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Volume 01 - Properties and Selection Irons, Steels, and High-Performance Alloys Part 9 pptx

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Tiêu đề Volume 01 - Properties and Selection Irons, Steels, and High-Performance Alloys Part 9
Trường học Unknown University
Chuyên ngành Materials Science and Engineering
Thể loại lecture presentation
Năm xuất bản Unknown
Thành phố Unknown City
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Hardenability Curves for Nickel-Chromium-Molybdenum 43xx Alloy Steels Figure 35... Hardenability Curves for Nickel-Molybdenum 46xx Alloy Steels Figure 38... Hardenability Curves for Nick

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Hardenability Curves for Nickel-Chromium-Molybdenum (43xx) Alloy Steels

Figure 35 SAE/AISI 4320H UNS H43200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

Trang 2

Figure 36 SAE/AISI 4340H UNS H43400 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

Trang 3

Figure 37 SAE/AISI E4340H UNS H43406 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Nickel-Molybdenum (46xx) Alloy Steels

Figure 38 SAE/AISI 4620H UNS H46200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

Trang 5

Figure 39 SAE/AISI 4626H UNS H46260 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (47xx) Alloy Steels

Figure 40 SAE/AISI 4718H UNS H47180 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 41 SAE/AISI 4720H UNS H47200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Hardenability Curves for Nickel-Molybdenum (48xx) Alloy Steels

Figure 42 SAE/AISI 4815H UNS H48150 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 845 °C (1550

°F)

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Figure 43 SAE/AISI 4817H UNS H48170 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 845 °C (1550

°F)

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Figure 44 SAE/AISI 4820H UNS H48200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Chromium (50xx) Alloy Steels

Figure 45 SAE/AISI 50B40H UNS H50401 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 46 SAE/AISI 50B44H UNS H50441 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 47 SAE/AISI 5046H UNS H50460 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 48 SAE/AISI 50B46H UNS H50461 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 49 SAE/AISI 50B50H UNS H50501 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 50 SAE/AISI 50B60H UNS H50601 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Chromium (51xx) Alloy Steels

Figure 51 SAE/AISI 5120H UNS H51200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 52 SAE/AISI 5130H UNS H51300 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Figure 53 SAE/AISI 5132H UNS H51320 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1650 °F) Austenitize: 845 °C (1600

°F)

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Figure 54 SAE/AISI 5135H UNS H51350 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1650 °F) Austenitize: 845 °C (1600

°F)

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Figure 55 SAE/AISI 5140H UNS H51400 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 56 SAE/AISI 5147H UNS H51470 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 57 SAE/AISI 5150H UNS H51500 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 58 SAE/AISI 5155H UNS H51550 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 59 SAE/AISI 5160H UNS H51600 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 60 SAE/AISI 51B60H UNS H51601 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Chromium-Vanadium (61xx) Alloy Steels

Figure 61 SAE/AISI 6118H UNS H61180 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 62 SAE/AISI 6150H UNS H61500 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (81xx) Alloy Steels

Figure 63 SAE/AISI 81B45H UNS H81451 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (86xx) Alloy Steels

Figure 64 SAE/AISI 8617H UNS H86170 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

Trang 31

Figure 65 SAE/AISI 8620H UNS H86200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

Trang 32

Figure 66 SAE/AISI 8622H UNS H86220 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 67 SAE/AISI 8625H UNS H86250 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Figure 68 SAE/AISI 8627H UNS H86270 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Figure 69 SAE/AISI 8630H UNS H86300 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Figure 70 SAE/AISI 86B30H UNS H86301 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

Trang 37

Figure 71 SAE/AISI 8637H UNS H86370 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

Trang 38

Figure 72 SAE/AISI 8640H UNS H86400 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 73 SAE/AISI 8642H UNS H86420 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 74 SAE/AISI 8645H UNS H86450 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 75 SAE/AISI 86B45H UNS H86451 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 76 SAE/AISI 8650H UNS H86500 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 77 SAE/AISI 8655H UNS H86550 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Figure 78 SAE/AISI 8660H UNS H86600 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (87xx) Alloy Steels

Figure 79 SAE/AISI 8720H UNS H87200 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 80 SAE/AISI 8740H UNS H87400 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 870 °C (1600 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (88xx) Alloy Steels

Figure 81 SAE/AISI 8822H UNS H88220 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Hardenability Curves for Silicon-Manganese (92xx) Alloy Steels

Figure 82 SAE/AISI 9260H UNS H92600 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (93xx) Alloy Steels

Figure 83 SAE/AISI 9310H UNS H93100 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 845 °C (1550

°F)

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Hardenability Curves for Nickel-Chromium-Molybdenum (94xx) Alloy Steels

Figure 84 SAE/AISI 94B15H UNS H94151 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 85 SAE/AISI 94B17H UNS H94171 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C (1700 °F) Austenitize: 925 °C (1700

°F)

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Figure 86 SAE/AISI 94B30H UNS H94301 Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 900 °C (1650 °F) Austenitize: 870 °C (1600

°F)

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Sheet Formability of Steels

Revised by W.G Granzow, Armco, Inc., Research & Technology

Introduction

STEEL SHEET is widely used for industrial and consumer products, partly because it is relatively strong, easily joined, and readily available at moderate cost However, it is not these factors, but the formability of steel sheets that is primarily responsible for its wide use The term formability is commonly used to described the ability of a steel to maintain its structural integrity while being plastically deformed into various shapes However, not all shapes require the same forming characteristics, and a steel that has excellent formability in one application may exhibit poor formability in another application In practice, therefore, formability must be optimized by selecting a grade of steel that has the forming characteristics needed to make the required shape

These forming characteristics are normally estimated from an analysis of the mechanical properties of steel, which are determined by uniaxial tensile tests Although this type of test does not simulate any commercial forming operations, the test results have been universally used for many years to evaluate formability, and some understanding of them is

essential to the understanding of sheet steel formability Sheet metal forming methods are described in detail in Forming

and Forging, Volume 14 of ASM Handbook

Examples of formed parts that require different forming characteristics in the steel are shown in Fig 1 Part A was formed

by drawing; that is, all the metal that was required to form the part from a flat blank came from the flanges This shape

requires that the steel have a high plastic-strain ratio, or r value, which determines the resistance of steel sheet to thinning

during forming operations Part C was formed by stretching; the flange on the blank was clamped during forming, and all

of the metal that was required to form the part came from reducing the thickness of the metal This type of part requires

good ductility in the steel However, the r value should be low, because high r values can cause failures of stretched parts

Part B has failed in plane strain, which is a type of stretching Parts that develop this strain condition, such as automotive panels, require good ductility

Fig 1 Parts that required different forming characteristics in the steel sheet

This article discusses the mechanical properties and formability of steel sheet, the use of circle grid analysis to identify the properties of complicated shapes, and various simulative forming tests It covers the effects of steel composition, steelmaking practices, and metallic coatings, as well as the correlation between microstructure and formability A guide to the selection of steel sheet is also included

Sheet Formability of Steels

Revised by W.G Granzow, Armco, Inc., Research & Technology

Mechanical Properties and Formability

Trang 54

The mechanical properties of steel sheet that influence its forming characteristics, either directly or indirectly, can be measured by uniaxial tension testing, such as that described in ASTM E 8 The tensile test results of particular interest include the yield strength, ultimate tensile strength, total elongation, uniform elongation, yield point elongation, plastic-strain ratio, planar anisotropy, and the strain-hardening exponent Uniaxial tensile tests may be made with specimens obtained from longitudinal, diagonal, transverse, or other orientations relative to the rolling direction Typical mechanical properties for common grades of hot-rolled and cold-rolled steel sheets are given in Tables 1 and 2

Table 1 Typical mechanical properties of hot-rolled steel sheet

Yield strength

Tensile strength Type or quality Special feature

MPa ksi MPa ksi

Elongation in

50

mm (2 in.), %

Hardness, HRB

hardening

Strain-exponent, n

strain

Table 2 Typical mechanical properties of cold-rolled steel sheet

Yield strength

Tensile strength Type or quality Special feature

MPa ksi MPa ksi

hardening

Strain-exponent, n

strain

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