DE3070554D1 - Method for producing aircraft stringer material - Google Patents
Method for producing aircraft stringer materialInfo
- Publication number
- DE3070554D1 DE3070554D1 DE8080303366T DE3070554T DE3070554D1 DE 3070554 D1 DE3070554 D1 DE 3070554D1 DE 8080303366 T DE8080303366 T DE 8080303366T DE 3070554 T DE3070554 T DE 3070554T DE 3070554 D1 DE3070554 D1 DE 3070554D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft stringer
- stringer material
- producing aircraft
- producing
- stringer
- 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
- 238000004519 manufacturing process Methods 0.000 title 1
Classifications
-
- 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
- B64C1/064—Stringers; Longerons
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/12764—Next to Al-base component
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Metal Rolling (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12598979A JPS5953347B2 (ja) | 1979-09-29 | 1979-09-29 | 航空機ストリンガ−素材の製造法 |
JP16319379A JPS5687647A (en) | 1979-12-14 | 1979-12-14 | Airplane stringer material and its manufacture |
JP16569679A JPS5690949A (en) | 1979-12-21 | 1979-12-21 | Material for airplane stringer with fine crystal grain and its manufacture |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3070554D1 true DE3070554D1 (en) | 1985-05-30 |
Family
ID=27315239
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8080303366T Expired DE3070554D1 (en) | 1979-09-29 | 1980-09-25 | Method for producing aircraft stringer material |
Country Status (5)
Country | Link |
---|---|
US (1) | US4569703A (de) |
EP (1) | EP0030070B1 (de) |
AU (1) | AU538304B2 (de) |
CA (1) | CA1173277A (de) |
DE (1) | DE3070554D1 (de) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS57161045A (en) * | 1981-03-31 | 1982-10-04 | Sumitomo Light Metal Ind Ltd | Fine-grain high-strength aluminum alloy material and its manufacture |
JPS619561A (ja) * | 1984-06-25 | 1986-01-17 | Mitsubishi Alum Co Ltd | 熱間成形性の優れたAl合金板の製造法 |
US4693747A (en) * | 1985-11-18 | 1987-09-15 | Aluminum Company Of America | Alloy having improved fatigue crack growth resistance |
FR2601967B1 (fr) * | 1986-07-24 | 1992-04-03 | Cerzat Ste Metallurg | Alliage a base d'al pour corps creux sous pression. |
US5186235A (en) * | 1990-10-31 | 1993-02-16 | Reynolds Metals Company | Homogenization of aluminum coil |
US5260142A (en) * | 1990-12-28 | 1993-11-09 | Honda Giken Kogyo Kabushiki Kaisha | Corrosion-resistant clad material made of aluminum alloys |
JP3053352B2 (ja) * | 1995-04-14 | 2000-06-19 | 株式会社神戸製鋼所 | 破壊靭性、疲労特性および成形性の優れた熱処理型Al合金 |
RU2345172C2 (ru) * | 2003-03-17 | 2009-01-27 | Корус Алюминиум Вальцпродукте Гмбх | Способ изготовления цельной монолитной алюминиевой конструкции и алюминиевое изделие, изготовленное путем механической обработки резанием из такой конструкции |
BRPI0411873B1 (pt) * | 2003-06-24 | 2016-11-22 | Alcan Rhenalu | elementos de estrutura para construção aeronáutica, fabricado a partir de pelo menos um produto trefilado, laminado ou forjado em liga de alumínio e processo de fabricação |
ATE548476T1 (de) * | 2003-12-16 | 2012-03-15 | Constellium France | Dickes bech aus al-zn-cu-mg zirkonarmen rekristallisierten legierung |
ES2393706T3 (es) * | 2003-12-16 | 2012-12-27 | Constellium France | Producto modelado en forma de chapa laminada y elemento de estructura para aeronave de aleación Al-Zn-Cu-Mg |
US10052670B2 (en) | 2015-09-11 | 2018-08-21 | Triumph Aerostructures, Llc | Stringer forming device and methods of using the same |
BR112017021490B1 (pt) * | 2015-10-30 | 2022-03-15 | Novelis Inc | Liga de alumínio, produto que compreende a liga de alumínio e método para produzir um produto de metal |
FR3071513B1 (fr) | 2017-09-26 | 2022-02-11 | Constellium Issoire | Alliages al-zn-cu-mg a haute resistance et procede de fabrication |
ES2936261T3 (es) | 2018-11-12 | 2023-03-15 | Novelis Koblenz Gmbh | Producto de aleación de aluminio de la serie 7xxx |
EP3670690A1 (de) * | 2018-12-20 | 2020-06-24 | Constellium Issoire | Al-zn-cu-mg-legierungen und deren herstellungsverfahren |
CN113302327A (zh) | 2019-01-18 | 2021-08-24 | 爱励轧制产品德国有限责任公司 | 7xxx系列铝合金产品 |
BR112021024430A2 (pt) | 2019-06-03 | 2022-01-18 | Novelis Inc | Produtos de liga de alumínio de ultra-alta resistência e métodos para fabricar os mesmos |
CN110983129B (zh) * | 2019-12-17 | 2021-02-05 | 北京科技大学 | 一种提高汽车用铝合金板材弯边性能的一体化过程调控方法 |
FR3138057A1 (fr) * | 2022-07-22 | 2024-01-26 | CONSTELLIUM VALAIS SA (AG- Ltd) | Tôles de précision en alliage d’aluminium 7XXX |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3198676A (en) * | 1964-09-24 | 1965-08-03 | Aluminum Co Of America | Thermal treatment of aluminum base alloy article |
US3231435A (en) * | 1964-11-25 | 1966-01-25 | Harvey Aluminum Inc | Method of eliminating stress corrosion cracking in copper-magnesium-zinc series aluminum alloys |
GB1247352A (en) * | 1967-12-05 | 1971-09-22 | Alcan Res & Dev | Solution heat treatment of wrought aluminium alloy articles |
US3573117A (en) * | 1968-11-21 | 1971-03-30 | Tyco Laboratories Inc | Method of improving stress corrosion resistance of aluminum alloys |
US3706606A (en) * | 1970-02-10 | 1972-12-19 | L Esercizio Dell Inst Sperimen | Thermomechanical treatment process for heat treatable aluminium alloys |
US3836405A (en) * | 1970-08-03 | 1974-09-17 | Aluminum Co Of America | Aluminum alloy product and method of making |
US3694272A (en) * | 1970-12-24 | 1972-09-26 | Kaiser Aluminium Chem Corp | Method for forming aluminum sheet |
US3743549A (en) * | 1971-02-09 | 1973-07-03 | I Esercizio Dell Istituto Sper | Thermomechanical process for improving the toughness of the high strength aluminum alloys |
US3881966A (en) * | 1971-03-04 | 1975-05-06 | Aluminum Co Of America | Method for making aluminum alloy product |
US3791880A (en) * | 1972-06-30 | 1974-02-12 | Aluminum Co Of America | Tear resistant sheet and plate and method for producing |
US3947297A (en) * | 1973-04-18 | 1976-03-30 | The United States Of America As Represented By The Secretary Of The Air Force | Treatment of aluminum alloys |
US3847681A (en) * | 1973-11-09 | 1974-11-12 | Us Army | Processes for the fabrication of 7000 series aluminum alloys |
US4092181A (en) * | 1977-04-25 | 1978-05-30 | Rockwell International Corporation | Method of imparting a fine grain structure to aluminum alloys having precipitating constituents |
FR2393070A1 (fr) * | 1977-06-02 | 1978-12-29 | Cegedur | Procede de traitement thermique de toles en alliages d'aluminium |
US4305763A (en) * | 1978-09-29 | 1981-12-15 | The Boeing Company | Method of producing an aluminum alloy product |
US4222797A (en) * | 1979-07-30 | 1980-09-16 | Rockwell International Corporation | Method of imparting a fine grain structure to aluminum alloys having precipitating constituents |
-
1980
- 1980-08-07 CA CA000357807A patent/CA1173277A/en not_active Expired
- 1980-09-08 AU AU62124/80A patent/AU538304B2/en not_active Expired
- 1980-09-25 DE DE8080303366T patent/DE3070554D1/de not_active Expired
- 1980-09-25 EP EP80303366A patent/EP0030070B1/de not_active Expired
-
1983
- 1983-06-01 US US06/500,200 patent/US4569703A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
AU6212480A (en) | 1981-04-02 |
AU538304B2 (en) | 1984-08-09 |
US4569703A (en) | 1986-02-11 |
EP0030070A1 (de) | 1981-06-10 |
EP0030070B1 (de) | 1985-04-24 |
CA1173277A (en) | 1984-08-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8339 | Ceased/non-payment of the annual fee |