US2004004108A1PendingUtilityA1

Preforms for forming machined structural assemblies

Assignee: BOEING COPriority: Mar 7, 2002Filed: Jul 2, 2003Published: Jan 8, 2004
Est. expiryMar 7, 2022(expired)· nominal 20-yr term from priority
B23K 20/129
39
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Claims

Abstract

A method of constructing a preform for use in forming a machined structural assembly is provided. The method includes determining the dimensions of the machined structural assembly. First and second structural members are selected based on the predetermined dimensions of the machined structural assembly. The first structural member is positioned adjacent the second structural member so as to define at least two contact surfaces. The contact surfaces of the first and second structural members are friction welded to construct the preform such that the preform has dimensions approximating the dimensions of the machined structural assembly to thereby reduce material waste when forming the machined structural assembly. A machined structural assembly having predetermined dimensions is formed from the preform by machining away excess material.

Claims

exact text as granted — not AI-modified
That which is claimed:  
     
         1 . A preform for use in forming a machined structural assembly of predetermined dimensions, comprising: 
 a first structural member defining at least one contact surface;    a second structural member defining at least one contact surface, said at least one contact surface of the second structural member being structured to correspond to said at least one contact surface of said first structural member; and    a friction weld joint joining said at least one contact surface of said first structural member and said at least one contact surface of said second structural member such that said first and second structural members form a preform having dimensions approximating the dimensions of the machined structural assembly to thereby reduce material waste and machining time when forming the machined structural assembly.    
     
     
         2 . A preform according to  claim 1  wherein said first and second structural members comprise a material selected from the group consisting of aluminum, aluminum alloys, titanium, titanium alloys, nickel-based, steel, copper-based alloys, and beryllium-based alloys.  
     
     
         3 . A preform according to  claim 1  wherein said first and second structural members comprise dissimilar materials.  
     
     
         4 . A preform according to  claim 1  further comprising a third structural member friction welded to at least one of the first and second structural members.

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