Turbocompressor provided with an abradable coating
AssigneeMotoren-und Turbinen-Union
InventorsAxel Rossmann, Herbert Merz
Life of this patent
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Abstract
An improvement for a turbocompressor having a rotor, a stator and a casing, and an abradable coating provided between the rotor blades and the casing, or between the stator vanes and the rotor, such that the blades make initial contact with the coating to abrade the coating and produce a minimal clearance. The abradable coating is formed on a member having a first layer of carbon-fiber reinforced graphite adapted for attaching the coating member to the casing or rotor, and a second layer of graphite in the region in which the blade tips are intended to rub. The second layer may optionally contain, preferably radially oriented brush-type graphite-fiber reinforcements, or be entirely composed thereof.
Claims16
In a turbocompressor having a rotatable element comprising a rotor including rotor blades, a stationary element comprising a stator including stator vanes and a casing, and a member with an abradable coating interposed between the rotatable and stationary elements, said abradable coating facing the rotor blades such that the rotor blades come into initial contact with the coating to produce a minimal clearance therewith, the improvement wherein said member with the abradable coating comprises a first layer of carbon-reinforced graphite and a second layer comprised solely of graphite, said first layer being supported by one of said elements with said second layer facing the other of said elements to be abraded upon relative rotation of said elements to establish the minimal clearance therebetween.
Dependencies are inferred from the claim text.