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    • 7. 发明申请
    • THERMAL BARRIER COATING SYSTEM AND METHOD FOR THE PRODUCTION THEREOF
    • 热障涂层系统及其生产方法
    • US20110244216A1
    • 2011-10-06
    • US12735609
    • 2009-01-29
    • Alexandra MeyerHolger KassnerRobert VassenDetlev StoeverJose-Luis Marques-Lopez
    • Alexandra MeyerHolger KassnerRobert VassenDetlev StoeverJose-Luis Marques-Lopez
    • B32B3/26C23C4/00C23C4/10
    • C23C28/36C23C4/11C23C4/134C23C28/322C23C28/345C23C28/3455Y10T428/249981
    • Disclosed is a method for producing a coating system on a component, wherein at least one coating is deposited on the component by way of atmospheric plasma spraying (APS) and at least one further coating is deposited by way of suspension plasma spraying (SPS). The coatings are particularly advantageously deposited in the sequence of APS+SPS or APS+SPS+APS or APS+SPS+erosion coating. These sequences of coatings applied in this way usually have an effect providing a first porous coating and a second porous coating disposed thereon, wherein the porosity of the second coating is greater than that of the first coating, and wherein the reflectivity is greater than that of the first coating. The increased reflectivity of the coating, particularly in the visible (VIS) and the near infrared (NIR) wavelength ranges, advantageously causes a lower thermal load for the substrate material because a smaller proportion of thermal radiation penetrates the ceramic thermal barrier coating, resulting in lower heating of the substrate (component).
    • 公开了一种在组分上制备涂料体系的方法,其中通过大气等离子体喷涂(APS)将至少一层涂料沉积在该组分上,并且通过悬浮等离子体喷涂(SPS)沉积至少一种另外的涂层。 涂层特别有利地以APS + SPS或APS + SPS + APS或APS + SPS +侵蚀涂层的顺序沉积。 以这种方式施用的这些涂层序列通常具有提供第一多孔涂层和设置在其上的第二多孔涂层的效果,其中第二涂层的孔隙率大于第一涂层的孔隙率,并且其中反射率大于 第一次涂层。 特别是在可见光(VIS)和近红外(NIR)波长范围内,涂层的增加的反射率有利地导致基底材料的较低的热负荷,因为较小比例的热辐射穿透陶瓷热障涂层,导致 较低的基板(部件)加热。
    • 9. 发明申请
    • Heat-Insulating Material, Production Method and Use Thereof
    • 绝热材料,生产方法和用途
    • US20080277618A1
    • 2008-11-13
    • US11886308
    • 2006-02-11
    • Gerhard PrachtRobert VassenDetlev Stover
    • Gerhard PrachtRobert VassenDetlev Stover
    • E04B1/74
    • C04B35/44C04B35/01C04B35/2675C04B35/62655C04B2235/3203C04B2235/3224C04B2235/3227C04B2235/3286C04B2235/761C04B2235/767C04B2235/80
    • The invention relates to a heat-insulating material, which is phase-stable particularly for high temperatures above 1150° C., especially above 1200° C., and which has a very good long-time stability. The heat-insulating material can exist in a number of phases of which at least one has the magnetoplumbite structure and stoichiometrically contains 0.1 to 10 mol % M12O3, 0.1 to 10 mol % Li2O and, as the remaining, M22O3 with incidental impurities. M1 is selected from the following elements: lanthanum, neodymium and gadolinium or mixtures thereof, and M2 is selected from the following elements: aluminum, gallium, iron or a mixture thereof. A particularly advantageous composition arises for this phase with the composition LaLiAl11O18.5 or LaLi0.5Al11.5O19. By using conventional methods, the heat-insulating material can be applied to the components subjected to a high level of thermal stress, for example, turbine blades. It is suited as a heat-insulating layer alone as well as for use in a composite material together with YSZ. The segmentation cracks regularly occurring in this heat-insulating material contribute significantly to a reduction in stresses between the heat-insulating layer and the coated component in the event of frequent alternating stresses.
    • 本发明涉及一种隔热材料,其特别是在高于1150℃,特别是高于1200℃的高温下是相稳定的,并且具有非常好的长时间稳定性。 隔热材料可以存在多个相,其中至少一个具有磁铅矿结构,并且化学计量地含有0.1至10摩尔%的M 2 O 3 O 3,0.1至 10mol%的Li 2 O 2,作为剩余的具有附带杂质的M 2 O 3 O 3。 M1选自以下元素:镧,钕和钆或其混合物,M2选自以下元素:铝,镓,铁或其混合物。 对于该组合​​物,组合物为LaLiAl 11 O 18.5或LaLi 0.5 Al 11 H 11 O,产生特别有利的组成, SUB> 19 。 通过使用常规方法,可以将绝热材料施加到受到高应力水平的部件,例如涡轮叶片。 它仅适用于隔热层,以及用于与YSZ一起的复合材料。 在这种绝热材料中经常发生的分割裂纹在频繁的交变应力的情况下显着地有助于降低隔热层和涂覆部件之间的应力。