为了正常的体验网站,请在浏览器设置里面开启Javascript功能!

NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求(1)

2017-09-25 23页 doc 107KB 38阅读

用户头像

is_852287

暂无简介

举报
NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求(1)NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求(1) New NADCAP Requirements for Temperature Uniformity for Vacuum Heat Treatment according to AMS 2750D NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求 Janusz Kowalewski – Vice General Manager SECO/WARWICK (Tianjin) Industrial Furnaces, Tian...
NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求(1)
NADCAP依据AMS2750D 对真空热处理温度均匀性的新要求(1) New NADCAP Requirements for Temperature Uniformity for Vacuum Heat Treatment according to AMS 2750D NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求 Janusz Kowalewski – Vice General Manager SECO/WARWICK (Tianjin) Industrial Furnaces, Tianjin, China 亚诺 . 斯基---赛科/沃克公司天津工业炉有限公司副总经理 (注:NADCAP 是“国家航空和国防承包商认证程序”的缩写) In conjunction with constant technological development in the aerospace industry field, the requirements set for equipment for heat treatment have increased, particularly in the area of temperature uniformity precision, the repeatability of results, and the proper archivization of results. Much attention is also being given to processes for facilitating the attainment of the proper balance between advanced technologies and their economic aspects. This places new demands in the coming years on the suppliers of vacuum furnaces, and it creates the need to adapt furnace design to the changing requirements and expectations of the market。 配合航空工业领域技术的不断发展,对热处理设备的要求也相应提高,特别在温度 均匀性精度、热处理结果的重复能力、以及适当的其结果编档保存方面。人们更关 注设备程序上要达到技术先进,和其经济上合理的平衡。近几年真空炉的制造商都 将这些作为新的要求,迎合对炉子设计的改进和市场的期望,而创造出相应的提 高。 The majority of world manufacturers and contractors operating in the aerospace industry are associated with the international program Nadcap, which was begun in 1990 by the PRI (Performance Review Institute), an outgrowth of the SAE organization. This program was designated initially as NADCAP, an acronym for National Aerospace and Defense Contractors Accreditation Program. Currently, in order to lend the program an international character, only the acronym Nadcap is used. 航空工业方面大多数的世界制造商和承包商在国际NADCAP规划下组织一起,这 个组织是1990年由PRI(性能审查协会)开始的,是SAE(美国汽车师学 会)派生形成的。它最初定名为NADCAP,是国家航空和国防承包商认证程序的 缩写。现在为了借用这个程序的国际性质,仅用其首字母缩写为Nadcap. Within the Nadcap framework, the primary manufacturers of aerospace equipment aim toward technological development and increase the quality of products among their contractors (subcontractors) by imposing strict process and procedures requirements. The Nadcap development plan establishes the total elimination of unaccredited contractors in this program over the course of the next few years. Growing number of subcontractors worldwide stimulated by new production programs (e.g., the Airbus A380, the Boeing 787 Dreamliner), requite adaptation of strict quality procedures. 在Nadcap的构架下,主要的航空设备制造商的目的是提高技术;再者就是严格程 序和步骤的要求,使承包商(转包商)提高产品的质量。在以后的几年,Nadcap 1 发展计划确定排除全部未经认可的承包商。受新生产规划(例如:空客 A380 ,波 音 787 梦班机)的激励,不断增加的转包商也要求其严格的质量步骤。 In the field of heat treatment, the program of annual Nadcap audits is based on inspection list AC7102, prepared in compliance with the SAE AS7102 standard (National Aerospace and Defense Contractors Accreditation Program -- REQUIREMENTS FOR HEAT TREATING), which were developed in 1993 and were revised in 1995: 在热处理领域,年度Nadcap审查以检查AC7102目录为基础,遵从SAE AS7102 标准(国家航空和国防承包商认证程序---热处理要求),其是1993年实施并在 1995年修改的: AS7001 National Aerospace and Defense Contractors Accreditation Program (NADCAP) - Program Description; (NADCAP)-程序描述 AS7002 National Aerospace and Defense Contractors Accreditation Program (NADCAP)- Rules for Implementation; (NADCAP)-执行规则 AS7003 National Aerospace and Defense Contractors Accreditation Program (NADCAP)- Program Operation; (NADCAP)-程序操作 AS7101 NADCAP-Requirements for Accreditation of Materials Test Laboratories; NADCAP- 对材料检测实验室条件的要求 AS7102/1 NADCAP-Requirements for Heat Treating Accreditation Programs- Brazing Requirements; NADCAP -对热处理鉴定程序要求—钎焊要求 AMS 2750D Pyrometry; 测高温 AMS2801 Heat Treatment, Titanium Alloy Parts; 热处理,钛合金部件 AMS 3025 Polyalkylene Glycol Heat Treatment Quenchant; 聚二醇、乙二醇热处理淬火ant ARP1820 Chord Method of Evaluating Surface Microstructural Characteristics 评价面显微组织特征的弦方法 ARP1962 Certification of Heat Treating Personnel. 热处理人员资质 Aerospace standard AS7102 defines requirements for contractors working toward Nadcap accreditation in the field of Heat Treatment, issued according to the following algorithm: 航空标准AS7102详细说明承包商的热处理工序要遵从Nadcap的要求,根据以下 的运算法则发布: Contractors who are seeking to acquire Nadcap accreditation develop internal operating procedures based upon the recommendations of the AS7102 standard. These recommendations cover: 2 希望获得Nadcap鉴定合格的承包商,在内部操作步骤上要符合AS7102标准的建 议。这些建议是: , development of internal Quality System procedures; 内部质量系统程序的发展 , planning and inspection of Heat Treatment processes; 热处理程序的计划和检测 , training and evaluation of personnel; 员工的与评估 , managing customer materials designated for heat treatment and safeguarding them properly; 对顾客热处理材料的合理设计和维护 , researching surface hardness, metallographic hardness, micro hardness, and the like; 研究表面硬度,金相硬度,显微硬度等等 , servicing, inspection, and maintenance of heat treatment furnaces. 热处理炉的服务,检测和保养维修 AS 7102 标准 INTERNAL QUALITY SYSTEM PROCEDURES 内部质量系统程序 PLANNING AND INSPECTION OF HEAT TREATMENT PROCESSES 热处理程序的计划和检测 TRAINING AND EVLUATION OF PERSONNEL 员工的培训与评价 MANAGING AND SAFEGUARDING HEAT TREATMENT MATERIALS 热处理材料的管理和维护 HARDNESS AND METALLOGRAPHIC RESEARCH 硬度和金相研究 INSPECTION AND MAINTENANCE OF HEAT TREATMENT FURNACES 热处理炉的检查和维护 DETAILED REQUIREMENTS OF RELATED STANDARDS (AMS2750D) 相关标准的详细要求 (AMS2750D) In the field related directly to heat treatment furnaces, requirements have been defined primarily related to: 直接与热处理炉相关的方面,主要基本详细要求是: 3 , guaranteeing and documenting the precise heating speed, the holding temperature and the cooling speed of heat-treated materials or parts; 保证和归档记载:准确的加热速度,热处理材料或部件的保温温 度和冷却速度 , periodic inspection of temperature distribution (uniformity) in the usable area of the furnace; 定期检查:使用期间炉子各个区域的温度分布(均匀性) , inspection of the accuracy of the measuring system (temperature sensors, test tracks and reading, regulating and recording equipment); 检查:测量系统的精确性(温度传感器、测试轨迹和读数、校准 和记录设备) , periodic calibration of testing equipment; 周期性校准:检测设备 , inspection of buildup (pressure increase) for vacuum furnaces; 检查:(由于压力增加)真空炉的杂质 , inspection of purity of cooling gas for vacuum furnaces with gas cooling; 对于带有气冷的真空炉,检查冷却气体的纯度 , planning of periodic prevention reviews and their scope and documentation. 定期的预防/评估计划,及其范围和文件 In the area of requirements related to the accuracy of temperature regulation and uniformity, standard AMS2750 (Aerospace Material Specification) is used most often. It was issued by SAE (Society of Automotive Engineers) in 1980. The most recent revision AMS2750D appeared in September, 2005. It introduces stricter requirements for temperature measurement, inspection and recording equipment in furnaces installed after September 2006. 关于温度校准精度和均匀性的要求,通常在AMS2750(航空材料性 能)标准中已经有所说明。它是SAE(汽车工程师学会)在1980年 公布的。在2005年9月推出了最近修订版AMS2750D。在2006年9 4 月后介绍了有关对炉子安装后的温度测量、检查和记录仪的严格要 求。 It is worth noting that a classification for furnaces was introduced in the AMS2750D with regard to minimum requirements for temperature uniformity in the work area: 值得说明的是在AMS2750D里,介绍了对各级别炉子分类、而对工 作区温度均匀性的最小要求。 Temperature uniformity (?C) Furnace class 炉子分类级别 温度均匀性 1 , 3 2 , 6 3 , 8 4 , 10 5 , 14 6 , 28 oC was thus in class two. Thus, furnace The equipment developed to date at standard ,5 manufacturers are now faced with the obligation to meet the class 1 requirements in their standard products. o到目前为止分类在级别2的炉子,其温度均匀性标准在,5C。那么,炉子制作商现 在面临的任务是使炉子的温度均匀性标准符合级别1的要求。 Photo. 1 Temperature distribution study in accordance with the requirements of standard AMS2750D. Seco/Warwick 10.0VPT-4050/60HV universal vacuum furnace with usable area dimensions of 36”Wx32”Hx60”L (900x800x1500mm.) 照片1 符合AMS2750D标准要求温度分布 /沃克10.0VPT-的研究。赛科 4050/60HV型通用真空炉,其有效 36”Wx32”Hx60”L 使用尺寸是 (900x800x1500mm.) In its revised version, standard AMS2750D imposes upon furnace users the duty of periodically inspecting the accuracy of the temperature measuring system. The so-called SAT (System Accuracy Test) tests are done with a frequency that depends upon the furnace class and the type of measuring equipment used in it ("A" or "E"). In the case of the vacuum furnace type classed as 2D, the SAT test should be performed weekly. End 5 users of vacuum furnaces from the aerospace industry are expecting a new design solution in the area of measuring sensors, recording and thermocouple feedthroughs, in order to optimizing this procedure. 在修订版里,AMS2750D标准加强对使用者在炉子运行期间检查温度系统精确度 的责任要求。所谓SAT检测(系统精确度的检测),其操作检测的频率主要依据 炉子的级别和测试设备的类型(A 或E)而定。在真空炉子类型级别分类为2D的 情况下,SAT要求每周检测一次。航空工业真空炉使用者希望设计一个新检测传 感器、记录仪和热电偶馈入装置等的,这样是为了优化完善这个步骤。 Photo. 2 Dual "S" type thermocouple (Controlling and Over-Temperature) adapted to the requirements of SAT inspection procedure in compliance with AMS2750D. 图片2 双芯“S”型热电偶(控制和超温)适合 SAT检测的要求,并符合AMS2750D标准。 Photo 2 presents one of the solutions used in Seco/Warwick furnaces. The so-called "nonresident" SAT thermocouples may be inserted at any time, including during the course of the production process into an impermeable thermo-well built into the regulatory-safeguarding thermocouple in the illustration. 照片2展示1个赛科/沃克炉子的解决方法。所谓的“非固定”SAT热电偶可以随 时插入炉中。包括在生产过程中插入密闭的热-井结构中,可调整-保护式热电偶。 如图所示。 The use of a tight cork safeguards the heating chamber of the furnace against oxidization in the event of a mechanical failure of the thermo-well. 使用密闭塞子装置在热-井结构发生机械故障事件时,防止炉子加热室氧化。 Vacuum furnaces for materials or subassembly heat treatment utilized in the aerospace industry should also meet the following general requirements [1]: 航空工业领域的真空炉对材料或部件热处理时,要符合以下常规要求[1]: -6 , maximum vacuum (empty and cold furnace after degassing) in the range of 10 Torr, -6 极限真空度(排气后空炉和冷炉)在10乇的范围 -4-5 , working vacuum at a level of 10 - 10Torr, -4-5工作真空:10 - 10乇水平, 6 , high accuracy of regulation, and temperature uniformity during heating and cooling, 在加热和冷却时,高精度调节和温度均匀性 , heating capacity of furnace sufficient for heating the charge through the range of o0C/min to 40C/min temperatures of technological utilization with a speed of 20 for example. 炉子对工件有充足的加热能力,在技术使用范围中,实际加热速度是每分钟 摄氏20-40度。 0o, cooling time of the charge from a temperature of 1100C to 540C, for example, for the array of parts used in these industries, at a maximum level of 6 min, which is normally reached in furnaces with a cooling gas pressure of 1.5 bar abs. 例如在炉中排列的工件,在1.5巴绝对压力冷却气体下,工件从温度1100 度冷却到540度的冷却时间,最多用6分钟。 , cooling of the charge with inert gas, most often argon (Ar), with a purity of at least 99.999%. 用惰性气体冷却工件,通常是纯度至少99.999%的氩气 1050In the figure inserted below, sample results of temperature uniformity researched in compliance with AMS2750D are presented, during the segments of heating and holding 1000at a given temperature. 如下图所示,在给定温度菜单下加热和保温的工件,呈现的温度均匀性符合 AMS2750D标准。 950 min. Temp = 669,4 C max. Temp = 695,0 C900,T=25,6 C min. Temp = 747,2 C max. Temp = 773,3 C850 ,T=26,1 C min. Temp = 858,7 C max. Temp = 875,5 C 800,T=16,8 C min. Temp = 901.9 C max. Temp = 904.8 750 C,T=2,9 C 1050 1000 min. Temp = 669,4 C950max. Temp = 695,0 C700,T=25,6 C 900min. Temp = 747,2 Cmax. Temp = 773,3 C ,T=26,1 C850min. Temp = 858,7 C,T=2.9 C max. Temp = 875,5 C 6 min.,T=16,8 C800min. Temp = 901.9 C max. Temp = 904.8 C,T=2,9 C 750 700650,T=2.9 C 6 min. min. Temp = 900.7 C 650600 max. Temp = 904.8 C 550,T=4.1 C 14:00:04 14:04:04t/c #1t/c #2t/c #3t/c #4t/c #5t/c #6t/c #7t/c #8t/c #914:08:04600 14:12:0414:16:04 14:20:0414:24:0414:28:0414:32:04 14:36:0414:40:0414:44:0455014:48:04 14:52:0414:56:04 14:00:04 14:04:04 t/c #1t/c #2t/c #3t/c #4t/c #5t/c #6t/c #7t/c #8t/c #914:08:04 14:12:04 14:16:04 7 14:20:04 14:24:04 14:28:04 14:32:04 14:36:04 14:40:04 14:44:04 14:48:04 14:52:04 14:56:04 The standard vacuum furnace for the aerospace industry yields results of approx. ,10?C in temperature uniformity during the course of heating and below ,3?C during the holding segment. The temperature stabilization time following the beginning of the holding segment is approx. 5 min until the range of ,5?C is reached and another 5 min. until total temperature stabilization at a level below ,3?C) is achieved. This feature is especially important for a quality brazing processes. 航空工业领域的标准真空炉,在加热时温度均匀性大约是,10?C、而在保温时温度 均匀性小于,3?C。温度稳定的时间,从保温阶段开始计算约5分钟后达到,5?C温 度均匀性范围,然后再经过一个5分钟获得整体温度均匀性好于,3?C水平。这个 特性对工件钎焊质量方面很重要。 Heat-retentive alloys of nickel and cobalt, austenitic and martensite stainless steels, and titanium alloys are use in the aerospace industry. 镍/钴硬磁性合金、奥氏体和马氏体不锈钢、和钛合金都用在航空工业上。 For brazing processes, two furnace designs are currently offered: furnaces with metal (shield) insulation or furnaces with insulation made up of graphite composites. 在钎焊处理中,通常提供设计两种炉子:带有金属隔热屏的真空炉、或是带有石墨 隔热屏的真空炉。 Photo. 3 Seco/Warwick type 6.OVP-4050/48MHV vacuum furnace with 6 bar cooling capability and all metal insulation and moly heating elements. 照片3 赛科/沃克6.OVP-4050/48MHV型真空 6巴冷却压力、全金属隔热屏和钼炉、 镧加热元件 A typical feature of vacuum furnaces with metal insulation is somewhat higher heat o2losses at a high temperature (for example1200C heat losses are approx. 10-11 kW/m) 8 in comparison to graphite chambers. After a certain period of utilization (depending upon the "purity" of heat treat processes), these losses increase to a level of up to 15-16 2. Such changes in heat losses over time means that it is significantly more difficult kW/m to maintain the temperature uniformity and increases energy consumption during heat treatment cycles. The design of heating zones, heating elements and for the manner of placement of heating elements are of key significance to the technological properties of these furnaces. 与石墨隔热屏炉室相比较、全金属隔热屏真空炉的一个典型特征是,在高温下损失 o2的热量会多一些(例如1200C热量损失是大约10-11 kW/m) 。炉子经过一段时间 2 的使用后(决定于热处理过程的“净化”程度)这个损失增加到15-16 kW/m。随 炉子使用时间延长而热损失的这些变化,意味着在热处理周期保持炉温均匀性是相 对很困难的、并增加了能量消耗。因此炉室加热区的设计、加热元件在加热室中的 布置,是决定这些炉子技术性能的关键重点。 The cost of a heating chamber with all metal insulation is higher than that of a heating chamber with graphite insulation. Moreover, to ensure the certainty of obtaining a temperature distribution over a long period of utilization, it is sometimes necessary to use zone regulation, adding heating elements to the door and the back wall, will increase the investment and utilization cost. With the proper quality of materials for the insulation wall, and properly selected vacuum pumps, graphite insulation likewise ensures the level -4-5 of the working vacuum at the level of 10 , 10Torr and the maximum vacuum of even -6at 10 Torr range. 全金属隔热屏加热室的成本要比石墨隔热屏加热室的成本高。而且,为了确保长期 使用后获得一定的温度均匀性分布,有时必须对加热区进行校准、另外在炉门和炉 后墙增加加热元件,这样会增加炉子的投资和使用成本。如果选择了合适的隔热屏 -4-5 材料和适当的真空泵,石墨隔热屏同样可以确保10 - 10乇工作真空度水平、和 -610乇范围的极限真空度水平。 Graphite materials for constructing of the insulation and the heating elements play an essential role. Properly constructed heating chamber graphite insulation is characterized by a significantly lower level of heat loss compared to that of furnaces with metal shield 2oinsulation. For the typical sizes of furnaces, heat loss is 6-7.5 kW/m at 1200C. In practice, the level of these losses does not change over the course of a 10-year period of utilization of the furnace, which significantly differentiated this type of insulation from metal shield insulation. For this reason, periodic certifications of temperature distribution are just as accurate as in an initial test, and the requirements relative to solutions in the area of managing heating zones are simplified. 石墨材料结构的隔热屏和加热元件,担负了真空炉种类的重要部分。合理结构的加 热室石墨隔热屏与金属屏相比,以较低的热量损失为特点。对于典型尺寸的炉子, 2在炉温1200摄氏度时热损失是6-7.5 kW/m。 实际上炉子使用了10年,不会改变 这个热损失水平,这一点有别于金属隔热屏。因此石墨隔热屏的温度分布保障与炉 子最初检测是一样的精确,简化解决了对加热区域的要求。 9 Photo. 4 Seco/Warwick 2.OVPT-4050/48HV vacuum furnace with a graphite heating chamber. 照片4 赛科/沃克2.OVPT-4050/48HV型带有石墨 隔热屏加热室的真空炉 In the design of Seco/Warwick vacuum furnaces with graphite insulation, heating chambers of a cylindrical configuration with curve graphite heating elements are used o 360around the charge. 赛科/沃克设计的带有石墨隔热屏的真空 炉,圆柱形加热室、带有片状弧形石墨加 热元件(在工件周围360度分布)。 The cylindrical hot zones provide better and more consistent temperature uniformity over long period of time (according to AMS 2750D class 1 requirements) compare to rectangular chambers with rod or tube heating elements especially after prolong usage. 与带有棒/管状加热元件的矩形加热室相比,圆柱形加热室提供更好的温度均匀性 (根据AMS2750D级别1类要求),尤其炉子在长期使用后(更明显)。 Moreover: 此外 , wide and light heating elements make it possible to heat the charge with very 2 low surface loads [W/cm]. Unlike the solutions with rod heating systems generally in use in Europe, this ensures that the above-mentioned "close connection" of the non-uniform approach of the temperature of the charge to the holding temperature is attained, which is more often required in rapid heating processes; 2 宽而轻的加热元件可以用非常低的表面负荷[W/cm]加热工件。不像欧洲现 在通常使用的棒状加热系统,这确保了使上述非均匀温度的工件密切衔接以 获得保温的温度,此点在快速加热过程中常常需要。 , a very light heating system makes possible a high rate of heating and cooling of the charge, fulfilling the requirement for heating with speeds in the range of 0of 40C/min. 0非常轻的加热系统能够高效率地加热和冷却工件,实现40C/min加热速 度的要求。 , good access to the heating chamber area during loading in and loading out. Work with additional charge thermo elements is also facilitated. 在装料/卸料时,工件进/出加热室。也安装附加的加热元件。 , circular construction of the heating chamber is relatively stable during the heating and cooling cycles over a period of long-term utilization of the furnace. 炉子在加热和冷却周期中长时期使用后,加热室的圆形结构仍是稳定的。 10 In conjunction with constant technological development in the aerospace industry field, the requirements set for equipment for heat treatment have increased, particularly in the area of temperature uniformity precision, the repeatability of results, and the proper archivization of results. Much attention is also being given to processes for facilitating the attainment of the proper balance between advanced technologies and their economic aspects. This places new demands in the coming years on the suppliers of vacuum furnaces, and it creates the need to adapt furnace design to the changing requirements and expectations of the market. 配合航空工业领域技术的不断发展,对热处理设备的要求也相应提高,特别在 温度均匀性精度、热处理结果的重复性上、以及适当的其结果编档保存方面。 人们更关注设备程序上要达到技术先进,和其经济上合理的平衡。近几年真空 炉的制造商将这些作为新的要求,迎合对炉子设计的改进和市场的期望,而创 造出相应的提高。 Literature: 文摘 1. J. Olejnik "Seco/Warwick Vacuum Furnaces for the Aerospace and Energy Industry". DVIGATIEL No 5 (23) 2002 pp. 34-37. J. Olejnik“航空和能源工业应用的赛科/沃克真空炉” DVIGATIEL No 5 (23) 2002 pp. 34-37. 11 12
/
本文档为【NADCAP依据AMS2750D 标准对真空热处理温度均匀性的新要求(1)】,请使用软件OFFICE或WPS软件打开。作品中的文字与图均可以修改和编辑, 图片更改请在作品中右键图片并更换,文字修改请直接点击文字进行修改,也可以新增和删除文档中的内容。
[版权声明] 本站所有资料为用户分享产生,若发现您的权利被侵害,请联系客服邮件isharekefu@iask.cn,我们尽快处理。 本作品所展示的图片、画像、字体、音乐的版权可能需版权方额外授权,请谨慎使用。 网站提供的党政主题相关内容(国旗、国徽、党徽..)目的在于配合国家政策宣传,仅限个人学习分享使用,禁止用于任何广告和商用目的。

历史搜索

    清空历史搜索