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Inventor profile of:

Timothy Warner

City:

Voreppe

Country:

France

Published Applications:

24

Last publication date:

2014-09-25

Top Assignees for applications by Timothy Warner

The entities that hold a legal rights for patent applications filed by inventor Warner Timothy:

Recent patent applications by Warner Timothy

Timothy Warner from Voreppe, FR has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2014-09-25
US20140283958A1
Chemistry; metallurgy

High Fracture Toughness Aluminum-Copper-Lithium Sheet or Light-Gauge Plates Suitable for Fuselage Panels

 #2 | 2013-10-17
US20130269840A1
Chemistry; metallurgy

Aluminum-copper-lithium alloy with improved impact resistance

 #3 | 2012-06-21
US20120152415A1
Chemistry; metallurgy

ALUMINUM COPPER LITHIUM ALLOY WITH IMPROVED RESISTANCE UNDER COMPRESSION AND FRACTURE TOUGHNESS

 #4 | 2011-09-01
US20110209801A2
Chemistry; metallurgy

Aluminum-copper-lithium alloy with improved mechanical strength and toughness

 #5 | 2011-02-10
US20110030856A1
Chemistry; metallurgy

Aluminum-copper-lithium alloy with improved mechanical strength and toughness

 #6 | 2010-11-23
US10736979
-

Process for manufacturing structural components by machining plates

 #7 | 2009-06-23
US10406609
-

Al-Zn-Mg-Cu alloys and products with improved ratio of static mechanical characteristics to damage tolerance

 #8 | 2008-11-27
US20080289728A1
Chemistry; metallurgy

High fracture toughness aluminum-copper-lithium sheet or light-gauge plate suitable for use in a fuselage panel

 #9 | 2008-10-02
US20080236708A1
Performing operations; transporting

Process for manufacturing structural components by machining plates

 #10 | 2008-09-04
US20080210350A1
Chemistry; metallurgy

Aircraft structural member made of an Al-Cu-Mg alloy

 #11 | 2007-12-13
US20070284019A1
Chemistry; metallurgy

AlCuMg ALLOYS WITH HIGH DAMAGE TOLERANCE SUITABLE FOR USE AS STRUCTURAL MEMBERS IN AIRCRAFTS

 #12 | 2007-11-13
US10612878
-

Aircraft structural member made of an Al-Cu-Mg alloy

 #13 | 2007-08-09
US20070181229A1
Chemistry; metallurgy

High fracture toughness aluminum-copper-lithium sheet or light-gauge plates suitable for fuselage panels

 #14 | 2007-08-07
US10614888
-

AlCuMg alloys with high damage tolerance suitable for use as structural members in aircrafts

 #15 | 2007-06-14
US20070131313A1
Chemistry; metallurgy

Al-Cu-Mg-Ag-Mn alloy for structural applications requiring high strength and high ductility

 #16 | 2006-11-14
US9855556
-

Thick products made of heat-treatable aluminum alloy with improved toughness and process for manufacturing these products

 #17 | 2006-08-31
US20060191609A1
Chemistry; metallurgy

Al-Zn-Cu-Mg aluminum base alloys and methods of manufacture and use

 #18 | 2006-08-17
US20060182650A1
Chemistry; metallurgy

Al-Zn-Mg-Cu alloys and products with high mechanical characteristics and structural members suitable for aeronautical construction made thereof

 #19 | 2005-07-14
US20050150578A1
Chemistry; metallurgy

Metallurgical product and structure member for aircraft made of Al-Zn-Cu-Mg alloy

 #20 | 2005-04-21
US20050084408A1
Chemistry; metallurgy

Al—Cu—Mg—Ag—Mn-alloy for structural applications requiring high strength and high ductility

 #21 | 2005-04-07
US20050072497A1
Chemistry; metallurgy

Al-Zn-Mg-Cu alloys and products with high mechanical characteristics and structural members suitable for aeronautical construction made thereof

 #22 | 2005-03-17
US20050058568A1
Chemistry; metallurgy

Products made of Al-Zn-Mg-Cu alloys with an improved compromise between static mechanical characteristics and damage tolerance

 #23 | 2005-02-17
US20050037188A1
Performing operations; transporting

Composite laminated aluminum-glass fiber sandwich panels

 #24 | 2005-01-20
US20050011932A1
Chemistry; metallurgy

Manufacturing method for friction welded aluminum alloy parts
InventorID:

481791 ⎘