阅读说明：本技术 具有由钼-碳化钛复合材料制成的接合层的陶瓷材料复合体、部件、燃气涡轮机和方法 (Ceramic material composite body with a bonding layer made of a molybdenum-titanium carbide composite material, component, gas turbine and method ) 是由 J·D·延森 O·施蒂尔 G·温克勒 于 2019-01-14 设计创作，主要内容包括：本发明涉及材料复合体(1),其具有第一层(2)和布置在第一层(2)上的第二层(3),所述第一层至少由陶瓷第一材料形成,所述第二层至少由不同于第一材料的陶瓷第二材料形成。为了实现更高的可热负荷性和/或可机械负荷性,设置了布置在第一层(2)和第二层(3)之间并且至少部分由钼-碳化钛复合材料形成的接合层(4),通过该接合层将第一层(2)与第二层(3)接合。(The invention relates to a composite body (1) comprising a first layer (2) which is formed from at least a first ceramic material and a second layer (3) which is arranged on the first layer (2) and which is formed from at least a second ceramic material which is different from the first material. In order to achieve a higher thermal and/or mechanical load-bearing capacity, a bonding layer (4) which is arranged between the first layer (2) and the second layer (3) and is formed at least partially from a molybdenum/titanium carbide composite is provided, by means of which bonding layer the first layer (2) is bonded to the second layer (3).)