公开(公告)号：US08961715B2

公开(公告)日：2015-02-24

申请号：US14255536

申请日：2014-04-17

Applicant: Alcoa Inc.

Inventor： Gary H. Bray ,  Dhruba J. Chakrabarti ,  Diana K. Denzer ,  Jen C. Lin ,  John Newman ,  Gregory B. Venema ,  Cagatay Yanar ,  Julien Boselli

IPC: C22C21/10 ,  B64C3/26 ,  B64C3/18 ,  C22F1/053 ,  B64C1/00

CPC classification number: C22F1/053 ,  B64C3/182 ,  B64C3/185 ,  B64C3/187 ,  B64C3/26 ,  B64C2001/0081 ,  C22C21/10 ,  Y02T50/42

Abstract: Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.

Abstract translation: 约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成 基本上为：约6.8至约8.5wt。 ％Zn，约1.5至约2.00wt。 ％Mg，约1.75至约2.3wt。 ％Cu; 约0.05至约0.3wt。 ％Zr，小于约0.1wt。 ％Mn，小于约0.05wt。 ％Cr，余量为Al，附带元素和杂质及其制备方法。 瞬时公开的合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。

公开(公告)号：US20140248176A1

公开(公告)日：2014-09-04

申请号：US14283024

申请日：2014-05-20

Applicant: ALCOA INC.

Inventor： Jen C. Lin ,  Ralph R. Sawtell ,  Gary H. Bray ,  Cindie Giummarra ,  Andre Wilson ,  Gregory B. Venema

IPC: C22C21/16

Abstract: New 2xxx aluminum alloys containing vanadium are disclosed. In one embodiment, the aluminum alloy includes 3.3-4.1 wt. % Cu, 0.7-1.3 wt. % Mg, 0.01-0.16 wt. % V, 0.05-0.6 wt. % Mn, 0.01 to 0.4 wt. % of at least one grain structure control element, the balance being aluminum, incidental elements and impurities. The new alloys may realize an improved combination of properties, such as in the T39 or T89 tempers.

公开(公告)号：US20140212326A1

公开(公告)日：2014-07-31

申请号：US14242577

申请日：2014-04-01

Applicant: ALCOA INC.

Inventor： Edward L. Colvin ,  Roberto J. Rioja ,  Les A. Yocum ,  Diana K. Denzer ,  Todd K. Cogswell ,  Gary H. Bray ,  Ralph R. Sawtell ,  Andre L. Wilson

IPC: C22C21/16

CPC classification number: C22C21/16 ,  C22C21/18 ,  C22F1/057

Abstract: Improved aluminum-copper-lithium alloys are disclosed. The alloys may include 3.4-4.2 wt. % Cu, 0.9-1.4 wt. % Li, 0.3-0.7 wt. % Ag, 0.1-0.6 wt. % Mg, 0.2-0.8 wt. % Zn, 0.1-0.6 wt. % Mn, and 0.01-0.6 wt. % of at least one grain structure control element, the balance being aluminum and incidental elements and impurities. The alloys achieve an improved combination of properties over prior art alloys.

Abstract translation: 公开了改进的铝 - 铜 - 锂合金。 合金可以包括3.4-4.2wt。 ％Cu，0.9-1.4重量％ ％Li，0.3-0.7wt。 ％Ag，0.1-0.6wt。 ％Mg，0.2-0.8wt。 ％Zn，0.1-0.6wt。 ％Mn，和0.01-0.6wt。 ％的至少一种晶粒结构控制元素，余量为铝和附带元素和杂质。 与现有技术的合金相比，合金实现了改进的性能组合。

公开(公告)号：US20150368773A1

公开(公告)日：2015-12-24

申请号：US14607912

申请日：2015-01-28

Applicant: ALCOA INC.

Inventor： Gary H. Bray ,  Dhruba J. Chakrabarti ,  Diana K. Denzer ,  Jen C. Lin ,  John Newman ,  Gregory B. Venema ,  Cagatay Yanar ,  Julien Boselli

IPC: C22F1/053 ,  C22C21/10

CPC classification number: C22F1/053 ,  B64C3/182 ,  B64C3/185 ,  B64C3/187 ,  B64C3/26 ,  B64C2001/0081 ,  C22C21/10 ,  Y02T50/42

Abstract: Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.

Abstract translation: 约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成 基本上为：约6.8至约8.5wt。 ％Zn，约1.5至约2.00wt。 ％Mg，约1.75至约2.3wt。 ％Cu; 约0.05至约0.3wt。 ％Zr，小于约0.1wt。 ％Mn，小于约0.05wt。 ％Cr，余量为Al，附带元素和杂质及其制备方法。 瞬时公开的合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。

公开(公告)号：US20140230974A1

公开(公告)日：2014-08-21

申请号：US13791988

申请日：2013-03-09

Applicant: Alcoa Inc.

Inventor： Jen C. Lin ,  John M. Newman ,  Ralph R. Sawtell ,  Rajeev G. Kamat ,  Darl G. Boysel ,  Gary H. Bray ,  James Daniel Bryant ,  Brett P. Connor ,  Mario Greco ,  Gino Norman Iasella ,  David J. McNeish ,  Shawn J. Murtha ,  Roberto J. Rioja ,  Shawn P. Sullivan

IPC: C22F1/047

CPC classification number: C22C21/06 ,  C22C21/08 ,  C22C21/10 ,  C22F1/047 ,  C22F1/053

Abstract: New magnesium-zinc aluminum alloy bodies and methods of producing the same are disclosed. The new magnesium-zinc aluminum alloy bodies generally include 3.0-6.0 wt. % magnesium and 2.5-5.0 wt. % zinc, where at least one of the magnesium and the zinc is the predominate alloying element of the aluminum alloy bodies other than aluminum, and wherein (wt. % Mg)/(wt. % Zn) is from 0.6 to 2.40, and may be produced by preparing the aluminum alloy body for post-solutionizing cold work, cold working by at least 25%, and then thermally treating. The new magnesium-zinc aluminum alloy bodies may realize improved strength and other properties.

Abstract translation: 公开了新的镁 - 锌铝合金体及其制造方法。 新的镁 - 锌铝合金体通常包括3.0-6.0wt。 ％镁和2.5-5.0重量％ ％锌，其中至少一种镁和锌是除铝以外的铝合金体的主要合金元素，其中（重量％Mg）/（重量％Zn）为0.6〜2.40，并且可以 通过制备用于后冷却冷加工的铝合金体，冷加工至少25％，然后进行热处理来制备。 新型镁锌铝合金体可以实现强度提高等性能。

公开(公告)号：US09587298B2

公开(公告)日：2017-03-07

申请号：US13791988

申请日：2013-03-09

Applicant: Alcoa Inc.

Inventor： Jen C. Lin ,  John M. Newman ,  Ralph R. Sawtell ,  Rajeev G. Kamat ,  Darl G. Boysel ,  Gary H. Bray ,  James Daniel Bryant ,  Brett P. Connor ,  Mario Greco ,  Gino Norman Iasella ,  David J. McNeish ,  Shawn J. Murtha ,  Roberto J. Rioja ,  Shawn P. Sullivan

IPC: C22F1/047 ,  C22C21/06 ,  C22C21/08 ,  C22C21/10 ,  C22F1/053

CPC classification number: C22C21/06 ,  C22C21/08 ,  C22C21/10 ,  C22F1/047 ,  C22F1/053

Abstract: New magnesium-zinc aluminum alloy bodies and methods of producing the same are disclosed. The new magnesium-zinc aluminum alloy bodies generally include 3.0-6.0 wt. % magnesium and 2.5-5.0 wt. % zinc, where at least one of the magnesium and the zinc is the predominate alloying element of the aluminum alloy bodies other than aluminum, and wherein (wt. % Mg)/(wt. % Zn) is from 0.6 to 2.40, and may be produced by preparing the aluminum alloy body for post-solutionizing cold work, cold working by at least 25%, and then thermally treating. The new magnesium-zinc aluminum alloy bodies may realize improved strength and other properties.

Abstract translation: 公开了新的镁 - 锌铝合金体及其制造方法。 新的镁 - 锌铝合金体通常包括3.0-6.0wt。 ％镁和2.5-5.0重量％ ％锌，其中至少一种镁和锌是除铝以外的铝合金体的主要合金元素，其中（重量％Mg）/（重量％Zn）为0.6〜2.40，并且可以 通过制备用于后冷却冷加工的铝合金体，冷加工至少25％，然后进行热处理来制备。 新型镁锌铝合金体可以实现强度提高等性能。

公开(公告)号：US20140227131A1

公开(公告)日：2014-08-14

申请号：US14255536

申请日：2014-04-17

Applicant: ALCOA INC.

Inventor： Gary H. Bray ,  Dhruba J. Chakrabarti ,  Diana K. Denzer ,  Jen C. Lin ,  John Newman ,  Gregory B. Venema ,  Cagatay Yanar ,  Julien Boselli

IPC: C22C21/10

CPC classification number: C22F1/053 ,  B64C3/182 ,  B64C3/185 ,  B64C3/187 ,  B64C3/26 ,  B64C2001/0081 ,  C22C21/10 ,  Y02T50/42

Abstract: Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.

Abstract translation: 约4英寸厚或以下的铝合金产品具有在固溶热处理，淬火和人工老化的同时实现的能力，以及由产品制成的零件中，改进了强度，断裂韧性和耐腐蚀性的组合，该合金组成 基本上为：约6.8至约8.5wt。 ％Zn，约1.5至约2.00wt。 ％Mg，约1.75至约2.3wt。 ％Cu; 约0.05至约0.3wt。 ％Zr，小于约0.1wt。 ％Mn，小于约0.05wt。 ％Cr，余量为Al，附带元素和杂质及其制备方法。 瞬时公开的合金可用于制造商用飞机的结构构件，包括但不限于上部翼皮和桁条，翼梁盖，翼梁腹板和构成或整体结构的肋。