• 분석과학
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• 제7권4호
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• pp.527-540
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• 1994

본 연구는 질소이온 주입시킨 7050A1 합금의 표면 미세구조 변화에 대하여 살펴보았다. 이온 주입은 이온을 가속시켜서 물리적으로 모재의 표면에 주입시키는 표면처리의 한 방법으로서, 본 연구에서는 가속 에너지를 100KeV로 하고 전류밀도는 $23.1{\mu}A/cm^2$, 주입량은 $5{\times}10^{15}ions/cm^2$, $5{\times}10^{17}ions/cm^2$과, $8{\times}10^{17}ions/cm^2$로 질소이온을 주입하였다. 이온 주입층은 EPMA, AES, XPS, TEM 등으로 분석하였으며, 그 결과를 computer simulation을 통하여 비교하여 보았다. 질소이온 주입시킨 7050A1 합금은 극 표면에서부터 약 $4000{\AA}$ 사이에서 AlN이 Gaussian 분포를 지니고 있었으며, 일정 깊이에서 이온의 주입에 의해 충격을 받은 영역을 관찰할 수 있었고 이러한 표면의 변화들은 미소경도에 영향을 미치게 되어 저하중에서 경도값의 상승을 야기했다.

• 열처리공학회지
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• 제9권2호
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• pp.139-146
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• 1996

The aero-industry is union industry which includes a research development type, a knowledge accumulation type and a developed country type. The aero-industry of Korea is in semi-developed type stage but departed later than that of other country such as Taiwan, Indonesia etc. Therefore, the necessity of domestic airplane material is required. This study on 7050Al extruded alloy aims to suggest an adequate heat treatment conditions of T73, T74 and T76. The results of this study show that; 1. The optimum conditions of T7x heat treatment in extruded 7050Al alloy show this; $$T73:121^{\circ}C{\times}7hr+177^{\circ}C{\times}14hr$$. $$T74:121^{\circ}C{\times}7hr+177^{\circ}C{\times}10hr$$. $$T76:121^{\circ}C{\times}7hr+163^{\circ}C{\times}21hr$$. 2. The 2nd step aging heat treatment such as T73, T74 and T76 etc. is efective in 7050Al alloy but the variation otf microstructure and mechanical property with dispersive inclusions produced for extrusion process causes some troubles. Accordingly, in order to produce a good 7050Al alloy, a careful attention is needed in manufacturing process.

• 대한기계학회논문집A
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• 제31권2호
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• pp.197-204
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• 2007

Fretting is a contact damage process that occurs between two contact surfaces. Fretting fatigue reduces fatigue strength of the material due to low amplitude oscillatory sliding and changes in the contact surfaces of strongly connected machine and structure such as bolt, key, pin, fixed rivet and connected shaft, which have relative slip of repeatedly extreme low frequency amplitude. In this research, the fretting fatigue behavior of 2024-T3511 and 7050-T7451 aluminum alloys used mainly in aircraft and automobile industry were experimentally estimated. Based on this experimental wort the following results were obtained: (1) A significant decrease of fatigue lift was observed in the fretting fatigue compared to the plain fatigue. The fatigue limit of 2024-T3511 aluminum alloy decreased about 59% while 7050-T7451 aluminum alloy decreased about 75%. (2) In 7050-T7451 specimen using ATSI4030 contact pad, crack was initiated more early stage than using 2024-T3511 contact pad. (3) In all specimens, oblique cracks were initiated at contact edge. (4) Tire tracks and rubbed scars were observed in the oblique crack region of fracture surface.

• 한국재료학회지
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• 제10권7호
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• pp.493-498
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• 2000

7050 AI합금을 RRA 처리하였을 때 경도, 전기전도도 및 미세조직의 변화를 조사하였다. 120도씨에서 24시간 동안 1차 시효처리한 후 175도씨에서 2차 퇴화처리하였을 때 경도값의 변화는 초기에 감소하다가 피크 경도를 보인 다음 다시 감소하였으며, 3차 재시효처리재가 2차 시효처리재 보다 큰 경도값을 나타내었다. 2차 퇴화처리시 초기 경도 감소는 T6의 주 강화상인 GP zone의 부분적인 분해에 의한 것이며, 3차 재시효 처리하였을 때 강화상은 GP zone과 파이상이었다. 120도씨에서 24시간 동안 1차 시효처리한 후 175도씨에서 2차 퇴화처리하였을 때 전기전도도 변화는 퇴화 쵤부터 연속적으로 증가혀였으며, 3차 재시효처리에 의해 2차 퇴화처리시 보다 %IACS가 0.5 ~ 2.7 증가하였다. 3단시효에 의해 T6정도의 강도를 유지하면서 38%IACS값 이상의 전기전도도를 얻을 수 있는 최적 퇴화처리 조건은 $175^{\circ}C$ 50분이었다. 이는 퇴화처리 경도곡선의 극소점 또는 극대점과 무관하며 오히려 약간 과시효 조건이다.

• 한국기계가공학회지
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• 제9권1호
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• pp.25-34
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• 2010

Fretting damage reduces fatigue life of the material due to low amplitude cyclic sliding and changes in the contact surfaces of strongly connected machine and structures such as bolt, key, fixed rivet and connected shaft, which have relative slip of repeatedly very low frequency amplitude. In this study, the fretting fatigue behavior of 7050-T7451 aluminum alloys used mainly in aircraft and automobile industry were evaluated. The plain fatigue test and fretting fatigue test under cyclic bending load carried out commercial bending fatigue tester and specially devised equipments to cause fretting damage. From these experimental work, the following results obtained: (1) The plain fatigue limit for stress ratio R=-l was about 151MPa. (2) In case of fretting fatigue, fatigue limit for stress ratio R=-l about 72MPa, the fatigue limit for R=0 about 81MPa, and the fatigue limit for R=0.3 about 93MPa. (3) The fatigue limit reduction rates by the fretting damage were about 52%(R=-1), 46%(R=0) and 38%(R=0.3) respectively. (4) The fatigue limit reduction rate decreased with stress ratio increase. In fretting bending test, as stress ratio increased, occurrence of initial oblique crack by fretting decreased or phased out, so that fracture surfaces were formed by plain fatigue crack occurrence, and such tendency was notable as stress amplitude increased. (5) Tire tracks and rubbed scars were observed in the fracture surface and contacted surface.

• 열처리공학회지
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• 제6권1호
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• pp.9-16
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• 1993

To investigate the properties of diffusion bonding of 7050 Al alloy, the diffusion bonding joints have been produced in self-made diffusion bonding hot-press which admits a defined application of the bonding pressure during the heating phase and also rapid cooling after the bonding process with various bonding condition. The strength of the bond increases with increasing the bonding time and temperature. Shear test at toom temperature showed that high strength up to 70% that of parent metal (320 MPa), 220 MPa for the specimen bonded 14 hr at $560^{\circ}C$, with 3 MPa. In this case, however, there is large deformation more than 20% reduction in thickness. The results were correlated with joint characteristics found by optical microstructure and by fractography by SEM. When the strengths of the bonds are more than 50% that of parent metal, a great deal of dimples stretched along the direction of shear stress are observed over the fractured surface of the bond. On the microstructure of the bond line, initial mophology of the bond line disapeared for the grain boundary migration with increasing the bonding time.