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Spun metal form used to manufacture dual alloy turbine wheel
   
Document Number
US Patent 7000306
Issued Date
February 21, 2006
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Abstract
A spun metal form used to manufacture a dual alloy turbine wheel. The spun metal form prevents braze alloy contamination of the hub/casting interface by relocating the braze joint away from the interface. The spun metal form allows for the re-working of components after failed vacuum brazing and increases the time to failure of dual alloy turbine wheels.
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Number of Claims:
34
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Owner
Published
February 21, 2006
Application Number
10/919,833
Filed
August 16, 2004
US Classification
29/559   29/281.1
Int'l Classification
B23Q   7/00   (20060101)  
Examiner
Attorney/Law Firm
Parent Case
CROSS-REFERENCE TO RELATED APPLICATIONS This is a divisional application of U.S. application Ser. No. 10/323,156, filed on Dec. 18, 2002, now U.S. Pat. No. 6,935,006.
USPTO Field of Search
29/559   29/28.1   29/889.1   29/458   29/49.1   29/428   29/281.3  
Related Patents
7516526 - Spun metal form used to manufacture dual alloy turbine wheel - Owned by Honeywell International Inc. (Morristown, NJ)

A spun metal form used to manufacture a dual alloy turbine wheel. The spun metal form prevents braze alloy contamination of the hub/casting interface by relocating the braze joint away from the interface. The spun metal form allows for the re-working of components after failed vacuum brazing and increases the time to failure of dual alloy turbine wheels.

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Description
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