(CMA)
(CNAS)
(ISO)
(高新技术企业)
镍钛 温度相关标准参考信息
YY/T 1771-2021 弯曲-自由恢复法测试镍钛形状记忆合金相变温度
简介：
信息：ICS：11.040.40 CCS：C35 发布：2021-03-09 实施：2022-04-01
DIN EN 4635-2010 航空航天系列.镍基合金(Inconel 718)耐高温短螺纹六瓣凹槽100°埋头螺钉.分类:1270 MPa(环境温度下)/650℃;德文版本和英文版本EN 4635-2009
简介：
信息：ICS：49.030.20 CCS：V20 发布：2010-12-01 实施：
NF L52-320-003-2008 航空航天系列.热电偶膨胀电缆.使用温度为-65℃～260℃.第003部分:单芯镍铬/镍铝电缆.产品标准
简介：
信息：ICS：49.060 CCS：V25 发布：2008-01-01 实施：2008-01-19
BS EN 4123-2018 航空航天系列.自锁紧螺纹镀银的耐热镍基合金NI-PH 2601(铬镍铁合金718)带柄螺母.等级:1550 MPa(环境温度)/600℃
简介：
信息：ICS：49.030.30 CCS：V20 发布：2018-05-24 实施：2018-05-24
DIN EN 4131-2010 航空航天系列.耐热镍基合金铝IVD涂层,标准六角边头松公差普通柄短螺纹螺栓.等级:1250 MPa(环境温度)/425℃.德文和英文版本EN 4131-2009 + AC-2010
简介：
信息：ICS：49.030.20 CCS：V20 发布：2010-08 实施：
BS EN 4049-004-2006 航空航天系列.热电偶膨胀电缆.工作温度在65℃～260℃之间.第004部分:双芯镍铬/镍铝屏蔽电缆和护套电缆.产品标准
简介：This standard specifies the characteristics of thermocouple cables used for the connection between the thermocouple and the equipment. Temperatures between − 65 °C and 260 °C (except otherwise specified in the product standard).
信息：ICS：49.060 CCS：V25 发布：2007-03-30 实施：2007-03-30
ASTM F2004-17 镍钛合金热分析转化温度的标准试验方法
简介：
信息：ICS：77.120.40 CCS： 发布：2017-10-01 实施：
ASTM F2004-05(2010) 镍钛合金热分析转化温度的标准试验方法
简介：
信息：ICS：77.120.40 CCS： 发布：2010-06-01 实施：
BS EN 4049-003-2006 航空航天系列.热电偶膨胀电缆.工作温度为65℃～260℃.第003部分:单芯镍铬/镍铝电缆.产品标准
简介：This standard specifies the characteristics of thermocouple cables used for the connection between the thermocouple and the equipment. Temperatures between − 65 °C and 260 °C (except otherwise specified in the product standard).
信息：ICS：49.060 CCS：V25 发布：2007-03-30 实施：2007-03-30
ASTM F2004-16 镍钛合金热分析转化温度的标准试验方法
简介：
信息：ICS：77.120.40 CCS： 发布：2016-12-01 实施：
NF L24-145-2009 航空航天系列.具有粗糙公差标准柄的铝IVD涂覆的耐热镍基合金标准六角头螺钉.类别:1250 MPa (在环境温度下)/425 oC
简介：
信息：ICS：49.030.20 CCS：V20 发布：2009-11-01 实施：2009-11-07
DIN EN 4120-2006 十二角、自锁紧、NI-PH1302耐热镍基合金(沃斯帕洛尹合金)、螺纹镀银的螺母.分类:1210MPa(环境温度下)/730 鳦
简介：This standard specifies the characteristics of self-locking bihexagonal nuts in NI-PH1302, silver plated on thread, for aerospace applications. Classification: 1210 MPa / 730 ?,
信息：ICS：49.030.30 CCS：V20 发布：2006-11 实施：
DIN 65442-2016 航空航天.使用温度315℃以下公称抗拉强度1550MPa耐蚀镍合金制中长等度MJ螺纹的紧公差十二角头螺栓.不适用于新设计
简介：
信息：ICS：49.030.20 CCS：V20 发布：2016-08 实施：
NF L24-127-2009 航空航天系列.螺栓,正规六角螺栓头,在热稳定铝IVD涂层镍基合金涂层下的正规六角低精度公差标准柄中等长度螺纹螺栓.分类:1 250 MPa(环境温度)/425 oC.
简介：
信息：ICS：49.030.20 CCS：V20 发布：2009-11-01 实施：2009-11-07
EN 3444-2006 航空航天系列.钝化的耐热镍基合金中长度螺纹,紧公差标准杆,大型十二角头螺栓.等级-1250MPa(环境温度)/650摄氏度
简介：This standard specifies the characteristics of bolts, large bihexagonal head, close tolerance normal shank,medium length thread, in heat resisting nickel base alloy, passivated.Classification: 1 250 MPa1) / 650 °C2).
信息：ICS：49.030.30 CCS： 发布：2006-07-01 实施：
DIN 65447-2016 航空航天系列. 带中等长度MJ螺纹的耐蚀镍合金紧公差十二角头螺栓. 公称抗拉强度1 550 MPa, 温度不超过315 ℃
简介：
信息：ICS：49.030.20 CCS： 发布：2016-08 实施：
BS EN 4635-2009 航空航天系列.镀银NI-PH2601镍基合金(Inconel 718)耐高温短螺纹六瓣凹槽100°埋头螺钉.分类:1270 MPa(环境温度)/650℃
简介：This standard specifies the characteristics of screws with 100° countersunk head, with six lobe recess, shortthread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), for aerospace applications.
信息：ICS：49.030.20 CCS：V20 发布：2009-08-31 实施：2009-08-31
DIN EN 4352-2006 航空航天系列.镀MoS2的耐热镍基合金NI-PH2601(铬镍铁合金 718)制带安全锁线孔、减径柄、长螺纹的双六角头螺栓.等级:1550MPa(环境温度)/425℃.德文和英文版本EN 4352-2004
简介：
信息：ICS：49.030.20 CCS：V20 发布：2006-03 实施：
ASTM F2082/F2082M-16 通过弯曲和自由回收测定镍 - 钛形状记忆合金的转变温度的标准测试方法
简介：
信息：ICS：77.120.50 CCS： 发布：2016-04-01 实施：
BS EN 4128-2009 航空航天系列.镀铝IVD镍基合金钢短螺纹粗公差标称杆标准六角头螺栓.分类:1250 MPa(环境温度)/425℃
简介：This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated.Classification: 1 250 MPa/425℃
信息：ICS：49.030.20 CCS：V20 发布：2009-07-31 实施：2009-07-31
DIN EN 4009-2006 航空航天系列.耐热镍基合金NI-PH2601(铬镍铁合金718)制带安全锁线孔、减径柄、长螺纹的双六角头螺栓.等级:1550MPa(环境温度)/650℃.德文和英文版本EN 4009:2004
简介：This standard specifies the characteristics of double hexagon headed bolts with close tolerance shank and medium length thread in NI-PH2601 for aerospace applications.
信息：ICS：49.030.20 CCS：V20 发布：2006-03 实施：
EN 4128-2016 航空航天系列-镀铝IVD镍基合金钢短螺纹粗公差标称杆标准六角头螺栓-分类:1250MPa(环境温度)/425℃
简介：This European Standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1250 MPa/425 °C.
信息：ICS：49.030.20 CCS：V11 发布：2016-03 实施：
EN 4128-2009 航空航天系列.铝IVD涂层耐热镍基合金中短螺纹紧公差标准柄标称六角头螺栓头螺栓.等级-1250 MPa(环境温度)/425℃
简介：This standard specifies the characteristics of bolts; normal hexagonal head; coarse tolerance normal shank; short thread; in heat resisting nickel base alloy; aluminium IVD coated. Classification: 1250 MPa / 425 ℃.
信息：ICS：49.030.20 CCS： 发布：2009-07-01 实施：
DIN EN 4321-2006 航空航天系列.镀银耐热镍基合金NI-PH2601(铬镍铁合金718)制带安全锁线孔、减径柄、长螺纹的双六角头螺栓.等级:1550MPa(环境温度)/650℃.德文和英文版本 EN 4321:2004
简介：
信息：ICS：49.030.20 CCS：V20 发布：2006-03 实施：
ASTM F2082/F2082M-2016 通过弯曲和自由恢复测定镍钛形状记忆合金变形温度的标准试验方法
简介：5.1x00a0;This test method provides a rapid, economical method for determination of transformation temperatures. 5.2x00a0;Measurement of the specimen motion closely parallels many shape memory applications and provides a result that is applicable to the function of the material. 5.3x00a0;This test method uses wire, tube, or strip samples; thus, it is able to provide an assessment of the product in its semifinished form. 5.4x00a0;This test method may be used on annealed samples to determine the transformation temperatures and assure the alloy formulation, since chemical analysis is not precise enough to determine adequately the nickel-to-titanium ratio of shape memory alloys. 5.5x00a0;Transformation temperatures derived from this test method may differ from those derived from other methods as a result of the effects of strain and load on the transformation temperature. 5.6x00a0;The test method is applicable to shape memory alloys with Af temperatures in the range of approximately x2013;25 to x00b1;8201;90x00b0;C. 1.1x00a0;This test method describes a procedure for determining the martensite-to-austenite transformation temperatures of either fully annealed or heat-treated nickel titanium alloys by measuring the deformation recovered during the thermal transformation. 1.2x00a0;The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with this standard. 1.3x00a0;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 establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
信息：ICS： CCS： 发布：2016 实施：
DIN EN 4134-2009 航空航天系列.镀铝IVD耐火镍基合金制普通六角头紧公差标准柄长螺纹螺栓.等级:1250 MPa(环境温度)/425℃.德文版本和英文版本EN 4134-2009
简介：This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank,long thread, in heat resisting nickel base alloy, aluminium IVD coated.Classification: 1 250 MPa / 425 ℃.
信息：ICS：49.030.20 CCS：V20 发布：2009-07 实施：
NF L24-143-2006 航空航天系列.十字凹槽、紧公差标准杆、中等长度螺纹、大十二头耐热钝化镍基合金铝覆层螺栓.分类:1 550 MPa(环境温度)/315℃
简介：
信息：ICS：49.030.20 CCS：V20 发布：2006-02-01 实施：2006-02-20
ASTM F2082-15 通过弯曲和自由回收测定镍 - 钛形状记忆合金的转变温度的标准测试方法
简介：
信息：ICS：77.120.50 CCS： 发布：2015-05-01 实施：
DIN EN 4131-2009 航空航天系列.铝IVD涂层耐热镍基合金普通六角头紧公差中等长度螺纹螺栓.分类:1250MPa(环境温度)/425C,德文和英文版本EN4131
简介：This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank,medium length thread, in heat resisting nickel base alloy, aluminium IVD coated.Classification: 1 250 MPa/ 425 ℃.
信息：ICS：49.030.20 CCS： 发布：2009-07 实施：
BS EN 4498-2005 航空航天系列.有色铝涂层、钝化的、耐热镍基合金、中等长度螺纹、紧公差标称杆、大双六角头螺栓.等级:1550MPa(环境温度)/315°C
简介：This standard specifies the characteristics of bolts, large bihexagonal head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated, with aluminium pigmented coating.Classification: 1 550 MPa 1) / 315 °C 2)
信息：ICS：49.030.20 CCS：V20 发布：2006-01-31 实施：2006-01-31
ASTM F2082-2015 通过弯曲和自由恢复测定镍钛形状记忆合金转变温度的标准试验方法
简介：5.1x00a0;This test method provides a rapid, economical method for determination of transformation temperatures. 5.2x00a0;Measurement of the specimen motion closely parallels many shape memory applications and provides a result that is applicable to the function of the material. 5.3x00a0;This test method uses wire, tube, or strip samples; thus, it is able to provide an assessment of the product in its semifinished form. 5.4x00a0;This test method may be used on annealed samples to determine the transformation temperatures and assure the alloy formulation, since chemical analysis is not precise enough to determine adequately the nickel-to-titanium ratio of shape memory alloys. 5.5x00a0;Transformation temperatures derived from this test method may differ from those derived from other methods as a result of the effects of strain and load on the transformation temperature. 5.6x00a0;The test method is applicable to shape memory alloys with Af temperatures in the range of approximately x2013; 25 to +90x00b0;C. 1.1x00a0;This test method describes a procedure for determining the martensite-to-austenite transformation temperatures of either fully annealed or heat-treated nickel titanium alloys by measuring the deformation recovered during the thermal transformation. 1.2x00a0;The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with this standard. 1.3x00a0;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 establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
信息：ICS： CCS： 发布：2015 实施：
BS EN 4131-2009 航空航天系列.耐高温镀铝IVD镍基合金中等螺纹粗公差标称杆标准六角头螺栓.等级:1250 MPa(环境温度)/425℃
简介：This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank,medium length thread, in heat resisting nickel base alloy, aluminium IVD coated.Classification: 1 250 MPa / 425 °C
信息：ICS：49.030.20 CCS：V20 发布：2009-05-31 实施：2009-05-31
ASTM F2082-2006 通过弯曲和自由回复试验测定镍钛形状记忆合金转变温度的标准试验方法
简介：This test method provides a rapid, economical method for determination of transformation temperatures. Measurement of the specimen motion closely parallels many shape memory applications and provides a result that is applicable to the function of the material. This test method uses wire, tube, or strip samples; thus, it is able to provide an assessment of the product in its semifinished form. This test method may be used on annealed samples to determine the transformation temperatures and assure the alloy formulation, since chemical analysis is not precise enough to determine adequately the nickel-to-titanium ratio of shape memory alloys. Transformation temperatures derived from this test method may differ from those derived from other methods as a result of effects of strain and load on the transformation temperature. The test method is applicable to shape memory alloys with Af temperatures in the range of approximately x2013; 25 to +90x00B0;C.1.1 This test method describes a procedure for determining the martensite-to-austenite transformation temperatures of either fully-annealed or heat-treated nickel titanium alloys by measuring the deformation recovered during the thermal transformation. 1.2 The values in SI units are to be regarded as the standard. The values given in inch-pound units are provided for information only.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 establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
信息：ICS：77.120.50 CCS：H64 发布：2006 实施：
YS/T 970-2014 镍钛形状记忆合金相变温度测定方法
简介：本标准规定了镍钛形状记忆合金相变温度测定方法——弯曲和自由回复法。本标准适用于通过测量热相变过程的回复变形量测定马氏体逆相变相变温度,适用于马氏体逆相变终了温度A介于-25 ℃~90 ℃的完全退火态或热处理态丝材、管材或者带材。
信息：ICS：77.160 CCS：H16 发布：2014-10-14 实施：2015-04-01
BS EN 4134-2009 航空航天系列.耐高温镀铝IVD镍基合金长螺纹粗公差标称杆标准六角头螺栓.等级:1250 MPa(环境温度)/425℃
简介：This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank,long thread, in heat resisting nickel base alloy, aluminium IVD coated.Classification: 1 250 MPa / 425 °C
信息：ICS：49.030.20 CCS：V20 发布：2009-05-31 实施：2009-05-31
EN 4049-004-2006 航空航天系列.热电偶膨胀电缆.工作温度在65℃～260℃之间.第004部分:双芯镍铬/镍铝屏蔽电缆和护套电缆.产品标准
简介：This standard specifies the characteristics of thermocouple cables used for the connection between the thermocouple and the equipment. Temperatures between ? 65 °C and 260 °C (except otherwise specified in the product standard).
信息：ICS：49.060 CCS： 发布：2006 实施：
JB/T 9500-2014 镍铬铁温度磁补偿合金带材
简介：本标准规定了镍铬铁温度磁补偿合金冷轧带材的产品分类、技术要求、试验方法、检验规则、标志、包装和质量证明书。本标准适用于电能表(电度表)及里程表用温度磁补偿合金冷轧带材。
信息：ICS：77.120.40 CCS：N05 发布：2014-07-09 实施：2014-11-01
EN 4134-2009 航空航天系列.铝IVD涂层的耐火镍基合金制普通六角头紧公差标准柄长螺纹螺栓.等级-1250MPa(环境温度)/425摄氏度
简介：This standard specifies the characteristics of bolts; normal hexagonal head; coarse tolerance normal shank; long thread; in heat resisting nickel base alloy; aluminium IVD coated. Classification: 1250 MPa / 425 ℃
信息：ICS：49.030.20 CCS： 发布：2009-04-01 实施：
EN 4049-003-2006 航空航天系列.热电偶膨胀电缆.工作温度为65℃～260℃.第003部分:单芯镍铬/镍铝电缆.产品标准
简介：This standard specifies the characteristics of thermocouple cables used for the connection between the thermocouple and the equipment. Temperatures between ? 65 °C and 260 °C (except otherwise specified in the product standard).
信息：ICS：49.060 CCS： 发布：2006 实施：
GOST 1791-2014 热电式温度传感器延长导线使用的镍和铜-镍合金线. 规格
简介：
信息：ICS：77.150.40 CCS： 发布：2014 实施：2015-09-01
GOST 6651-2009 国家测量统一性保证体系.铂金,铜及镍阻抗温度传感器.一般要求及测试方法
简介：
信息：ICS：17.200.20 CCS： 发布：2009 实施：2011-01-01
ASTM F2004-05 镍钛合金热分析转化温度的标准试验方法
简介：
信息：ICS：77.120.40 CCS： 发布：2005-10-01 实施：
NF L52-010-008-2013 航空航天系列. 电缆安装. 间位芳族聚酰胺纤维制保护套. 第008部分: 工作温度介于-55℃至200℃之间的灵活点安装, 带镍铜编制的自卷屏蔽式(EMI)保护套. 产品标准
简介：
信息：ICS：49.060 CCS：V25 发布：2013-05-03 实施：2013-05-03
GOST 8.461-2009 国家测量统一性保证体系.铂金,铜和镍的电阻温度传感器.验证方法
简介：
信息：ICS：17.200.20 CCS： 发布：2009 实施：2011-01-01
NF L24-560-2005 航空航天系列.十二角、自锁紧、NI-PH1302耐热镍基合金(沃斯帕洛尹合金)、螺纹镀银的螺母.分类:1210MPa(环境温度下)/730 鳦
简介：
信息：ICS：49.030.30 CCS：V20 发布：2005-05-01 实施：2005-05-20
DIN EN 6049-008-2013 航空航天系列. 电缆装置. 间位芳香族聚酰胺纤维保护套管. 第008部分:工作温度为-55℃至200℃的灵活点装置用带镍铜编织带的自包裹式 (EMI) 保护套管. 产品标准; 德文和英文版本EN 6049-008-2013
简介：
信息：ICS：49.060 CCS：V25 发布：2013-03 实施：
EN 3672-2008 航空航天系列.30°型铁用镀银NI-P101HT型耐热镍合金(沃斯帕洛伊合金)自锁紧带柄螺母.分类-1210MPa(环境温度)/73℃
简介：This standard specifies the characteristics of self-locking shank nuts in NI-P101HT; silver plated; for use in 30° cone holes; for aerospace applications. Classification: 1210 MPa1)/730 ℃2)
信息：ICS：49.030.30 CCS： 发布：2008-08-01 实施：
AECMA PREN 4612-011-2005 航空航天系列.通用单芯和多芯电缆XLETFE族 护套或屏蔽和护套.第011部分:镍镀铜 操作温度负65摄氏度到150摄氏度双压壁
简介：The text of this standard, which exists in three equivalent versions (English, French, German) has been drawn up under the responsibility of A ECMA (Association Européenne des Constructeurs de Matériel Aérospatial) andhas been circulated to Official Services. Any reservations expressed by Official Services and not resolved in thisissue, have been incorporated in the history sheet which has accompanied rhis prEN to CEN.
信息：ICS：67.080.20 CCS：V25 发布：2005-03-01 实施：
GOST R 55917-2013 热电温度传感器扩展导线用镍和铜镍合金线. 规格
简介：
信息：ICS：77.150.40 CCS： 发布：2013 实施：2015-01-01
DIN EN 4049-003-2008 航空航天系列.热电偶延伸电缆.工作温度为-65℃～260℃.第003部分:单芯镍铬/镍铝.产品标准
简介：This standard specifies the characteristics of thermocouple cables used for the connection between the ther-mocouple and the equipment. Temperatures between - 65 ~C and 260 ~C (except otherwise specified in theproduct standard).
信息：ICS：49.060 CCS：V40 发布：2008-05 实施：
AECMA PREN 4612-013-2005 航空航天系列.通用单芯和多芯电缆XLETFE族 护套或屏蔽和护套.第013部分:SX,TC和UC 镍镀铜 操作温度负65摄氏度到150摄氏度单压壁
简介：This draft is now available for public comment and your views and technical comments on it would be appreciated.If you have no specific comments to make but find it generally acceptable it would be helpful if you would notify usaccordingly. Suggestions entailing revision of the text should indicate the preferred wording. Please quote therelevant clause number against any comnnient.
信息：ICS：67.080.20 CCS：V25 发布：2005-03-01 实施：
GOST R 55917-2013 热电温度传感器扩展导线用镍和铜镍合金线. 规格
简介：
信息：ICS：77.150.40 CCS： 发布：2013 实施：2015-01-01
DIN EN 4049-004-2008 航空航天系列.热电偶延伸电缆.工作温度为-65℃～260℃.第004部分:屏蔽的和置于壳内的双芯镍铬/镍铝电缆.产品标准
简介：This standard specifies the characteristics of thermocouple cables used for the connection between the ther-mocouple and the equipment. Temperatures between - 65 ℃ and 260 ℃ (except otherwise specified in theproduct standard).
信息：ICS：49.060 CCS：V40 发布：2008-05 实施：
AECMA PREN 4612-012-2005 航空航天系列.通用单芯和多芯电缆XLETFE族 护套或屏蔽和护套.第012部分:镍镀铜 操作温度负65摄氏度到150摄氏度双压壁
简介：This industrial standard for the aerospace sector has been drawn up under the responsibility of AECMA.
信息：ICS：67.080.20 CCS：V25 发布：2005-03-01 实施：
ASTM B637-2012e1 中等或较高温度作业用沉淀硬化镍合金棒材、锻件及锻坯标准规格
简介：1.1 This specification2 covers hot- and cold-worked precipitation-hardenable nickel alloy rod, bar, forgings, and forging stock for moderate or high temperature service (Table 1).TABLE 1 Chemical Requirements Element Composition Limits, % UNS N07022 UNS N07208 UNS N07252 (Formerly Grade 689) UNS N07001 (Formerly Grade 685) UNS N07500 (Formerly Grade 684) UNS N07750 (Formerly Grade 688) UNS N07718 (Formerly Grade 718) Carbon 0.010 max 0.04???0.08 0.10???0.20 0.03???0.10 0.15 max 0.08 max 0.08 max
信息：ICS：77.150.40 (Nickel and chromium products) CCS：H62 发布：2012 实施：
ASD-STAN PREN 4635-2008 航空航天系列．耐热镍基合金NI-PA2601（铬镍铁合金 718）制短螺纹六瓣凹槽100°沉头螺钉．等级:1270MPa（环境温度条件下）/650℃;第P1版
简介：
信息：ICS： CCS： 发布：2008-01-31 实施：
ASTM F2004-2005 用热分析法测定镍-钛合金转变温度的标准试验方法
简介：Differential scanning calorimetry provides a rapid method for determining the transformation temperature(s) of nickel-titanium shape memory alloys. This test method uses small, stress-free, annealed samples to determine whether a sample of nickel-titanium alloy containing nominally 54.5 to 56.5 % nickel by weight is austenitic or martensitic at a particular temperature. Since chemical analysis of these alloys does not have sufficient precision to determine the transformation temperature by measuring the nickel to titanium ratio of the alloy, direct measurement of the transformation temperature of an annealed sample of known thermal history is recommended. This test method is useful for quality control, specification acceptance, and research. Transformation temperatures derived from differential scanning calorimetry (DSC) may not agree with those obtained by other test methods due to the effects of strain and load on the transformation.1.1 This test method defines procedures for determining the transformation temperatures of nickel-titanium shape memory alloys.1.2 The values stated in SI units are to be regarded as the standard.1.3 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 establish appropriate safety and health practices and to determine the applicability of regulatory limitations prior to use.
信息：ICS：77.120.40 (Nickel, chromium and their alloys); 77. CCS：H62 发布：2005 实施：
DIN 65539-2011 航空航天.带内细齿和MJ螺纹,短螺纹,镍合金制,标称抗拉强度1,250MPa,温度最高达315℃/425℃的凸圆头螺栓
简介：
信息：ICS：49.030.20 CCS：V20 发布：2011-07 实施：
NF L52-320-003-2008 航空航天系列.热电偶膨胀电缆.使用温度为-65℃～260℃.第003部分:单芯镍铬/镍铝电缆.产品标准
简介：
信息：ICS：49.060 CCS：V25 发布：2008-01-01 实施：2008-01-19
ASTM F2004-2005(2010) 标准转化镍钛合金温度的热分析的标准试验方法
简介：Differential scanning calorimetry provides a rapid method for determining the transformation temperature(s) of nickel-titanium shape memory alloys. This test method uses small, stress-free, annealed samples to determine whether a sample of nickel-titanium alloy containing nominally 54.5 to 56.5 % nickel by weight is austenitic or martensitic at a particular temperature. Since chemical analysis of these alloys does not have sufficient precision to determine the transformation temperature by measuring the nickel to titanium ratio of the alloy, direct measurement of the transformation temperature of an annealed sample of known thermal history is recommended. This test method is useful for quality control, specification acceptance, and research. Transformation temperatures derived from differential scanning calorimetry (DSC) may not agree with those obtained by other test methods due to the effects of strain and load on the transformation.1.1 This test method defines procedures for determining the transformation temperatures of nickel-titanium shape memory alloys. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.3 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 establish appropriate safety and health practices and to determine the applicability of regulatory limitations prior to use.
信息：ICS：77.120.50 CCS：H13 发布：2005 实施：
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