US Patent 7322223 Creep forming a metallic component

Patent 7322223 was granted and assigned to Airbus UK on January, 2008 by the United States Patent and Trademark Office.

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Patent

Patent attributes

Current Assignee

Airbus UK

Patent Jurisdiction

United States Patent and Trademark Office

Patent Number

73222230

Patent Inventor Names

Andrew Levers0

Date of Patent

January 29, 2008

Patent Application Number

104772280

Date Filed

July 4, 2002

Patent Citations Received

‌

US Patent 11852035 Multi-cover gas turbine engine component

Patent Primary Examiner

Roy King

Patent abstract

A method of creep forming a metallic component is provided. The method includes the steps of applying static loading and cyclic loading and/or vibration to the component during the creep forming thereof to act as a source of additional energy.

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