US Patent No: 6,582,539

Number of patents in Portfolio can not be more than 2000

Method for making large composite structures without use of an autoclave

Stats

ALSO PUBLISHED AS: 20020185207
ATTORNEY / AGENT: (SPONSORED)
 

Importance

Loading Importance Indicators... loading....

Abstract

A method for fabrication or production of composite structures, which has particular advantages when fabricating large structures, includes the steps of procuring a composite panel, such as carbon-fiber-reinforced resin. The edge of the composite panel its adhesively fixed in the slot of a bifurcated metallic piece. After the composite panel is adhesively fixed to the metallic piece, the metallic piece is stir-friction welded to another metal piece. The stir-friction welding occurs at a lower temperature than fusion welding, and so the adhesive bond between the metallic element and the composite panel is less affected. When two composite panels are each adhesively fastened to a metallic element, the two metallic elements can, in turn, be stir-friction welded. Thus, large panels can be fabricated.

Loading the Abstract Image... loading....

First Claim

Related Publications

Loading Related Publications... loading....

Patent Owner(s)

Patent OwnerAddressTotal Patents
LOCKHEED MARTIN CORPORATIONBETHESDA, MD5429

International Classification(s)

  • [Classification Symbol]
  • [Patents Count]

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Arbegast, William John Cheriere, MS 2 57
Iwanczyk, Timothy Dennis St. Tammany Parish, LA 1 7

Cited Art

Patent Info (Count) # Cites Year
 
HITACHI, LTD. (4)
6,193,137 Constructive body and friction stir welding method 59 1998
6,354,483 Friction stir welding method 11 2000
6,378,754 Friction stir welding method including removal of protruding portion, and structural body formed thereby 12 2001
6,382,498 Friction stir welding method including positioning of rotary tool, and structural body formed thereby 15 2001
 
THE BOEING COMPANY (1)
6,045,027 Friction stir welding interlocking joint design and method 49 1998

Patent Citation Ranking

Forward Cites

Patent Info (Count) # Cites Year
 
THE BOEING COMPANY (2)
7,240,821 Method for joining at least two adjoining work-pieces by friction stir and/or friction stir spot welding 4 2005
8,186,567 Method for forming a weldbonded structure 0 2006
 
AIRBUS OPERATIONS LIMITED (1)
7,392,928 Welding process for large structures 0 2004
 
ALCOA INC. (1)
7,115,324 Method of combining welding and adhesive bonding for joining metal components 3 2003
 
ECLIPSE AEROSPACE, INC. (1)
7,225,966 Welded joints with polymer sealant 3 2003
 
LOCKHEED MARTIN CORPORATION (1)
8,261,961 Metal matrix carbon nanotube composite material and method of making same 0 2008
 
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY (1)
7,959,058 Hybrid composite welded joint 2 2006

Maintenance Fees

Fee Large entity fee small entity fee micro entity fee due date
11.5 Year Payment $7400.00 $3700.00 $1850.00 Dec 24, 2014
Fee Large entity fee small entity fee micro entity fee
Surcharge - 11.5 year - Late payment within 6 months $160.00 $80.00 $40.00
Surcharge after expiration - Late payment is unavoidable $700.00 $350.00 $175.00
Surcharge after expiration - Late payment is unintentional $1,640.00 $820.00 $410.00