ES8102198A1 - Procedimiento de fabricacion de cuerpos huecos de aleacion de aluminio resistentes a una presion interna - Google Patents
Procedimiento de fabricacion de cuerpos huecos de aleacion de aluminio resistentes a una presion internaInfo
- Publication number
- ES8102198A1 ES8102198A1 ES491989A ES491989A ES8102198A1 ES 8102198 A1 ES8102198 A1 ES 8102198A1 ES 491989 A ES491989 A ES 491989A ES 491989 A ES491989 A ES 491989A ES 8102198 A1 ES8102198 A1 ES 8102198A1
- Authority
- ES
- Spain
- Prior art keywords
- products
- hollow bodies
- manufacture
- aluminium alloy
- bursting strength
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Continuous Casting (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Pressure Vessels And Lids Thereof (AREA)
- Extrusion Of Metal (AREA)
Abstract
PROCEDIMIENTO DE FABRICACION DE CUERPOS HUECOS EN ALEACION DE ALUMINIO CON ALTAS CARACTERISTICAS MECANICAS. SE CONSIGUE DISMINUYENDO LOS CONTENIDOS DE LOS ELEMENTOS CR, MN Y ZR. SE MEJORAN LAS CARACTERISTICAS MECANICAS DE LA ALEACION, AUMENTANDO MAS ALLA DE LOS LIMITES HABITUALES LOS CONTENIDOS EN ELEMENTOS PRINCIPALES, TALES COMO ZN, CU Y ZG, Y LIMITANDO A NIVELES BAJOS O MUY BAJOS LOS CONTENIDOS DE ELEMENTOS MENORES (FE, SI, TI) Y DE LAS IMPUREZAS. POSTERIORMENTE SE CUELA Y SE TRANSFORMA EN CALIENTE LA ALEACION HOMOGENEIZADA EN FORMA DE TUBO Y SE RECALCA EN CALIENTE UNO O LOS DOS EXTREMOS. A CONTINUACION SE TRATA TERMICAMENTE POR PUESTA EN SOLUCION, TEMPLE Y REVENIDO. CON EL PROCEDIMIENTO DESCRITO PUEDEN ALCANZARSE VALORES DE LA CARGA DE RUPTURA SUPERIORES A LOS 600 MPA. APLICABLE PARA FABRICAR CUERPOS HUECOS SOMETIDOS A PRESION INTERIOR.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7915054A FR2457908A1 (fr) | 1979-06-01 | 1979-06-01 | Procede de fabrication de corps creux en alliage d'aluminium et produits ainsi obtenus |
Publications (2)
Publication Number | Publication Date |
---|---|
ES491989A0 ES491989A0 (es) | 1980-12-16 |
ES8102198A1 true ES8102198A1 (es) | 1980-12-16 |
Family
ID=9226502
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES491989A Expired ES8102198A1 (es) | 1979-06-01 | 1980-05-30 | Procedimiento de fabricacion de cuerpos huecos de aleacion de aluminio resistentes a una presion interna |
Country Status (11)
Country | Link |
---|---|
US (1) | US4345951A (es) |
EP (1) | EP0020282B1 (es) |
BE (1) | BE883565A (es) |
CA (1) | CA1118190A (es) |
CH (1) | CH644402A5 (es) |
DE (1) | DE3061495D1 (es) |
ES (1) | ES8102198A1 (es) |
FR (1) | FR2457908A1 (es) |
IT (1) | IT1130700B (es) |
NO (1) | NO153184C (es) |
ZA (1) | ZA803235B (es) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4863528A (en) * | 1973-10-26 | 1989-09-05 | Aluminum Company Of America | Aluminum alloy product having improved combinations of strength and corrosion resistance properties and method for producing the same |
FR2517702B1 (es) * | 1981-12-03 | 1985-11-15 | Gerzat Metallurg | |
US5221377A (en) * | 1987-09-21 | 1993-06-22 | Aluminum Company Of America | Aluminum alloy product having improved combinations of properties |
FR2640644B1 (fr) * | 1988-12-19 | 1991-02-01 | Pechiney Recherche | Procede d'obtention par " pulverisation-depot " d'alliages d'al de la serie 7000 et de materiaux composites a renforts discontinus ayant pour matrice ces alliages a haute resistance mecanique et bonne ductilite |
KR100341541B1 (ko) * | 1993-04-15 | 2002-11-29 | 엘지엘 1996 리미티드 | 중공본체의 제조방법 |
FR2716896B1 (fr) * | 1994-03-02 | 1996-04-26 | Pechiney Recherche | Alliage 7000 à haute résistance mécanique et procédé d'obtention. |
US5496426A (en) * | 1994-07-20 | 1996-03-05 | Aluminum Company Of America | Aluminum alloy product having good combinations of mechanical and corrosion resistance properties and formability and process for producing such product |
IL156386A0 (en) | 2000-12-21 | 2004-01-04 | Alcoa Inc | Aluminum alloy products and artificial aging method |
FR2838136B1 (fr) * | 2002-04-05 | 2005-01-28 | Pechiney Rhenalu | PRODUITS EN ALLIAGE A1-Zn-Mg-Cu A COMPROMIS CARACTERISTIQUES STATISTIQUES/TOLERANCE AUX DOMMAGES AMELIORE |
FR2838135B1 (fr) | 2002-04-05 | 2005-01-28 | Pechiney Rhenalu | PRODUITS CORROYES EN ALLIAGES A1-Zn-Mg-Cu A TRES HAUTES CARACTERISTIQUES MECANIQUES, ET ELEMENTS DE STRUCTURE D'AERONEF |
EP1683882B2 (de) | 2005-01-19 | 2010-07-21 | Otto Fuchs KG | Abschreckunempfindliche Aluminiumlegierung sowie Verfahren zum Herstellen eines Halbzeuges aus dieser Legierung |
US8083871B2 (en) | 2005-10-28 | 2011-12-27 | Automotive Casting Technology, Inc. | High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting |
US8840737B2 (en) * | 2007-05-14 | 2014-09-23 | Alcoa Inc. | Aluminum alloy products having improved property combinations and method for artificially aging same |
US8673209B2 (en) * | 2007-05-14 | 2014-03-18 | Alcoa Inc. | Aluminum alloy products having improved property combinations and method for artificially aging same |
US8206517B1 (en) | 2009-01-20 | 2012-06-26 | Alcoa Inc. | Aluminum alloys having improved ballistics and armor protection performance |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB552972A (en) * | 1942-06-12 | 1943-05-03 | Nat Smelting Co | Improvements in or relating to aluminium base alloys |
FR1322510A (fr) * | 1962-05-02 | 1963-03-29 | Aluminum Co Of America | Perfectionnement à des articles en alliage à base d'aluminium obtenu par traitement thermique |
DE2052000C3 (de) * | 1970-10-23 | 1974-09-12 | Fa. Otto Fuchs, 5882 Meinerzhagen | Verwendung einer hochfesten Aluminiumlegierung |
US4305763A (en) * | 1978-09-29 | 1981-12-15 | The Boeing Company | Method of producing an aluminum alloy product |
-
1979
- 1979-06-01 FR FR7915054A patent/FR2457908A1/fr active Granted
-
1980
- 1980-05-28 EP EP80420064A patent/EP0020282B1/fr not_active Expired
- 1980-05-28 DE DE8080420064T patent/DE3061495D1/de not_active Expired
- 1980-05-29 IT IT22416/80A patent/IT1130700B/it active
- 1980-05-30 NO NO801611A patent/NO153184C/no unknown
- 1980-05-30 CH CH421480A patent/CH644402A5/fr not_active IP Right Cessation
- 1980-05-30 US US06/155,116 patent/US4345951A/en not_active Expired - Lifetime
- 1980-05-30 ZA ZA00803235A patent/ZA803235B/xx unknown
- 1980-05-30 CA CA000353060A patent/CA1118190A/fr not_active Expired
- 1980-05-30 BE BE0/200831A patent/BE883565A/fr not_active IP Right Cessation
- 1980-05-30 ES ES491989A patent/ES8102198A1/es not_active Expired
Also Published As
Publication number | Publication date |
---|---|
IT1130700B (it) | 1986-06-18 |
FR2457908B1 (es) | 1984-03-02 |
BE883565A (fr) | 1980-12-01 |
ZA803235B (en) | 1981-05-27 |
NO153184B (no) | 1985-10-21 |
CA1118190A (fr) | 1982-02-16 |
ES491989A0 (es) | 1980-12-16 |
CH644402A5 (fr) | 1984-07-31 |
NO153184C (no) | 1986-01-29 |
NO801611L (no) | 1980-12-02 |
IT8022416A0 (it) | 1980-05-29 |
US4345951A (en) | 1982-08-24 |
EP0020282B1 (fr) | 1982-12-29 |
FR2457908A1 (fr) | 1980-12-26 |
EP0020282A1 (fr) | 1980-12-10 |
DE3061495D1 (en) | 1983-02-03 |
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