US Patent 7114255 Method of making a gas turbine engine diffuser
Patent 7114255 was granted and assigned to Pratt & Whitney Canada on October, 2006 by the United States Patent and Trademark Office.
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Patent Inventor Names
Bertrand Gendreau0
Ioan Sasu0
Robert Francois Lanoue0
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Patent abstract
A method of machining a plurality of intersecting bores in an object, the method comprising steps of machining a first bore, plugging the first bore, machining a second bore so as to intersect the first bore, and unplugging the first bore.
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US Patent 07114255 Method of making a gas turbine engine diffuser US Patent 7114255 Method of making a gas turbine engine diffuser
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Patent Number
071142550
Patent Number
71142550
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Official Website
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
071142550
Date of Patent
October 3, 2006
0Patent Application Number
107221250
Date Filed
November 26, 2003
0Official Website
Patent Primary Examiner
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US Patent 07114255 Method of making a gas turbine engine diffuser
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07114255
Date of patent
October 3, 2006
Patent application number
10722125
Date Filed
November 26, 2003
Patent primary examiner
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