US2007003412A1PendingUtilityA1

Abradable material composition, a thermomechanical part or casing including a coating, and a method of fabricating or repairing a coating presenting said composition

Assignee: SNECMAPriority: Jun 30, 2005Filed: Jun 29, 2006Published: Jan 4, 2007
Est. expiryJun 30, 2025(expired)· nominal 20-yr term from priority
F05D 2300/611F05D 2250/241C08K 7/24B29C 39/10B29K 2083/00C09D 183/04F05D 2230/80B23P 6/002F04D 29/164F05D 2300/437F05D 2300/61F05D 2230/90B29C 67/246F04D 29/023F01D 11/122
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Claims

Abstract

The invention relates to an abradable material composition comprising a resin-based matrix, in particular a silicone matrix together with filler comprising hollow beads. In characteristic manner, the hollow beads withstand high temperatures and are made of refractory material. The hollow beads are preferably made of an alumino-silicate material. The composition is applicable to making abradable coverings for compressor casings, in particular casings for compressors of the low pressure type or of the booster type, or for a fan, the covering being in register with moving blades.

Claims

exact text as granted — not AI-modified
1 . A composition of abradable material comprising a matrix based on resin, in particular silicone resin, and filler comprising hollow beads, wherein the hollow beads are made of refractory material, glass being excluded.  
   
   
       2 . A composition according to  claim 1 , wherein the refractory material comprises alumina and/or silica and/or zirconia.  
   
   
       3 . A composition according to  claim 1 , wherein the refractory material belongs to the family constituted by alumino-silicate materials.  
   
   
       4 . A composition according to  claim 1 , wherein said refractory material presents a melting temperature greater than 700° C., preferably greater than 750° C.  
   
   
       5 . A thermomechanical part comprising a metal substrate covered in a wear portion comprising a covering presenting the composition according to  claim 1  and a bonding primer layer comprising silicone.  
   
   
       6 . A thermomechanical part according to  claim 5 , wherein the substrate is made to titanium, steel, aluminum, or an alloy of any one of said metals.  
   
   
       7 . A thermomechanical part according to  claim 5 , wherein the primer layer is colored.  
   
   
       8 . A thermomechanical part according to  claim 5 , the part serving to form a wear portion of a sealing labyrinth, associated with wipers, in particular for a booster.  
   
   
       9 . A casing for a compressor or a fan, in which the face of the wall that is to be in register with the moving blades includes an abradable covering presenting the composition according to  claim 1 .  
   
   
       10 . A turbomachine including a casing according to  claim 9  or a thermomechanical part according to  claim 5 .  
   
   
       11 . A method of fabricating or repairing an abradable covering on a metal substrate, wherein the following steps are performed: 
 a) preparing a composition according to  claim 1;  and    b) applying said composition on said metal substrate in order to form said covering.    
   
   
       12 . A method according to  claim 11 , wherein application step b) is performed by direct injection.  
   
   
       13 . A method according to  claim 11 , wherein application step b) comprises the following substeps: 
 b1) providing at least one pre-molded element presenting the composition according to  claim 1;     b2) depositing adhesive on the metal substrate and/or on said pre-molded element; and    b3) depositing said element on the substrate and holding said element firmly against the substrate while the adhesive sets.    
   
   
       14 . A method according to  claim 13 , wherein the adhesive comprises hot-polymerizable silicone resin.  
   
   
       15 . A method according to  claim 11 , wherein an additional step is performed prior to step a) in which a bonding primer layer is applied to the substrate, the primer layer comprising silicone.

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