Product Classification:High Temperature Alloy | ||||||||||||||||||||||
Material:GH4169 | ||||||||||||||||||||||
Corresponding Brand | ||||||||||||||||||||||
National Standard | American Standard | France Standard | ||||||||||||||||||||
GH4169(GH169) | Inconel718 | NC19FeNb | ||||||||||||||||||||
Chemical Composition | ||||||||||||||||||||||
Category | C | Cr | Ni | Co | Al | Ti | Fe | |||||||||||||||
Standard | ≤0.08 | 17.0~21.0 | 50.0~55.0 | ≤1.0 | 0.30~0.70 | 0.75~ 1.15 | The resting | |||||||||||||||
High Quality | 0.02~0.06 | 17.0~21.0 | 50.0~55.0 | ≤1.0 | 0.30~0.70 | 0.75~ 1.15 | The resting | |||||||||||||||
High Purity | 0.02~0.06 | 17.0~21.0 | 50.0~55.0 | ≤1.0 | 0.30~0.70 | 0.75~ 1.15 | The resting | |||||||||||||||
Category | Nb | B | Mg | Mn | Si | P | S | Cu | Ca | |||||||||||||
≤ | ≤ | ≤ | ≤ | ≤ | ≤ | ≤ | ≤ | |||||||||||||||
Standard | 4.75~5.50 | 0.006 | 0.01 | 0.35 | 0.35 | 0.015 | 0.015 | 0.30 | 0.01 | |||||||||||||
High Quality | 5.00~5.50 | 0.006 | 0.01 | 0.35 | 0.35 | 0.015 | 0.015 | 0.30 | 0.01 | |||||||||||||
High Purity | 5.00~5.50 | 0.006 | 0.005 | 0.35 | 0.35 | 0.015 | 0.015 | 0.30 | 0.005 | |||||||||||||
Category | Bi | Sn | Pb | Ag | Se | Te | Tl | N | O | |||||||||||||
≤ | ≤ | ≤ | ≤ | ≤ | ≤ | ≤ | ≤ | ≤ | ||||||||||||||
Standard | 0.0005 | 0.0005 | 0.0003 | |||||||||||||||||||
High Quality | 0.001 | 0.005 | 0.001 | 0.001 | 0.0003 | 0.01 | 0.01 | |||||||||||||||
High Purity | 0.00003 | 0.005 | 0.001 | 0.001 | 0.0003 | 0.00005 | 0.0001 | 0.005 | ||||||||||||||
Physical and Mechanical Properties | ||||||||||||||||||||||
1) Melting temperature range: melting point 1260~1320ºC , thermal conductivity as follows: | ||||||||||||||||||||||
θ/ºC | 11 | 100 | 200 | 300 | 400 | 500 | 600 | 700 | 800 | 900 | 1000 | |||||||||||
λ/(W/(m·ºC)) | 13.4 | 14.7 | 15.7 | 17.8 | 18.3 | 19.6 | 21.2 | 22.8 | 23.6 | 27.6 | 30.4 | |||||||||||
2) Density ρ=8.24g/cm3, linear expansion coefficient is as follows: | ||||||||||||||||||||||
θ/ºC | 20~100 | 20~200 | 20~300 | 20~400 | 20~500 | 20~600 | 20~700 | 20~800 | 20~900 | 20~1000 | ||||||||||||
α/10-6ºC-1 | 11.8 | 13 | 13.5 | 14.1 | 14.4 | 14.8 | 15.4 | 17 | 18.4 | 18.7 | ||||||||||||
Application | ||||||||||||||||||||||
GH4141 is applied to the manufacturing of various stationary and rotating components in aviation and aerospace engines, such as discs, rings, casings, shafts, blades, fasteners, elastic components, gas ducts, sealing components, and welded structural components. |