公开(公告)号：US20110189026A1

公开(公告)日：2011-08-04

申请号：US12739929

申请日：2008-10-18

Applicant: Wilfried Smarsly ,  Helmut Clemens ,  Volker Guether ,  Sascha Kremmer ,  Andreas Otto ,  Harald Chladil

Inventor： Wilfried Smarsly ,  Helmut Clemens ,  Volker Guether ,  Sascha Kremmer ,  Andreas Otto ,  Harald Chladil

IPC: F01D5/14 ,  C22C14/00 ,  C22C30/00 ,  B21D22/00

CPC classification number: C22C14/00 ,  C22F1/183

Abstract: A material for a gas turbine component, to be specific a titanium-aluminum-based alloy material, including at least titanium and aluminum. The material has a) in the range of room temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase with a proportion of the β/B2-Ti phase of at most 5% by volume, and b) in the range of the eutectoid temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase, with a proportion of the β/B2-Ti phase of at least 10% by volume.

Abstract translation: 用于燃气轮机部件的材料，特别是至少包括钛和铝的钛 - 铝基合金材料。 该材料具有a）在室温的范围内，bgr / / B-Ti相，α2-Ti3Al相和γ-TiAl相，其中bgr / B2-Ti相的比例最多为5％，通过 体积，b）在共析温度，＆Bgr / / B-Ti相，α2-Ti3Al相和γ-TiAl相的范围内，bgr / B-Ti相的比例至少为10 按体积计。

公开(公告)号：US08888461B2

公开(公告)日：2014-11-18

申请号：US12739929

申请日：2008-10-18

Applicant: Wilfried Smarsly ,  Helmut Clemens ,  Volker Guether ,  Sascha Kremmer ,  Andreas Otto ,  Harald Chladil

Inventor： Wilfried Smarsly ,  Helmut Clemens ,  Volker Guether ,  Sascha Kremmer ,  Andreas Otto ,  Harald Chladil

IPC: F01D5/14 ,  C22F1/18 ,  C22C14/00

CPC classification number: C22C14/00 ,  C22F1/183

Abstract: A material for a gas turbine component, to be specific a titanium-aluminum-based alloy material, including at least titanium and aluminum. The material has a) in the range of room temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase with a proportion of the β/B2-Ti phase of at most 5% by volume, and b) in the range of the eutectoid temperature, the β/B2-Ti phase, the α2-Ti3Al phase and the γ-TiAl phase, with a proportion of the β/B2-Ti phase of at least 10% by volume.

Abstract translation: 用于燃气轮机部件的材料，特别是至少包括钛和铝的钛 - 铝基合金材料。 该材料具有a）在室温的范围内，bgr / / B-Ti相，α2-Ti3Al相和γ-TiAl相，其中bgr / B2-Ti相的比例最多为5％，通过 体积，b）在共析温度，＆Bgr / / B-Ti相，α2-Ti3Al相和γ-TiAl相的范围内，bgr / B-Ti相的比例至少为10 按体积计。

公开(公告)号：US6057031A

公开(公告)日：2000-05-02

申请号：US137815

申请日：1998-08-21

Applicant: Frank Breme ,  Volker Guether ,  Karl-Uwe van Osten

Inventor： Frank Breme ,  Volker Guether ,  Karl-Uwe van Osten

IPC: A61L27/00 ,  B32B9/00 ,  C23C16/02 ,  C23C16/18 ,  C23C16/30 ,  C23C30/00 ,  B32B18/00 ,  B32B27/32 ,  B32B27/34 ,  B32B27/36 ,  B32B27/40

CPC classification number: C23C16/30 ,  C23C16/029 ,  C23C16/18 ,  Y10T428/265 ,  Y10T428/3154 ,  Y10T428/31544 ,  Y10T428/31609 ,  Y10T428/31681 ,  Y10T428/31692 ,  Y10T428/31765 ,  Y10T428/31786 ,  Y10T428/31855

Abstract: The invention relates to a composite composed of a plastic substrate and a thin, continuous metal-containing layer, characterised in that the metal-containing layer is ductile, adheres firmly to the plastic substrate, has a thickness of

Abstract translation: 本发明涉及一种由塑料基材和薄的连续的含金属层组成的复合材料，其特征在于含金属层具有延展性，牢固地粘附在塑料基材上，厚度<2μm，由 的化合物对应于式M a O b C x N y B z，其中M表示包含Ti，Ta，Nb，Zr和Hf的一种或多种金属，a = 0.025至0.9b = 0.025至0.7x = 0.2至0.9y = 0至0.7z = 0至0.7a + b + x + y + z = 1，条件是从基板表面开始的a的值从接近于零的值向层表面增加，并且至少50％的碳原子在 该基底通过CC键与其它碳原子结合。