For a gas turbine (2) exhaust diffuser (1) comprises a tubular transition sheath (5), the transition sheath (5) having: a central axis (10); having a circular cross section and to be connected to the turbine (2 ) downstream of the inlet end of the sheath (6); and to be connected...
A gas turbine exhaust diffuser includes a frustoconical portion that defines an interior surface and an axial centerline. In particular embodiments, the interior surface may have a slope greater than 6 degrees, 10 degrees, or 20 degrees with respect to the axial centerline to define an axial cro...
A gas turbine exhaust diffuser includes a frustoconical portion that defines an interior surface and an axial centerline. In particular embodiments, the interior surface may have a
摘要: PROBLEM TO BE SOLVED: To provide an exhaust diffuser of a gas turbine for lengthening the service life by restraining thermal stress with an economical and simple structure, without requiring study of a design change in a gas turbine facility....
摘要: PROBLEM TO BE SOLVED: To provide an exhaust diffuser of a gas turbine enabling the increase of a low cycle fatigue life by reducing a difference in heat capacity between an exhaust cylinder cylindrical part and an exhaust outside cylindrical part....
Exhaust gas diffuser for a gas turbine and a method for operating a gas turbine that comprises such an exhaust gas diffuser 本发明涉及一种用于燃气轮机(1)的排气扩散器(20),所述排气扩散器具有用于引导扩散流(30)的环形的外壁(28),在所述外壁中设有同心于外壁(28)设置的,用于影响扩散流(30)......
燃气涡轮机排气扩散器及其排气框架本实用新型提供一种燃气涡轮机排气扩散器及其排气框架,所述燃气涡轮机排气框架包括内部套筒和外部套筒,以在所述内部套筒和所述外部套筒之间形成环形排气流通道. The utility model provides a gas turbine exhaust diffuser and exhaust frame, the gas turbine exhaust frame includes ...
专利内容由知识产权出版社提供 专利名称:EXHAUST GAS DIFFUSER 发明人:Deepesh Dinesh Nanda 申请号:US12579637 申请日:20091015 公开号:US20110088379A1 公开日:201104 21 专利附图: 摘要:An exhaust gas diffuser includes a center body having an inlet adapted for coupling to a gas turbine, an outer wall,...
摘要: PROBLEM TO BE SOLVED: To provide a gas turbine not to reduce mounting precision of an exhaust diffuser with respect to the axis of the gas turbine and to facilitate assembly and to enable reduction of a cost even in a case of a small gas turbine having no surplus in a space....
United States Patent US9115602 Note: If you have problems viewing the PDF, please make sure you have the latest version ofAdobe Acrobat. Back to full text