-
1.发明公开
公开(公告)号：EP1496198A3
公开(公告)日：2005-01-19
申请号：EP04023742.2
申请日：2001-08-25
发明人： Oya, Takeaki, c/o Takasago Mach. Works , Hirokawa, Kazuharu, c/o Takasago Mach. Works , Tanioka, Tadateru, c/o Takasago Mach. Works , Tanaka, Katsunori, c/o Takasago Mach. Works , Uematsu, Kazuo, c/o Takasago Mach. Works , Shinohara, Tanehiro, c/o Takasago R. & Dvpt. Cen.
CPC分类号： F01D5/085 , F01D5/08 , F01D25/125 , F05D2240/61 , F05D2260/205 , F05D2260/2322
摘要： The invention refers to a bearing structure (24) for bearing a shaft portion (14) of a rotor tail end (10) of a gas turbine, comprising: a rotor assembly of the gas turbine having a center axis (0); rotor blades of the gas turbine; a steam passage (20) extending along the center axis for supplying and recovering a steam for cooling the rotor blades; a bearing pad (24a) which forms a journal bearing; and seal portions (26c) provided on opposite sides of the bearing pad in the axial direction to prevent leakage of a lubricant for lubricating a space between the bearing pad and the shaft portion, the width of said seal portion in the axial direction being such that the surface temperature of the shaft portion of the rotor tail end is maintained below a predetermined temperature by the lubricant, within the width of the bearing pad in the axial direction.
摘要翻译： 一种燃气轮机的转子尾端（10）的轴结构，其中用于供应和回收用于冷却燃气轮机的转子叶片的蒸汽的蒸汽通道（20）沿燃气轮机的转子组件的中心轴线延伸 其特征在于，在所述转子尾端部（10）上形成有与所述蒸汽通路的中心轴线同轴的转子尾端（10）的中心孔。 在蒸汽通道（20）和转子尾端（10）的中心孔（15）的内表面之间还设置有热套筒（16），从而形成绝热气体层（18） 在转子尾端（10）的中心孔的内表面和热套（16）之间。 绝热气体层（18）从外部气密地且液密地隔离。
-
公开(公告)号：EP1496198B1
公开(公告)日：2008-01-23
申请号：EP04023742.2
申请日：2001-08-25
发明人： Oya, Takeaki, c/o Takasago Mach. Works , Hirokawa, Kazuharu, c/o Takasago Mach. Works , Tanioka, Tadateru, c/o Takasago Mach. Works , Tanaka, Katsunori, c/o Takasago Mach. Works , Uematsu, Kazuo, c/o Takasago Mach. Works , Shinohara, Tanehiro, c/o Takasago R. & Dvpt. Cen.
CPC分类号： F01D5/085 , F01D5/08 , F01D25/125 , F05D2240/61 , F05D2260/205 , F05D2260/2322
-
3.发明公开Bearing structure for a steam cooled gas turbine 有权Wellen- und LageranordnungfüreinedampfgekühlteGurburbine
公开(公告)号：EP1496198A2
公开(公告)日：2005-01-12
申请号：EP04023742.2
申请日：2001-08-25
发明人： Oya, Takeaki, c/o Takasago Mach. Works , Hirokawa, Kazuharu, c/o Takasago Mach. Works , Tanioka, Tadateru, c/o Takasago Mach. Works , Tanaka, Katsunori, c/o Takasago Mach. Works , Uematsu, Kazuo, c/o Takasago Mach. Works , Shinohara, Tanehiro, c/o Takasago R. & Dvpt. Cen.
CPC分类号： F01D5/085 , F01D5/08 , F01D25/125 , F05D2240/61 , F05D2260/205 , F05D2260/2322
摘要： The invention refers to a bearing structure (24) for bearing a shaft portion (14) of a rotor tail end (10) of a gas turbine, comprising:
a rotor assembly of the gas turbine having a center axis (0);
rotor blades of the gas turbine;
a steam passage (20) extending along the center axis for supplying and recovering a steam for cooling the rotor blades;
a bearing pad (24a) which forms a journal bearing; and seal portions (26c) provided on opposite sides of the bearing pad in the axial direction to prevent leakage of a lubricant for lubricating a space between the bearing pad and the shaft portion, the width of said seal portion in the axial direction being such that the surface temperature of the shaft portion of the rotor tail end is maintained below a predetermined temperature by the lubricant, within the width of the bearing pad in the axial direction.摘要翻译： 本发明涉及一种用于承载燃气轮机的转子尾端（10）的轴部分（14）的轴承结构（24），包括：具有中心轴线（0）的燃气涡轮机的转子组件; 燃气轮机的转子叶片; 沿着中心轴线延伸的蒸汽通道（20），用于供应和回收用于冷却转子叶片的蒸汽; 轴承座（24a），其形成轴颈轴承; 以及沿轴向设置在所述轴承瓦的相对侧上的密封部（26c），以防止用于润滑轴承瓦块和轴部之间的空间的润滑剂的泄漏，所述密封部在轴向上的宽度使得 转子尾端的轴部的表面温度在轴向瓦块的宽度方向上通过润滑剂维持在规定温度以下。
-
公开(公告)号：EP1496197B1
公开(公告)日：2008-11-26
申请号：EP04023741.4
申请日：2001-08-25
发明人： Oya, Takeaki, c/o Takasago Mach. Works , Hirokawa, Kazuharu, c/o Takasago Mach. Works , Tanioka, Tadateru, c/o Takasago Mach. Works , Tanaka, Katsunori, c/o Takasago Mach. Works , Uematsu, Kazuo, c/o Takasago Mach. Works , Shinohara, Tanehiro, c/o Takasago Res. & Dvpt. Cen
CPC分类号： F01D5/085 , F01D5/08 , F01D25/125 , F05D2240/61 , F05D2260/205 , F05D2260/2322
-
5.发明公开
公开(公告)号：EP1496197A1
公开(公告)日：2005-01-12
申请号：EP04023741.4
申请日：2001-08-25
发明人： Oya, Takeaki, c/o Takasago Mach. Works , Hirokawa, Kazuharu, c/o Takasago Mach. Works , Tanioka, Tadateru, c/o Takasago Mach. Works , Tanaka, Katsunori, c/o Takasago Mach. Works , Uematsu, Kazuo, c/o Takasago Mach. Works , Shinohara, Tanehiro, c/o Takasago Res. & Dvpt. Cen
CPC分类号： F01D5/085 , F01D5/08 , F01D25/125 , F05D2240/61 , F05D2260/205 , F05D2260/2322
摘要： The invention refers to a shaft structure of a rotor tail (10) end of a gas turbine, comprising:
a rotor assembly of the gas turbine having a center axis (0); rotor blades of the gas turbine;
a steam passage extending along the center axis (0) for supplying and recovering a steam for cooling the rotor blades;
a plurality of shaft portion cooling air passages (31a,31b,31c) formed between the steam passage and an outer surface of a shaft portion (14) of the rotor tail end. Such a shaft structure according to the invention has practically no or at least little thermal deformation of the rotor tail end of the gas turbine.摘要翻译： 本发明涉及一种燃气轮机的转子尾部（10）端的轴结构，包括：具有中心轴线（0）的燃气轮机的转子组件; 燃气轮机的转子叶片; 沿着中心轴线（0）延伸的蒸汽通道，用于供应和回收用于冷却转子叶片的蒸汽; 形成在蒸汽通道与转子尾端的轴部（14）的外表面之间的多个轴部冷却空气通路（31a，31b，31c）。 根据本发明的这种轴结构实际上对于燃气轮机的转子尾端几乎没有或至少少量的热变形。
-
-
-
-
搜索结果
5 条记录 (耗时 0.011 秒)
