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    • 4. 发明申请
    • METHOD FOR DETERMINING THE ADHESIVENESS OF A COATING ON A COMPONENT
    • 确定组分上涂层的粘合强度的方法
    • WO03008938A3
    • 2003-05-22
    • PCT/DE0202310
    • 2002-06-25
    • SIEMENS AGLAMPENSCHERF STEFAN
    • LAMPENSCHERF STEFAN
    • G01N3/02G01N19/04G01N33/32
    • G01N19/04G01N2203/0254G01N2203/0282
    • The invention relates to a method for determining the adhesiveness of a coating applied to a component (10), is characterised by the following steps: a) the coating (11) which is to be examined is reinforced locally by at least one additional coating (12) having at least one defined geometric parameter, preferably by several additional coatings with various thicknesses and surfaces; b) subsequently, the component (10) is subjected to a strain, whereby said strain is increased in the region of the local reinforcements (12); c) a quantitative and/or qualitative evaluation of the adhesiveness is carried out by means of an analysis method based on the locally increased strain in the region of the local reinforcement (12). Said method can be applied in an advantageous manner in close to real conditions for the component and without the need for additional test apparatus to be used.
    • 它是,除其他外,用于确定的粘合强度的成分(10)上位于所述的涂层(11)的方法,其特征在于以下步骤:a)将测试涂层(11)被至少一个辅助涂层(12),其具有至少 一个确定的几何参数,最好在局部增强的不同厚度和面积的几种附加涂层上; b)对所述部件(10),然后一个负载,其中在)局部增强的区域(12产生的负荷的正视图; c)以分析的方法是基于在局部增强(12)的区域中的过大的局部载荷进行的粘合强度的定量和/或定性评估。 在这种情况下,该方法可以有利地在组件的紧凑条件下并且不需要额外的测试设备来执行。
    • 5. 发明申请
    • GAS TURBINE ARRANGEMENT, POWER PLANT AND METHOD FOR THE OPERATION THEREOF
    • 燃气轮机装置,电厂和操作程序的
    • WO2013026702A3
    • 2013-05-02
    • PCT/EP2012065493
    • 2012-08-08
    • SIEMENS AGHAMMER THOMASLAMPENSCHERF STEFANPHAM GIA KHANHPICKARD ANDREAS
    • HAMMER THOMASLAMPENSCHERF STEFANPHAM GIA KHANHPICKARD ANDREAS
    • F02C6/18F01D15/10H01L35/30
    • H01L35/30F01D15/10F02C6/18F05D2220/64F05D2220/76
    • The invention relates to a gas turbine arrangement (10) for a power plant, having a compressor (12) for compressing combustion air, which compressor is coupled, by means of a shaft (22), to a turbine (20) which can be driven by combustion gases, wherein the combustion gases can be generated by combustion of fuel with the compressed combustion air, and also having an exhaust gas system (26) through which the combustion gases can, after passing through the turbine, be discharged into the atmosphere, characterized in that at least one thermoelectric generator (30) for generating electrical energy from the residual heat of the combustion gases is provided in the exhaust gas system. According to the invention, at least one thermoelectric generator for generating electrical energy from the residual heat of the combustion gases is provided in the exhaust gas system. Such a gas turbine arrangement allows waste heat from the combustion gases to be utilized and thus the overall efficiency of the gas turbine arrangement to be increased and the pollutant emissions thereof to be lowered.
    • 本发明涉及一种燃气涡轮机组件(10)的发电设备,其包括用于压缩燃烧用空气,压缩机(12),其通过一个轴装置(22)被耦合到一个涡轮机(20),其可以通过燃烧气体驱动,由燃烧产生的燃烧气体 的可以产生,以及与排气管线(26),通过该燃烧气体可以通过涡轮机到环境后发射,至少一个热电发生器(30),其特征在于,在排气系用于产生电与所述压缩的燃烧空气燃料 能量从燃烧气体的余热提供。 根据本发明,至少对于从在排气系统中所提供的燃烧气体的余热产生电能的热电发电机。 通过这样的燃气涡轮机布置的方法,从燃烧气体中的余热被使用,从而增加了燃气涡轮机组件的整体效率,降低了其Schadstoff¬放电。