Vorsicht!

In Ihrem Browser ist die Javascript-Aktivierung nicht erlaubt. Einige Funktionen mögen nicht richtig funktionieren. Für vollständige Funktionalität des Internet-Geschäfts empfehlen wir Javascript zu aktivieren. Siehe hier Instruktion, wie man im Ihren Web-Browser JavaScript aktiviert.

Angezeigte Währung: €

Preisanzeige: ohne MWS

Ergänzende Informationen

ASTM B575-17

Standard Specification for Low-Carbon Nickel-Chromium-Molybdenum, Low-Carbon Nickel-Chromium-Molybdenum-Copper, Low-Carbon Nickel-Chromium-Molybdenum-Tantalum, Low-Carbon Nickel-Chromium-Molybdenum-Tungsten, and Low-Carbon Nickel-Molybdenum-Chromium Alloy Plate, Sheet, and Strip

Name übersetzen

NORM herausgegeben am 1.6.2017

Sprache
Realisierung	PDF - sofortiges Download - 61.80 € Gedruckt - 61.80 €
Zugänglichkeit	AUF LAGER
Preis	61.80 € ohne MWS
61.80 €

Informationen über die Norm:

Bezeichnung normen: ASTM B575-17
Anmerkung: UNGÜLTIG
Ausgabedatum normen: 1.6.2017
SKU: NS-686091
Zahl der Seiten: 4
Gewicht ca.: 12 g (0.03 Pfund)
Land: Amerikanische technische Norm
Kategorie: Technische Normen ASTM

Drucken

Einem Bekannten abschicken

Anfrage

Kategorie - ähnliche Normen:

Nickel and chromium products

Die Annotation des Normtextes ASTM B575-17 :

Keywords:
N06022, N06035, N06044, N06058, N06059, N06200, N06210, N10362, N06455, N06686, N10276, plate, sheet, strip,, ICS Number Code 77.150.40 (Nickel and chromium products)

Ergänzende Informationen

1. Scope

1.1 This specification2 covers plate, sheet, and strip of low-carbon nickel-chromium-molybdenum alloys (UNS N10276, N06022, N06455, N06035, N06044, UNS N06058, UNS N06059),3 low-carbon nickel-chromium-molybdenum-copper alloy (UNS N06200), low-carbon nickel-molybdenum-chromium (UNS N10362), low-carbon nickel-chromium-molybdenum-tantalum alloy (UNS N06210), and low-carbon nickel-chromium-molybdenum-tungsten alloy (UNS N06686) as shown in Table 1, for use in general corrosive service.

TABLE 1 Chemical Requirements

Element

Composition Limits, %

Alloy
N06035

Alloy
N06044

Alloy
N10276

Alloy
N06022

Alloy
N06455

Alloy
N06059

Alloy
N06058

Alloy
N06200

Alloy
N06210

Alloy
N10362

Alloy
N06686

Molybdenum

7.60–9.00

0.80-1.20

15.0–17.0

12.5–14.5

14.0–17.0

15.0–16.5

18.5–21.0

15.0–17.0

18.0–20.0

21.5–23.0

15.0-17.0

Chromium

32.25–34.25

43.5-45.3

14.5–16.5

20.0–22.5

14.0–18.0

22.0–24.0

20.0–23.0

22.0–24.0

18.0–20.0

13.8–15.6

19.0-23.0

Iron

2.00 max

0.3 max

4.0–7.0

2.0–6.0

3.0 max

1.5, max

3.0 max

1.0 max

1.25 max

5.0 max

Tungsten

0.60 max

...

3.0–4.5

2.5–3.5

...

0.3 max

...

3.0-4.4

Cobalt, max

1.00

...

2.5

2.0

0.3

2.0 max

1.0

...

Carbon, max

0.050

0.02

0.010

0.015

0.010

0.015

0.010

Silicon, max

0.60

0.20

0.08

0.10

0.08

Manganese, max

0.50

0.07-0.30

1.0

0.50

1.0

0.5

0.50

0.5

0.60

0.75

Vanadium, max

0.20

...

0.35

...

0.35

...

Phosphorus, max

0.030

0.020

0.04

0.02

0.04

0.015

0.025

0.02

0.025

0.04

Sulfur, max

0.015

0.020

0.03

0.02

0.03

0.010

0.02

0.010

0.02

Titanium

...

0.10-0.30

...

0.7 max

...

0.02-0.25

Nickel

remainder^A

Bal

remainder^A

Bal

remainder^A

Aluminum

0.40 max

0.30 max

...

0.1–0.4

0.40 max

0.50 max

...

0.50 max

...

Copper

0.30 max

...

0.50 max

1.3–1.9

...

Tantalum

...

1.5–2.2

...

Nitrogen

...

0.02–0.15

TABLE 2 Mechanical Property Requirements

Alloy

Tensile Strength, min, psi (MPa)

Yield Strength (0.2 % Offset), min, psi
(MPa)

Elongation in 2 in.
(50.8 mm) or 4D^A
min, %

Rockwell Hardness,^B
max

N10276

100 000 (690)

41 000 (283)

100 HRB

N06022

100 000 (690)

45 000 (310)

100 HRB

N06455

100 000 (690)

40 000 (276)

100 HRB

N06035

85 000 (586)

35 000 (241)

100 HRB

N06044

100 000 (690)

45 000 (310)

100 HRB

N06058

110 000 (760)

52 000 (360)

100 HRB

N06059

100 000 (690)

45 000 (310)

100 HRB

N06200

100 000 (690)

45 000 (310)

100 HRB

N10362

105 000 (725)

45 000 (310)

100 HRB

N06686

100 000 (690)

45 000 (310)

100 HRB

N06210

100 000 (690)

45 000 (310)

100 HRB

1.2 The following products are covered under this specification:

1.2.1 Sheet and Strip—Hot or cold rolled, solution annealed, and descaled unless solution anneal is performed in an atmosphere yielding a bright finish.

1.2.2 Plate—Hot or cold rolled, solution annealed, and descaled.

1.3 The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.

1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to become familiar with all hazards including those identified in the appropriate Safety Data Sheet (SDS) for this product/material as provided by the manufacturer, to establish appropriate safety and health practices, and determine the applicability of regulatory limitations prior to use.

1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

2. Referenced Documents

B906-22	Standard Specification for General Requirements for Flat-Rolled Nickel and Nickel Alloys Plate, Sheet, and Strip
E140-12B(2019)e1	Standard Hardness Conversion Tables for Metals Relationship Among Brinell Hardness, Vickers Hardness, Rockwell Hardness, Superficial Hardness, Knoop Hardness, Scleroscope Hardness, and Leeb Hardness (Includes all amendments and changes 5/7/2019).
E527-23	Standard Practice for Numbering Metals and Alloys in the Unified Numbering System (UNS)
E112-13(2021)	Standard Test Methods for Determining Average Grain Size

Empfehlungen:

EEviZak – alle Gesetze einschließlich ihrer Evidenz in einer Stelle

Bereitstellung von aktuellen Informationen über legislative Vorschriften in der Sammlung der Gesetze bis zum Jahr 1945.
Aktualisierung 2x pro Monat!

Brauchen Sie mehr Informationen? Sehen Sie sich diese Seite an.