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1.
研究了W6Mo5Cr4V2高速钢圆刀片热处理后的组织,性能,与Cr12MoV刀片进行比较,寿命617-1000t/一次修磨,比日本进口刀片寿命略有提高。 相似文献
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研究了梯度结构硬质合金涂层刀片和无梯度结构硬质合金涂层刀片的切削性能.并对不同钴含量梯度结构硬质合金刀片的切削性能进行了对比实验。实验表明:具有梯度结构硬质合金涂层刀片的切削性能比无梯度结构硬质合金涂层刀片的切削性能优良;达到同一磨损高度hB=0.15mm时,前者的切削寿命较后者提高了近一倍;同时随着合金钴含量增多,硬质合金刀片的切削性能提高。 相似文献
3.
金属加工工业的发展要求采用高效率加工方法,提高工具寿命及切削速度,因此,当前改进硬质合金金属切削工具的主要方向之一是高效率的可转位刀片的推广应用。可转位刀片的应用可以省去刀片焊接及刀刃重磨等工序,消除工具制造过程中出现的裂纹及显微裂纹,从而大大地提高了切削工具的使用性能。缩短了工具的调整时间,降低了生产费用。装配国产可转位刀片的刀具在苏联的维 相似文献
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Co含量对硬质合金梯度结构和性能的影响 总被引:3,自引:1,他引:3
采用分段烧结的试验工艺,通过改变原料中钴的含量来研究钴含量对硬质合金梯度结构和性能的影响。试验主要从钴含量对梯度烧结后、涂层后合金的机械性能、梯度结构的变化情况进行了探索,并研究了梯度硬质合金刀片的切削性能。试验表明,随着合金钴含量增多,合金梯度结构越明显,梯度层厚度增加;合金的强度与磁饱和提高,硬度、磁力和密度减小。同时随着合金钴含量增多,经涂层处理的硬质合金刀片的切削性能提高,达到同一磨损高度VB=0.12mm时,FGCC-Co-8刀片的切削寿命较FGCC-Co-6刀片提高了三分之一。 相似文献
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《金属材料与冶金工程》1976,(3)
株洲硬质合金厂在生产斗争和科学实验中不断地总结经验,74年以来开始大批生产机夹刀片,75年产量已突破50吨大关,43个品种,24个规格。76年要在75年基础上实现翻番,突破100吨大关。与焊接刀片相比,机夹刀片有如下一些优点: 1.刀具不需焊接刃磨,完全避免了产生内应力和裂纹的可能性,因而刀具的寿命平均提高1~1.5倍。 相似文献
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《钢铁》1977,(3)
在毛主席“农业的根本出路在于机械化”的光辉教导指引下,北京钢铁研究院于1974年底接受了一机部委托的“关于提高收割机刀片使用寿命”的研究课题。1975年初即开展了这方面的工作。收割机刀片是易磨损、用量大的关键部件,原用T,高频感应淬火的刀片磨损快、寿命低,影响收割速度,误农时,远远满足不了农业大发展的需要。科技人员本着急广大贫下中农之所急,在课题一开展就坚持科研、生产、使用三结合,为贫下中农服务,在确定研究方案时尽力考虑到研究出来的刀片既经济、又耐用,为广大贫下中农所欢迎。首先将原来的刀片材料T_9冷轧带改为45号碳素结构钢冷轧带,并采用工艺简便、原料来源方便又便宜的液体渗硼工艺,进行定刀刃边渗硼处理,使刃口获 相似文献
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采用热常数仪和高温维氏硬度计对Co含量(质量分数)分别为6%和10%的硬质合金进行热学性能与高温力学性能检测,然后用以这2种硬质合金为基体的涂层刀片对镍基高温合金GH4133进行高速车削,采用扫描电镜(SEM)和能谱(EDS)对车削后刀片的磨损区域进行观察和成分分析,研究刀片基体的Co含量对刀具切削性能的影响。研究结果表明,硬质合金中的Co含量由10%降低到6%时,热导率由62.78(W.m)/K升高到84.57(W.m)/K,与此同时同一温度下的高温维氏硬度提高10%左右;YBG202刀片(基体中Co含量为10%)的切削刃与后刀面的磨损均较迅速,而YBG102(基体中的Co含量为6%)刀片后刀面的磨损相对均匀,磨损速率低;基体中的Co含量由10%降低到6%时,刀片的切削寿命提高约3倍。故高速连续切削镍基高温合金时应当尽量选用低Co硬质合金作为刀片的基体。 相似文献
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双卧轴强制式混凝土搅拌机是一种高效、快速的混凝土搅拌器械,广泛用于各种混凝土工程中。以某型号双卧轴强制式混凝土搅拌机为研究对象,根据磨料磨损机理推出搅拌叶片线磨损率的计算公式,通过Fluent软件的计算和相关后处理工作得出搅拌叶片表面线磨损率的分布。分析结果表明,搅拌叶片的顶端附近处线磨损率最大,磨损最为严重;根据线磨损率的数值可预估搅拌叶片的使用寿命。研究对于预估整机的使用寿命提供了一定的理论依据和数值依据,对搅拌臂的布局和搅拌叶片材料的选择和处理也提供了一定的科学依据。 相似文献
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William Oldfield Freda M. Oldfield 《Metallurgical and Materials Transactions A》1993,24(10):2313-2319
Surface-connected porosity in current military aircraft hot-stage turbine engine blades is associated with blade failure.
Oxidation ratcheting is suggested as the failure mechanism. Sta- tistical comparison of new and used blade populations showed
that for blades cast with an equiaxed structure, the porosity in new blades was associated with crack formation on the con-
cave surface of the used blades. The pores did not tend to develop into cracks on the compressed (convex) surface of the blade.
Insufficient suitable data on directionally solidified blades pre- vented similar statistical correlations. However, metallography
of the directionally solidified blades showed that the in-service cracks were related to oxidation inside surface-connected
pores and that the cracks were oriented in the same direction as the (axial) casting pores. Thus, the proposed failure mechanism
through ratcheting is based on the following insights: (1) the blades are thermally cycled as a normal part of service; (2)
the hot blades expand and the open pores are filled with oxide; (3) when the blade is cooled, thermal contraction of the metal
is greater than the oxide, causing compressive stress and yield; and (4) thermal expansion of the blades opens the pores again,
since yield relaxed compressive stress at low temperature. These insights were supported by metallographic and computer-simulation
studies which showed that the pores grow 20 to 50 pct in width per 100 missions (about 90 hours of operation) for a military
aircraft on a typical mission profile. 相似文献
13.
以多元少量的合金化原则设计的4Cr2WMoVSi钢是一种经济型热作模具钢,研究了4Cr2WMoVSi钢的热处理工艺及性能,并与3Cr2W8V钢的热处理工艺和性能作了对比,用4Cr2WMoVSi钢制作了热剪刃,进行了装机使用试验,其使用寿命与3Cr2WSV剪刃的寿命相当,而是5CrW2Si剪刃寿命的3.4倍。 相似文献
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Microstructure,creep properties,and rejuvenation of service-exposed alloy 713C turbine blades 总被引:1,自引:0,他引:1
T. M. Maccagno A. K. Koul J. -P. Immarigeon L. Cutler R. Allem G. L’espérance 《Metallurgical and Materials Transactions A》1990,21(12):3115-3125
A study was carried out on the microstructure and creep properties of aero engine first-stage turbine blades made from Alloy
713C nickel-base superalloy. Results are reported for new blades, blades in two service-exposed conditions, and service-exposed
blades subjected to one of three rejuvenation treatments: a recoating heat treatment, a hot isostatic pressing (HIP) + recoating
heat treatment, and a HIP + controlled cooling + recoating heat treatment. The blade microstructure undergoes significant
change during service, and this leads to a loss in creep properties exhibited by specimens machined from the blade airfoils.
Good correlations were observed between the rupture time and the amount of blade airfoil untwist and between the minimum creep
rate and the amount of untwist. The recoating heat treatment and the HIP + controlled cooling + recoating treatment were moderately
successful in restoring the microstructure and creep properties of the service-exposed blades. In comparison, the HIP + recoating
treatment was very successful in rejuvenating creep properties but only for blades having a chemical composition with a lower
propensity to form σ phase. For the blades with an unfavorable composition, σ phase was found to form preferentially near
the grain boundaries during creep testing, and this had a detrimental effect on the creep properties. Nonetheless, the degree
of rejuvenation for these blades was always at least as good as that obtained through the recoating heat treatment alone.
Formerly National Aeronautical Establishment 相似文献
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秦岭发电厂对本厂使用的12.5万千瓦和20万千瓦发电机组的排粉机叶片、引风机包头及防磨板、除尘器喷嘴喉部喷水管等部件进行了粉末喷焊。不仅延长了零部件的使用寿命、减少更换次数、保证安全发电和供电,而且一年之内节约直接资金达到338258元。应用该技术获得了显著的技术经济效益。 相似文献
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文中介绍风机叶片由原来采用钢板冲压成形、焊接而成,改为铝合金并应用激冷与微量元素锑复合变质后,不仅使叶片的内、外质量得到了保证,还大大提高了铸件的耐蚀性和使用寿命,降低了动力消耗和成本。 相似文献
18.
The Ni-base superalloys, which are normally melted and cast in a vacuum, entrain their surface-oxide film during turbulent pouring of the melt; unfortunately at this time, this process is universally practiced for investment castings of these materials. The entrained film becomes a bifilm crack automatically, so that cast alloys have a large population of cracks that controls their failure behavior. The problems of the growth of single crystals and the welding of polycrystalline alloys are reviewed to illustrate the central role of bifilms in the cracking of turbine blades, the heat-affected zones of welds, and the reliability of properties. It has been demonstrated that improved gravity pouring systems can reduce these problems significantly, but only countergravity filling of molds is expected to result in defect-free castings. Recent cases in which turbine blades failed in service are examined, and the central role of bifilm defects in these failures is discussed. 相似文献
19.
The problems of the fatigue life of gas-compressor unit blades are discussed. In particular, the results of fractographic investigation are used to formulate the specific features of fracture of stamped lowpressure turbine blades made of an EI893 alloy, which exhibit the maximum number of damages in a five-year period. In 80% cases, fracture begins with the formation of a brittle zone in the leading edge of a blade airfoil because of the resonance phenomena caused by a break in the stiffness of the blade–turbine disk joint. This conclusion is supported by pronounced traces of fretting corrosion in the contact surfaces of the joint of a failed blade and a disk. 相似文献
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龙首矿采用下向水平分层六角形进路充填采矿法,分层道是关键通道,其稳定性至关重要。应用FLAC3D软件建立了分层道及六角形进路数值模型,应用强度等效原则确定了分层道底部配筋充填体的力学参数。分别研究了分层道假顶为素充填体和配筋充填体情况下的稳定性。结果表明,分层道开挖暴露的大面积矩形薄板,最大挠曲在中部位置,破坏方式从中部开始拉断破坏,应在开采过程中加强对顶板的支护及对中部位置的监测。此外,分层道假顶为素充填体时不利于矿山的安全生产,尤其在进路与分层道交叉巷道处,应加密配筋密度,防止出现冒落及掉块现象。 相似文献