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Nickel-titanium alloy service temperature

Nickel-titanium alloy service temperature, Total:67 items.

In the international standard classification, Nickel-titanium alloy service temperature involves: Powder metallurgy, Products of non-ferrous metals, Non-ferrous metals, Paints and varnishes, Medical equipment, Materials for aerospace construction, Fasteners for aerospace construction, Corrosion of metals, Construction of waterways and ports.

Professional Standard - Non-ferrous Metal, Nickel-titanium alloy service temperature

YS/T 970-2014 Phase change temperature measuring method for nickel-titanium shape memory alloys

国家市场监督管理总局、中国国家标准化管理委员会, Nickel-titanium alloy service temperature

GB/T 39151-2020 Nickel beryllium titanium alloy strip for high temperature elastic component

American Society for Testing and Materials (ASTM), Nickel-titanium alloy service temperature

ASTM F2004-17 Standard Test Method for Transformation Temperature of Nickel-Titanium Alloys by Thermal Analysis
ASTM F2004-16 Standard Test Method for Transformation Temperature of Nickel-Titanium Alloys by Thermal Analysis
ASTM D3450-00(2010) Standard Test Method for Washability Properties of Interior Architectural Coatings
ASTM F2004-05 Standard Test Method for Transformation Temperature of Nickel-Titanium Alloys by Thermal Analysis
ASTM F2004-00 Standard Test Method for Transformation Temperature of Nickel-Titanium Alloys by Thermal Analysis
ASTM F2004-03 Standard Test Method for Transformation Temperature of Nickel-Titanium Alloys by Thermal Analysis
ASTM F2004-05(2010) Standard Test Method for Transformation Temperature of Nickel-Titanium Alloys by Thermal Analysis
ASTM F2082/F2082M-23 Standard Test Method for Determination of Transformation Temperature of Nickel-Titanium Shape Memory Alloys by Bend and Free Recovery
ASTM F2082-01 Standard Test Method for Determination of Transformation Temperature of Nickel-Titanium Shape Memory Alloys by Bend and Free Recovery
ASTM F2082-15 Standard Test Method for Determination of Transformation Temperature of Nickel-Titanium Shape Memory Alloys by Bend and Free Recovery
ASTM F2082/F2082M-16 Standard Test Method for Determination of Transformation Temperature of Nickel-Titanium Shape Memory Alloys by Bend and Free Recovery
ASTM F2082-03 Standard Test Method for Determination of Transformation Temperature of Nickel-Titanium Shape Memory Alloys by Bend and Free Recovery
ASTM F2082-06 Standard Test Method for Determination of Transformation Temperature of Nickel-Titanium Shape Memory Alloys by Bend and Free Recovery
ASTM E1938-13 Standard Test Method for Determination of Titanium in Nickel Alloys by Diantipyrylmethane Spectrophotometry
ASTM B670-07 Standard Specification for Precipitation-Hardening Nickel Alloy (UNS N07718) Plate, Sheet, and Strip for High-Temperature Service
ASTM B637-12e1 Standard Specification for Precipitation-Hardening and Cold Worked Nickel Alloy Bars, Forgings, and Forging Stock for Moderate or High Temperature Service
ASTM A690/A690M-05 Standard Specification for High-Strength Low-Alloy Nickel, Copper, Phosphorus Steel H-Piles and Sheet Piling with Atmospheric Corrosion Resistance for Use in Marine Environments

RU-GOST R, Nickel-titanium alloy service temperature

GOST 1791-2014 Nickel and copper-nickel alloys wire for extension leads for thermoelectric temperature transducers. Specifications
GOST R 55917-2013 Nickel and copper-nickel alloys wire for extension leads for thermoelectric temperature transducers. Specifications

国家药监局, Nickel-titanium alloy service temperature

YY/T 1771-2021 Bending-free recovery method to test the phase transition temperature of nickel-titanium shape memory alloy

Society of Automotive Engineers (SAE), Nickel-titanium alloy service temperature

SAE AMS2281A-2002 Trace Element Control Nickel Alloy, Cobalt Alloy, and Iron Alloy Wrought Products for High-Temperature, High-Stressed Applications

BE-NBN, Nickel-titanium alloy service temperature

NBN A 21-222-1977

German Institute for Standardization, Nickel-titanium alloy service temperature

DIN 65464:1990 Aerospace; studs with MJ thread, ring locked, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65268:2011 Aerospace - Hexagon bolts, with MJ thread, short thread, titanium alloy, nominal tensile strength 1 100 MPa, for temperatures up to 315 C
DIN 65526:1998 Aerospace - Hexagon bolts, close tolerance, with short-length MJ thread, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65438:1993 Aerospace; bihexagonal head bolts, close tolerance, with MJ-thread, short thread length, in titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65338:1993 Aerospace; hexagon bolts, close tolerance, with short-length MJ thread, shoulder, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65442:1993 Aerospace; bihexagonal head bolts, close tolerance, with medium-length MJ thread, corrosion resisting nickel alloy; nominal tensile strength 1550 MPa, for temperatures up to 315 °C
DIN 65265:1998 Aerospace - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65537:1987 Aerospace; cheese head bolts with bihexagon socket and MJ thread, short thread, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C
DIN 65442:2016 Aerospace - bihexagonal head bolts, close tolerance, with medium-length MJ thread, corrosion resisting nickel alloy - nominal tensile strength 1 550 MPa, for temperatures up to 315 °C; Inactive for new design
DIN 65526:2016 Aerospace series - Hexagon bolts, close tolerance, with short-length MJ thread, titanium alloy, nominal tensile strength 1100 MPa, for temperatures up to 315 °C; Text in German and English
DIN 65538:1987 Aerospace; cheese head bolts, close tolerance, with bihexagon socket and MJ thread, short thread, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C
DIN 65557:1989 Aerospace; pan head screws with ribbed TORQ-SET (ACR) recess and MJ thread, fully threaded, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65558:1989 Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, fully threaded, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65324:1993 Aerospace; pan head bolts, close tolerance, with internal offset cruciform ribbed drive recess and short-length MJ thread, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65526:2020-10 Aerospace series - Hexagon bolts, close tolerance, with short-length MJ thread, titanium alloy, nominal tensile strength 1 100 MPa, for temperatures up to 315 °C; Text in German and English
DIN 65289:1987 Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, titanium alloy, nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65324:2015 Aerospace series - Pan head bolts, close tolerance, with internal offset cruciform ribbed drive recess and short-length MJ thread, titanium alloy, nominal tensile strength 1 100 MPa, for temperatures up to 315 °C; Text in German and English
DIN 65179:1993 Aerospace; countersunk head bolts, close tolerance, with internal offset cruciform ribbed drive and MJ thread, short thread length, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65515:1984-07 Aerospace; cheese head bolts, with internal serration and MJ-thread, short thread, titanium alloy, nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65338:2020-10 Aerospace series - Hexagon bolts, close tolerance, with short-length MJ thread, shoulder, titanium alloy, nominal tensile strength 1 100 MPa, for temperatures up to 315 °C; Text in German and English
DIN 65289:1987-03 Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, titanium alloy, nominal tensile strength 1100 MPa, for temperatures up to 315 °C
DIN 65541:1987 Aerospace; pan head bolts with ribbed TORQ-SET (ACR) recess and MJ thread; fully threaded, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C
DIN 65542:1987 Aerospace; countersunk head screws, close tolerance, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, nickel alloy, nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C
DIN 65542:1987-03 Aerospace; countersunk head screws, close tolerance, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, nickel alloy, nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C
DIN 65517:2020-03 Aerospace series - Cheese head bolts, close tolerance, with internal serrations and MJ thread, short thread, titanium alloy, nominal tensile strength 1 100 MPa, for temperatures up to 315 °C; Text in German and English

(U.S.) Ford Automotive Standards, Nickel-titanium alloy service temperature

FORD WSS-M2A137-B7-2005 ALUMINUM, HIGH TEMPERATURE. EUTECTIC SILICON COPPER NICKEL MAGNESIUM ALLOY ***TO BE USED WITH FORD WSS-M99P1111-A***
FORD WSF-M6A12-B-2003 TEMPERATURE COMPENSATOR ALLOY ***TO BE USED WITH FORD WSS-M99P1111-A***

AENOR, Nickel-titanium alloy service temperature

UNE 38856:2000 Magnesium and its alloys. Determination of nickel. Photometric method using dimethylglyoxime.
UNE-EN 3379:1997 AEROSPACE SERIES. BOLTS, DOUBLE HEXAGON HEAD, CLOSE TOLERANCE SHANK, MEDIUM LENGTH THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), FOR INCREASED HEIGHT NUTS. CLASSIFICATION: 1 210 MPA (AT AMBIENT TEMPERATURE)/730 oC.

International Organization for Standardization (ISO), Nickel-titanium alloy service temperature

ISO 22910:2020 Corrosion of metals and alloys — Measurement of the electrochemical critical localized corrosion temperature (E-CLCT) for Ti alloys fabricated via the additive manufacturing method

British Standards Institution (BSI), Nickel-titanium alloy service temperature

BS EN 4011:2004 Aerospace series. Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated. Classification: 1550 MPa (at ambient temperature)/600°C
15/30323936 DC BS EN 3833. Aerospace series. Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated. Classification: 1550 MPa (at ambient temperature) / 650 °C. Technical specification
16/30352446 DC BS EN 3833. Aerospace series. Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated. Classification: 1550 MPa (at ambient temperature) / 650 °C. Technical specification

IPC - Association Connecting Electronics Industries, Nickel-titanium alloy service temperature

IPC TM-650 2.6.21B-2011 Service Temperature of Metal-Clad Flexible Laminate@ Cover Material and Adhesive Bonding Films

未注明发布机构, Nickel-titanium alloy service temperature

BS EN 3012:1996(1999) Nuts, bihexagonal, self - locking, in heat resisting nickel base alloy NI - P101HT (Waspaloy) — Classification : 1210 MPa (at ambient temperature)/ 730 °C
BS EN 3013:1996(1999) Nuts, bihexagonal, self - locking, in heat resisting nickel base alloy NI - P101HT (Waspaloy), silver plated — Classification : 1210 MPa (at ambient temperature)/ 730 °C

Aerospace Industries Association, Nickel-titanium alloy service temperature

AIA NASM85604-2000 Bolt, Nickel Alloy 718, Tension, High Strength, (125 KSI Fsu and 220 KSI Ftu), High Temperature, Spline Drive General Specification for FSC 5306

Aerospace, Security and Defence Industries Association of Europe (ASD), Nickel-titanium alloy service temperature

ASD-STAN PREN 3915-1999 Aerospace Series Insert, Thin Wall, Self-Locking, Mj Threads, in Heat Resisting Nickel Base Alloy NI-PH2601 (Ni-P100HT, Inconel 718), for Salvage of Components Classification: 1 275 MPa (at Ambient Temperature)/ 550 C Degrees Technical Specification (Edit
ASD-STAN PREN 3672-1994 Aerospace Series Shank Nuts, Self-Locking, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy), Silver Plated, for 30 Degree Swage Classification: 1 210 MPa (at Ambient Temperature)/730 Degrees C Edition P 1; Corrigendum

European Committee for Standardization (CEN), Nickel-titanium alloy service temperature

EN 3672:2008 Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30 Degrees swage - Classification: 1 210 MPa (at ambient temperature)/730 Degrees C
EN 3672:2016 Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage - Classification: 1210 MPa (at ambient temperature) / 730 °C

ASD-STAN - Aerospace and Defence Industries Association of Europe - Standardization, Nickel-titanium alloy service temperature

PREN 4124-1994 Aerospace Series Shank Nuts@ Self-Locking@ in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy)@ Silver Plated on Thread@ for 60 Degree Swage Classification: 1 210 MPa (at Ambient Temperature)/730 Degrees C (Edition P1)

Association Francaise de Normalisation, Nickel-titanium alloy service temperature

NF ISO 3506-5:2022 Fixations - Caractéristiques mécaniques des fixations en acier inoxydable résistant à la corrosion - Partie 5 : fixations spéciales (incluant également les fixations en alliages de nickel) pour utilisation à hautes températures