d'une bague intérieure intégrée (10) d'un stator de turbocompresseur sur une couronne d'aubes directrices (12), consistant à fournir la couronne d'aubes directrices (12) ayant un rayon intérieur (S); à fournir la bague intérieure (10) ayant un rayon extérieur (R) correspondant au rayon intérieur (S); à serrer la bague intérieure (10) à un rayon extérieur (r) inférieur au rayon extérieur (R) de la bague intérieure (10) non précontrainte; et à détendre la bague intérieure (10) au rayon extérieur (R).
Millman Ip
Mtu Aero Engines Gmbh
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