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Exploratory Development for Design Data on Structural Aluminum Alloys in Representative Aircraft Environments.

机译：代表性飞机环境中结构铝合金设计数据的探索性发展。

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摘要

The mechanical properties, fracture toughness, fatigue, fatigue-crack growth rates in three environments and corrosion characteristics of 10 lots each of 2048-T851, 7050-T7351 and 7475-T7351 plate and 2219-T852 hand forgings have been evaluated. Data for establishing MIL-HDBK-5 values, including modulus of elasticity and stress-strain are presented.

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作者
brownhill, d. j. davies, r. e.;
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年度 1977
页码 1-196
总页数 196
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aluminum alloys; Airframes; Structural engineering; Fracture(Mechanics); Fatigue(Mechanics); Crack propagation; Stress corrosion; Forging; Modulus of elasticity; Stress strain relations; Yield strength; Aerospace systems; Exfoliation; Aluminum alloy 2048; Aluminum alloy 7050; Aluminum alloy 7475; Aluminum alloy 2219;

机译：铝合金;机身;结构工程;断裂（力学）;疲劳（力学）;裂纹扩展;应力腐蚀;锻造;弹性模量;应力应变关系;屈服强度;航空航天系统;剥落;铝合金2048;铝合金7050;铝合金7475;铝合金2219;

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专利

1. Backward Extrusion of Aluminum Alloy Sections Used in Aircraft Structural Components / Wyciskanie Przeciwbie?ne Kszta?towników Ze Stopów Aluminium Stosowanych Na Elementy Konstrukcji Lotniczych [J] . B. Paw?owska, R.E. ?liwa Archives of Metallurgy and Materials . 2016,第4期

机译：用于飞机结构部件的铝合金型材的向后挤压。
2. Backward Extrusion of Aluminum Alloy Sections Used in Aircraft Structural Components / Wyciskanie Przeciwbie?ne Kszta?towników Ze Stopów Aluminium Stosowanych Na Elementy Konstrukcji Lotniczych [J] . B. Paw?owska, R.E. ?liwa Archives of Metallurgy and Materials . 2016,第4期

机译：用于飞机结构部件的铝合金型材的向后挤压。
3. BACKWARD EXTRUSION OF ALUMINUM ALLOY SECTIONS USED IN AIRCRAFT STRUCTURAL COMPONENTS [J] . Pawlowska B., Sliwa R. E. Archives of Metallurgy and Materials . 2015,第4aPta1期

机译：用于飞机结构组件的铝合金型材的向后挤压
4. Application of Design Strategies and Casting Optimization Techniques for the Development of a Heavy Specialty Truck Structural Suspension Component made from Aluminum Alloy A206 [C] . Winston Sequeira, Vadim Pikhovich, David Weiss American Foundry Society International Conference on High Integrity Light Metal Castings; 20051031-1101; Indianapolis,IN(US) . 2005

机译：设计策略和铸造优化技术在开发重型A206铝合金特种卡车结构悬架零件中的应用
5. Effects of frequency and amplitude variations of superimposed minor loading sequences on the corrosion fatigue behavior of aircraft structural aluminum alloys. [D] . Paulson, Andrew Danton. 1993

机译：叠加的次要加载序列的频率和幅度变化对飞机结构铝合金腐蚀疲劳行为的影响。
6. Crashworthiness Optimization Design of Aluminum Alloy Thin-Walled Triangle Column Based on Bioinspired Strategy [O] . Kangjie Li, Yixiong Feng, Yicong Gao, 2020

机译：基于生物启发策略的铝合金薄壁三角柱耐撞性优化设计
7. Backward Extrusion of Aluminum Alloy Sections Used in Aircraft Structural Components / Wyciskanie Przeciwbieżne Kształtowników Ze Stopów Aluminium Stosowanych Na Elementy Konstrukcji Lotniczych [O] . Pawłowska B., Śliwa R.E. 2015

机译：用于飞机结构件的铝合金型材的向后挤压/ WyciskanieprzeciwbieżneKształtownikówZestopówaluminiumstosowanych Na Elementy Konstrukcji Lotniczych
8. CUMULATIVE FATIGUE DAMAGE OF AIRCRAFT STRUCTURAL MATERIALS Part 2:2024 and 7075 Aluminum Alloy Additional Data and Evaluation [R] . ALFRED M. FREUDENTHAL, ROBERT A. HELLER 1956

机译：飞机结构材料的累积疲劳损伤第2部分：2024和7075铝合金附加数据和评估

Exploratory Development for Design Data on Structural Aluminum Alloys in Representative Aircraft Environments.

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