US2007160464A1PendingUtilityA1

Anti-wear device for a guide pivot of a variable-pitch vane of a turbomachine compressor

Assignee: SNECMAPriority: Jan 6, 2006Filed: Dec 29, 2006Published: Jul 12, 2007
Est. expiryJan 6, 2026(expired)· nominal 20-yr term from priority
C23C 4/04F01D 5/3092F01D 17/162F05D 2300/509F05D 2300/133F04D 29/563F16C 2360/23
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Claims

Abstract

The invention relates to a variable-pitch vane for a turbomachine compressor, the vane including a bushing mounted to rotate about a guide pivot of the vane for mounting in a casing of the turbomachine, the pivoting contact between the bushing and the guide pivot being of the nickel-graphite and titanium type.

Claims

exact text as granted — not AI-modified
1 . A variable-pitch vane for a turbomachine compressor, the vane including a bushing mounted to pivot about a guide pivot of the vane and for mounting in a casing of the turbomachine, wherein the pivoting contact between the bushing and the guide pivot is of the nickel-graphite and titanium type. 
   
   
       2 . A vane according to  claim 1 , in which the guide pivot is made of a titanium-based material, wherein the bushing is constituted by a material based on nickel and on graphite. 
   
   
       3 . A vane according to  claim 2 , in which the bushing is obtained by sintering a powder based on nickel and on graphite in a mold. 
   
   
       4 . A vane according to  claim 1 , in which the guide pivot is not constituted by a titanium-based metallic material, wherein said guide pivot is covered by a deposit of nickel-graphite, and the bushing is constituted by a titanium-based material. 
   
   
       5 . A vane according to  claim 1 , in which the guide pivot is not constituted by a titanium-based metallic material, the vane further including a metal ferrule covered in a deposit of nickel-graphite and heat-shrunk on the guide pivot, the bushing being constituted by a titanium-based material. 
   
   
       6 . A vane according to  claim 1 , in which the guide pivot is not constituted by a titanium-based metallic material, the vane further including a ferrule constituted by a material based on nickel and on graphite, and heat-shrunk onto the guide pivot, the bushing being constituted by a titanium-based material. 
   
   
       7 . A vane according to  claim 6 , wherein the ferrule is obtained by sintering a powder based on nickel and on graphite in a mold. 
   
   
       8 . A vane according to  claim 4 , wherein the nickel-graphite is deposited by thermally spraying a powder based on nickel and on graphite. 
   
   
       9 . A turbomachine compressor, including a plurality of variable-pitch vanes according to  claim 1 . 
   
   
       10 . A turbomachine, including a plurality of variable-pitch vanes according to  claim 1 .

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