US2014248157A1PendingUtilityA1

Blade or vane of differing roughness and production process

Assignee: AHMAD FATHIPriority: Oct 24, 2012Filed: Oct 24, 2013Published: Sep 4, 2014
Est. expiryOct 24, 2032(~6.3 yrs left)· nominal 20-yr term from priority
Inventors:Fathi Ahmad
F04D 29/681F05D 2250/61F05D 2240/123F05D 2240/306F05D 2250/611F05D 2300/516F04D 29/023F04D 29/30F05B 2250/611F05D 2250/62F05D 2250/60F05B 2250/621Y10T29/49336F05D 2300/611F05B 2250/60F05D 2240/124F05B 2250/62F05D 2240/31F05B 2250/61F01D 5/147F05D 2240/305F04D 29/284Y02T50/60F04D 29/324F05D 2250/621
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Claims

Abstract

A blade or vane of different roughness and a process for producing such a blade or vane are presented. The performance of the blade or vane of a compressor or of a turbine can be improved because of the different configuration of the roughness of the surfaces on the suction side and the pressure side of the blade or vane.

Claims

exact text as granted — not AI-modified
1 . A curved blade or vane, comprising:
 a suction side; and   a pressure side,   wherein the blade or vane comprises a different roughnesses between a surface of the suction side and a surface of the pressure side, and   wherein the surface of the suction side comprises a lesser roughness than the surface of the pressure side.   
     
     
         2 . The blade or vane as claimed in  claim 1 , wherein the blade or vane comprises an uncoated substrate surface, and wherein the different roughnesses are formed on the substrate surface. 
     
     
         3 . The blade or vane as claimed in  claim 1 , wherein a metallic coating is applied to the blade or vane as an outermost layer and comprises the different roughnesses. 
     
     
         4 . The blade or vane as claimed in  claim 1 , wherein a ceramic coating is applied to the blade or vane as an outermost layer and comprises the different roughnesses. 
     
     
         5 . The blade or vane as claimed in  claim 1 , wherein roughness of the surface of the pressure side is at least two times greater than roughness of the surface of the suction side. 
     
     
         6 . The blade or vane as claimed in  claim 1 , wherein roughness of the surface of the pressure side is at least three times greater than roughness of the surface of the suction side. 
     
     
         7 . The blade or vane as claimed in  claim 1 , wherein the surface of the suction side comprises a roughness of ≦6 μm. 
     
     
         8 . The blade or vane as claimed in  claim 1 , wherein the surface of the pressure side comprises a roughness of ≧20 μm. 
     
     
         9 . The blade or vane as claimed in  claim 1 , wherein the surface of the pressure side comprises a roughness of 20 μm to 30 μm. 
     
     
         10 . The blade or vane as claimed in  claim 1 , wherein roughness of the surface of the suction side is at least 20% less rough than the surface of the pressure side. 
     
     
         11 . The blade or vane as claimed in  claim 1 , wherein the blade or vane is for a compressor or a turbine. 
     
     
         12 . A process for producing a blade or vane, comprising:
 producing the blade or vane according to  claim 1 ,   wherein only the surface of the pressure side of the blade or vane is roughened.   
     
     
         13 . A process for producing a blade or vane, comprising:
 producing the blade or vane according to  claim 1 ,   wherein only the surface of the suction side of the blade or vane is smoothed.

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