JPS5687647A - Airplane stringer material and its manufacture - Google Patents
Airplane stringer material and its manufactureInfo
- Publication number
- JPS5687647A JPS5687647A JP16319379A JP16319379A JPS5687647A JP S5687647 A JPS5687647 A JP S5687647A JP 16319379 A JP16319379 A JP 16319379A JP 16319379 A JP16319379 A JP 16319379A JP S5687647 A JPS5687647 A JP S5687647A
- Authority
- JP
- Japan
- Prior art keywords
- rate
- cooled
- manufacture
- softening
- reheated
- 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.)
- Granted
Links
Landscapes
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Abstract
PURPOSE: To manufacture an airplane stringer material with superior characteristics such as mechanical properties, elongation and rupture toughness by homogenizing an Al alloy contg. specified alloying elements followed by hot rolling, cold rolling to a desired thickness and softening by rapid cooling.
CONSTITUTION: An Al alloy a contg. 5.1W8.1% Zn, 1.8W3.4% Mg. 1.2W2.6% Cu, <0.2% Ti and 0.18W0.35% Cr and/or 0.05W0.25% Zr is homogenized at 400W490°C, hot rolled at 350W470°C, and cold rolled to a predetermined thickness at ≥20% reduction ratio to form a structure having ≤100μm grain size. Softening is then carried out by rapid heating to 320W500°C at ≥11°C/min average temp. rising rate. When the cooling rate at this time is ≥30°C/hr, the softened material is reheated to 200W500°C, and when the reheating temp. is 200W350°C and 350W 500°C, the reheated material is air cooled or cooled at ≤30°C/hr rate and cooled at ≤30°C/hr rate, respectively.
COPYRIGHT: (C)1981,JPO&Japio
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16319379A JPS5687647A (en) | 1979-12-14 | 1979-12-14 | Airplane stringer material and its manufacture |
| US06/173,529 US4410370A (en) | 1979-09-29 | 1980-07-30 | Aircraft stringer material and method for producing the same |
| CA000357807A CA1173277A (en) | 1979-09-29 | 1980-08-07 | Aircraft stringer material and method for producing the same |
| AU62124/80A AU538304B2 (en) | 1979-09-29 | 1980-09-08 | Aircraft stringer material and method |
| DE8080303366T DE3070554D1 (en) | 1979-09-29 | 1980-09-25 | Method for producing aircraft stringer material |
| EP80303366A EP0030070B1 (en) | 1979-09-29 | 1980-09-25 | Method for producing aircraft stringer material |
| US06/500,200 US4569703A (en) | 1979-09-29 | 1983-06-01 | Aircraft stringer material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16319379A JPS5687647A (en) | 1979-12-14 | 1979-12-14 | Airplane stringer material and its manufacture |
Related Child Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP21679182A Division JPS58113345A (en) | 1982-12-13 | 1982-12-13 | Alloy for stringer of aircraft |
| JP21679282A Division JPS58113346A (en) | 1982-12-13 | 1982-12-13 | Alloy for stringer of airplane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5687647A true JPS5687647A (en) | 1981-07-16 |
| JPS613388B2 JPS613388B2 (en) | 1986-01-31 |
Family
ID=15769030
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16319379A Granted JPS5687647A (en) | 1979-09-29 | 1979-12-14 | Airplane stringer material and its manufacture |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5687647A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58181851A (en) * | 1982-04-06 | 1983-10-24 | Kobe Steel Ltd | Preparation of al-zn-mg-cu base alloy material having uniform moldability |
| JPS6333539A (en) * | 1986-07-24 | 1988-02-13 | ソシエテ・メタル−ルジク・ドウ・ジエルザ | Al alloy for pressure hollow body |
| JPH08283892A (en) * | 1995-04-14 | 1996-10-29 | Kobe Steel Ltd | Heat treated type al alloy excellent in fracture toughness, fatigue characteristic, and formability |
| JP2010179363A (en) * | 2009-01-08 | 2010-08-19 | Nippon Light Metal Co Ltd | Aluminum alloy ingot and method for producing the same |
| JP2012214905A (en) * | 2003-04-10 | 2012-11-08 | Aleris Aluminum Koblenz Gmbh | Al-Zn-Mg-Cu ALLOY |
| JP2014037557A (en) * | 2012-08-10 | 2014-02-27 | Nippon Light Metal Co Ltd | Aluminum-zinc based alloy extrusion material and method for producing teh same |
| JP2018090839A (en) * | 2016-11-30 | 2018-06-14 | アイシン軽金属株式会社 | Extrusion material aluminium alloy, extrusion material using the same and method for manufacturing extrusion material |
| JP2022532347A (en) * | 2019-06-03 | 2022-07-14 | ノベリス・インコーポレイテッド | Ultra-high-strength aluminum alloy products and their manufacturing methods |
-
1979
- 1979-12-14 JP JP16319379A patent/JPS5687647A/en active Granted
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58181851A (en) * | 1982-04-06 | 1983-10-24 | Kobe Steel Ltd | Preparation of al-zn-mg-cu base alloy material having uniform moldability |
| JPS6333539A (en) * | 1986-07-24 | 1988-02-13 | ソシエテ・メタル−ルジク・ドウ・ジエルザ | Al alloy for pressure hollow body |
| JPH08283892A (en) * | 1995-04-14 | 1996-10-29 | Kobe Steel Ltd | Heat treated type al alloy excellent in fracture toughness, fatigue characteristic, and formability |
| US5759302A (en) * | 1995-04-14 | 1998-06-02 | Kabushiki Kaisha Kobe Seiko Sho | Heat treatable Al alloys excellent in fracture touchness, fatigue characteristic and formability |
| JP2012214905A (en) * | 2003-04-10 | 2012-11-08 | Aleris Aluminum Koblenz Gmbh | Al-Zn-Mg-Cu ALLOY |
| JP2010179363A (en) * | 2009-01-08 | 2010-08-19 | Nippon Light Metal Co Ltd | Aluminum alloy ingot and method for producing the same |
| JP2014037557A (en) * | 2012-08-10 | 2014-02-27 | Nippon Light Metal Co Ltd | Aluminum-zinc based alloy extrusion material and method for producing teh same |
| JP2018090839A (en) * | 2016-11-30 | 2018-06-14 | アイシン軽金属株式会社 | Extrusion material aluminium alloy, extrusion material using the same and method for manufacturing extrusion material |
| JP2022532347A (en) * | 2019-06-03 | 2022-07-14 | ノベリス・インコーポレイテッド | Ultra-high-strength aluminum alloy products and their manufacturing methods |
| US11746400B2 (en) | 2019-06-03 | 2023-09-05 | Novelis Inc. | Ultra-high strength aluminum alloy products and methods of making the same |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS613388B2 (en) | 1986-01-31 |
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