MX2017011840A - Aleaciones de aluminio 7xxx de alta resistencia y metodos para fabricarlas. - Google Patents
Aleaciones de aluminio 7xxx de alta resistencia y metodos para fabricarlas.Info
- Publication number
- MX2017011840A MX2017011840A MX2017011840A MX2017011840A MX2017011840A MX 2017011840 A MX2017011840 A MX 2017011840A MX 2017011840 A MX2017011840 A MX 2017011840A MX 2017011840 A MX2017011840 A MX 2017011840A MX 2017011840 A MX2017011840 A MX 2017011840A
- Authority
- MX
- Mexico
- Prior art keywords
- methods
- alloys
- making
- high strength
- ingot
- Prior art date
Links
- 229910000838 Al alloy Inorganic materials 0.000 title abstract 3
- 238000000034 method Methods 0.000 title abstract 3
- 229910045601 alloy Inorganic materials 0.000 abstract 3
- 239000000956 alloy Substances 0.000 abstract 3
- 229910052751 metal Inorganic materials 0.000 abstract 2
- 239000002184 metal Substances 0.000 abstract 2
- 238000005266 casting Methods 0.000 abstract 1
- 238000005097 cold rolling Methods 0.000 abstract 1
- 238000005098 hot rolling Methods 0.000 abstract 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
- B62D29/008—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of light alloys, e.g. extruded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Abstract
En la presente se describen aleaciones de aluminio de la serie 7xxx novedosas. Las aleaciones exhiben resistencia alta. Las aleaciones se pueden usar en una variedad de aplicaciones, que incluyen aplicaciones automotrices, de transporte, electrónicas, aeroespaciales e industriales. En la presente también se describen métodos para fabricar y procesar estas aleaciones. En la presente también se describen métodos para producir una lámina de metal, que incluye fundir una aleación de aluminio como se describe en la presente para formar un lingote, homogeneizar el lingote, laminar en caliente el lingote para producir una banda caliente y laminar en frío la banda caliente para formar una lámina de metal de un espesor final.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201562248796P | 2015-10-30 | 2015-10-30 | |
US201662326858P | 2016-04-25 | 2016-04-25 | |
PCT/US2016/059272 WO2017075319A1 (en) | 2015-10-30 | 2016-10-28 | High strength 7xxx aluminum alloys and methods of making the same |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2017011840A true MX2017011840A (es) | 2018-02-01 |
Family
ID=57960808
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2017011840A MX2017011840A (es) | 2015-10-30 | 2016-10-28 | Aleaciones de aluminio 7xxx de alta resistencia y metodos para fabricarlas. |
MX2023001684A MX2023001684A (es) | 2015-10-30 | 2017-09-14 | Aleaciones de aluminio 7xxx de alta resistencia y metodos para fabricarlas. |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2023001684A MX2023001684A (es) | 2015-10-30 | 2017-09-14 | Aleaciones de aluminio 7xxx de alta resistencia y metodos para fabricarlas. |
Country Status (23)
Country | Link |
---|---|
US (2) | US11421309B2 (es) |
EP (2) | EP3265595B1 (es) |
JP (2) | JP6971151B2 (es) |
KR (2) | KR20170138533A (es) |
CN (2) | CN107406925A (es) |
AU (1) | AU2016344192B2 (es) |
BR (1) | BR112017021490B1 (es) |
CA (1) | CA2979717C (es) |
CY (1) | CY1121505T1 (es) |
DK (1) | DK3265595T3 (es) |
ES (1) | ES2719555T3 (es) |
HR (1) | HRP20190548T1 (es) |
HU (1) | HUE042400T2 (es) |
IL (1) | IL258885A (es) |
LT (1) | LT3265595T (es) |
MX (2) | MX2017011840A (es) |
PL (1) | PL3265595T3 (es) |
PT (1) | PT3265595T (es) |
RS (1) | RS58615B1 (es) |
RU (1) | RU2717434C2 (es) |
SI (1) | SI3265595T1 (es) |
WO (1) | WO2017075319A1 (es) |
ZA (1) | ZA201802759B (es) |
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