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7 条记录 (耗时 0.012 秒)

    Method for producing metallic articles having durable ceramic thermal barrier coatings
    3.
    发明授权
    Method for producing metallic articles having durable ceramic thermal barrier coatings 失效
    具有耐用陶瓷热障涂层的金属制品的制造方法

    公开(公告)号：US4405660A

    公开(公告)日：1983-09-20

    申请号：US327376

    申请日：1981-12-04

    申请人： Nicholas E. Ulion ,  Duane L. Ruckle

    发明人： Nicholas E. Ulion ,  Duane L. Ruckle

    IPC分类号： C23C14/02 ,  C23C14/08 ,  F01D5/28 ,  C23C11/00 ,  C23C13/00

    CPC分类号： F01D5/284 ,  C23C14/024 ,  C23C14/025 ,  C23C14/028 ,  C23C14/083 ,  F05D2250/621

    摘要： A coated article and method for producing the coated article are described. The article is coated with a system which provides protection against oxidation and corrosion and which significantly reduces the substrate temperature. An MCrAlY layer is applied to the article to be protected and a columnar grain ceramic is applied by vapor deposition to the MCrAlY coated article. An alumina layer which exists between the MCrAlY layer and the columnar ceramic layer provides for the adherence of the columnar layer to the MCrAlY layer. An important feature of the invention is that the interface between the MCrAlY layer and the alumina layer has a low surface roughness and this greatly improves the columnar ceramic layer adherence.

    摘要翻译： 描述了涂覆制品和用于生产涂层制品的方法。 该制品被涂覆有提供防止氧化和腐蚀并且显着降低基材温度的系统。 将MCrAlY层施加到待保护的制品上，并通过气相沉积将圆柱状晶粒陶瓷施加到MCrAlY涂覆制品上。 存在于MCrAlY层和柱状陶瓷层之间的氧化铝层提供了柱状层与MCrAlY层的粘附。 本发明的一个重要特征是MCrAlY层与氧化铝层之间的界面具有较低的表面粗糙度，极大地提高了柱状陶瓷层的粘附性。

    Method for heat treating cast titanium articles to improve their mechanical properties
    4.
    发明授权
    Method for heat treating cast titanium articles to improve their mechanical properties 失效
    用于热处理铸钛制品以提高其机械性能的方法

    公开(公告)号：US4631092A

    公开(公告)日：1986-12-23

    申请号：US662212

    申请日：1984-10-18

    申请人： Duane L. Ruckle ,  Ponciano P. Millan, Jr.

    发明人： Duane L. Ruckle ,  Ponciano P. Millan, Jr.

    IPC分类号： C22C14/00 ,  C22F1/00 ,  C22F1/18 ,  F01D5/28

    CPC分类号： C22F1/183 ,  Y10T29/49336

    摘要： Cast titanium alloys and a method of heat treating the alloys in order to obtain fatigue and mechanical properties comparable to wrought titanium is disclosed. The heat treatment is practiced by solution heat treating a cast titanium article above its beta transus, rapidly cooling, stabilizing at a temperature within the alloy's alpha/beta phase range, and finally aging the article to achieve the desired properties.

    摘要翻译： 公开了铸造钛合金和热处理合金以获得与锻造钛相当的疲劳和机械性能的方法。 热处理是通过在其β转子上方的铸造钛制品进行固溶热处理，快速冷却，在合金的α/β相范围内的温度下稳定化，最后使制品老化以达到所需的性能。

    Quench-cracked ceramic thermal barrier coatings
    5.
    发明授权
    Quench-cracked ceramic thermal barrier coatings 失效
    淬火裂纹陶瓷热障涂层

    公开(公告)号：US4457948A

    公开(公告)日：1984-07-03

    申请号：US401689

    申请日：1982-07-26

    申请人： Duane L. Ruckle ,  David S. Duvall

    发明人： Duane L. Ruckle ,  David S. Duvall

    IPC分类号： C04B38/00 ,  C23C4/18 ,  B05D1/08

    CPC分类号： C04B38/00 ,  C23C4/18 ,  Y02T50/67

    摘要： Plasma flame sprayed ceramic thermal barrier coatings on metal substrates are treated to make the coatings resistant to damage from thermal cycling. The coating and substrate are heated to a temperature in the range of 820.degree.-1150.degree. C. then are quenched in a medium capable of producing a surface heat flux of at least 1.3.times.10.sup.5 watts/m.sup.2. This causes creation of a fine network of cracks extending from the surface of the coating to the surface of the substrate whereby during thermal cycling, buildup of damaging stresses at the coating-substrate interface is avoided.

    摘要翻译： 对金属基底上的等离子火焰喷涂陶瓷热障涂层进行处理，使涂层耐热循环损伤。 将涂层和基材加热至820°-1150℃的温度，然后在能够产生至少1.3×10 5瓦特/平方米的表面热通量的介质中淬火。 这导致产生从涂层表面延伸到衬底表面的细小的裂缝网络，由此在热循环期间，避免了涂层 - 衬底界面处的损伤应力的积累。

    Diffusion bonding of titanium alloys with hydrogen-assisted phase transformation
    6.
    发明授权
    Diffusion bonding of titanium alloys with hydrogen-assisted phase transformation 失效
    钛合金与氢辅助相变的扩散结合

    公开(公告)号：US4982893A

    公开(公告)日：1991-01-08

    申请号：US394708

    申请日：1989-08-15

    申请人： Duane L. Ruckle ,  Thomas E. Strangman ,  Robert J. Keiser

    发明人： Duane L. Ruckle ,  Thomas E. Strangman ,  Robert J. Keiser

    IPC分类号： B23K20/00 ,  B23K20/22 ,  B23K20/233

    CPC分类号： B23K20/22 ,  B23K20/233

    摘要： A piece of a titanium-base alloy having an elevated temperature phase transformation is diffusion bonded to a second phase at an accelerated rate or reduced temperature, as compared with conventional diffusion bonding, by manipulating the phase transformation with an alloying element that can be readily introduced into, and removed from, the titanium piece. The introduction of hydrogen into the titanium alloy reduces the temperature of the phase transformation. The titanium alloy can be repeatedly cycled through the phase transformation before or during bonding, by the introduction and removal of hydrogen, to reduce the flow stress through transformation plasticity. Alternatively, the titanium alloy may be loaded with hydrogen to reduce the phase transformation temperature, increasing the fraction of the more deformable phase and then reducing the flow stress of the alloy at the diffusion bonding temperature.

    摘要翻译： 与常规的扩散接合相比，具有高温相变的一片钛基合金通过用易于引入的合金元素进行相变来与加速速率或降低的温度扩散接合到第二相 进入和移出钛片。 在钛合金中引入氢降低了相变的温度。 通过引入和除去氢，钛合金可以在结合之前或期间通过相变重复循环，以通过转变可塑性降低流动应力。 或者，钛合金可以加载氢以降低相变温度，增加更易变形相的分数，然后在扩散接合温度下降低合金的流动应力。

    Fatigue resistant nickel superalloy
    7.
    发明授权
    Fatigue resistant nickel superalloy 失效
    耐疲劳镍超合金

    公开(公告)号：US4325756A

    公开(公告)日：1982-04-20

    申请号：US115655

    申请日：1980-01-28

    申请人： Edgar E. Brown ,  Duane L. Ruckle

    发明人： Edgar E. Brown ,  Duane L. Ruckle

    IPC分类号： C22C19/03

    CPC分类号： C22C19/03

    摘要： Disclosed is a nickel base alloy of the gamma-gamma prime type, the composition of which is controlled, to provide a gamma matrix phase in which solid solution hardener elements are minimized, to less than 12.5 weight percent. Preferably, the alloy consists essentially by weight percent of 0.25-9Al, 1-4Ti, 2-6Cb, 0.01-0.1C, at least one material selected from the group consisting by weight percent of 0-6Co, 0-6Mo, 2-7.5Cr, 0-2.5Hf and mixtures thereof, balance nickel. The gamma prime fraction in a heat treated article is in the range 10-45 volume percent. The stacking fault energy is preferably in the range 80-120 ergs/cm.sup.2. A gas turbine engine disc made of the material exhibits a three fold increase in fatigue life in the 550-750.degree. C. range, as compared to discs made of typical superalloys in current use, while retaining comparable tensile and stress rupture strength.

    摘要翻译： 公开了一种γ-γ基型的镍基合金，其组成被控制，以使固溶固化剂元素最小化的γ基质相小于12.5重量％。 优选地，合金基本上由0.25-9Al，1-4Ti，2-6Cb，0.01-1.1C的重量百分比组成，选自0-6Co，0-6Mo，2- 7.5Cr，0-2.5Hf及其混合物，其余为镍。 热处理制品中的伽马质量分数在10-45体积％的范围内。 堆垛层错能最好在80-120 ergs / cm2范围内。 与当前使用的典型超级合金制成的圆盘相比，由该材料制成的燃气涡轮发动机圆盘在550-750℃范围内的疲劳寿命显示出三倍的增加，同时保持相当的拉伸和应力断裂强度。