청두 진춘 금속 재료 유한 공사

구형 금속 분말 GH5188 코발트 기반 고온 합금 분말

제품 캐릭터 : 제품 캐릭터

GH5188 is a solid solution strengthened cobalt based high-temperature alloy, which is strengthened by adding 14% tungsten to give the alloy excellent high-temperature thermal strength. At the same time, adding a high content of chromium and trace amounts of La gives the alloy good high-temperature oxidation resistance. Compared to nickel based high-temperature alloys, GH5188 has more good creep resistance, thermal corrosion resistance, fatigue resistance, and high temperature strength. GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates.

브랜드 이름 진춘
원산지 중국
제품 이름 GH5188 powder
애플리케이션 Aircraft engines, etc.
모양 파우더
색상 Metal gray
크기 15~53μm
표준 GB/T 19001-2016/ISO9001: 2015
순도  Ni: 20-24%, Cr:20-24%, W:13-16%, Co: Bal.
재료 Ni, Cr, W, Co
포장 진공 포장
제품 캐릭터 GH5188 is a solid solution strengthened cobalt based high-temperature alloy, which is strengthened by adding 14% tungsten to give the alloy excellent high-temperature thermal strength. At the same time, adding a high content of chromium and trace amounts of La gives the alloy good high-temperature oxidation resistance. Compared to nickel based high-temperature alloys, GH5188 has more good creep resistance, thermal corrosion resistance, fatigue resistance, and high temperature strength. GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates.   2.사양 GH5188 powder
화학 성분(중량 %)
요소 C Cr Ni Co La W Si Fe
표준 0.05~0.15 20.0~24.0 20.0~24.0 Bal. 0.03~0.12 13.0~16.0 0.2~0.5 ≤3.0
typical 0.11 22.33 22.17 Bal. 0.06 14.91 0.44 0.49
요소 Mn P S Cu B O N
표준 ≤1.25 ≤0.02 ≤0.015 ≤0.070 ≤0.015 ≤0.030 ≤0.030
typical 0.26 0.006 0.006 0.021 0.0092 0.017 0.01
 
GH5188 15~53μm 입자 크기 분포 유량 (50g의 경우 초) 겉보기 밀도(g/cm3) 탭 밀도(g/cm3)
D10 D50 D90
표준 15~25 30~40 50~60 ≤25 ≥4.55 ≥5.30
typical 22.2μm 35.6μm 55.0μm 17 4.57 5.33
  3. 분말 SEM 형태 사진 프로덕션 및 테스트 사진:   4.애플리케이션
  • GH5188 has excellent formability, welding and other process properties, making it suitable for manufacturing parts for aircraft engines that require high strength below 980 ℃ and anti-oxidation below 1000 ℃. In the 1980s, GH5188 alloy was applied to components such as vortex plates and flame deflectors in turboshaft eight aircraft engines. Currently, some aircraft engines use GH5188 alloy sheets to prepare high-temperature components such as combustion chamber walls, outer walls, and sealing plates.

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