公开(公告)号：US20110113785A1

公开(公告)日：2011-05-19

申请号：US12852788

申请日：2010-08-09

申请人： Remigi TSCHUOR ,  Russell Bond JONES ,  Nilze Isabel SEDA-MAURELL ,  Marion Oneil DUGGANS

发明人： Remigi TSCHUOR ,  Russell Bond JONES ,  Nilze Isabel SEDA-MAURELL ,  Marion Oneil DUGGANS

IPC分类号： F02C1/00 ,  B23P17/00

CPC分类号： F01D9/023 ,  F05D2230/232 ,  F05D2260/36 ,  F05D2260/94 ,  F05D2260/941 ,  F23R3/002 ,  F23R3/50 ,  F23R2900/00017 ,  Y10T29/49229

摘要： A thermal machine is provided, in particular a gas turbine, which includes an annular combustion chamber which is bounded on the outside by an outer shell and an inner shell. The outer shell and the inner shell are each split on a separating plane into an upper half and a lower half, which are mechanically interlocked by welding one to the other on the separating plane. Increased mechanical robustness and a longer life of the combustion chamber are achieved in that an additional mechanical interlock is provided on the separating planes in order to absorb tensile and shear forces acting on the separating planes.

摘要翻译： 提供一种热机，特别是一种燃气轮机，其包括通过外壳和内壳在外部限定的环形燃烧室。 外壳和内壳分别在分离平面上分成上半部分和下半部分，它们通过在分离平面上彼此焊接而机械联锁。 通过在分离平面上提供额外的机械联锁，以吸收作用在分离平面上的拉伸和剪切力，实现燃烧室的机械坚固性和寿命更长。

公开(公告)号：US20110135451A1

公开(公告)日：2011-06-09

申请号：US12857131

申请日：2010-08-16

申请人： Remigi TSCHUOR ,  Russell Bond JONES ,  Luis J. RODRIGUEZ ,  Hartmut HAEHNLE ,  Marion Oneil DUGGANS

发明人： Remigi TSCHUOR ,  Russell Bond JONES ,  Luis J. RODRIGUEZ ,  Hartmut HAEHNLE ,  Marion Oneil DUGGANS

IPC分类号： F01D11/00 ,  F01D5/08

CPC分类号： F01D9/023 ,  F02C7/28 ,  F05D2240/55 ,  F05D2250/42

摘要： A gas turbine includes a turbine section; an annular combustor disposed upstream of the turbine section and configured to discharge a hot gas flow on an outlet side to the turbine section; an outer shell delimiting the combustor and splittable at a parting plane; a plenum enclosing the outer shell; a rotor; a turbine vane carrier encompassing the rotor; a plurality of stator vanes disposed on the vane carrier, and at least two sealing segments forming a ring, each of the at least two sealing segments having an inner edge and a head and a foot section and being movably mounted on the inner edge by the foot section to the outer shell and by the head section to the turbine vane carrier so as to mechanically connect the combustor to the turbine vane carrier.

摘要翻译： 燃气轮机包括涡轮部分; 设置在所述涡轮部分的上游并且被配置为将出口侧的热气流排放到所述涡轮部分的环形燃烧器; 外壳限定燃烧器并在分型平面处可分开; 包围外壳的增压室; 转子 包围转子的涡轮叶片载体; 设置在所述叶片载体上的多个定子叶片和形成环的至少两个密封段，所述至少两个密封段中的每一个具有内边缘和头部和脚部，并且可移动地安装在所述内边缘上 脚部到外壳，并且通过头部到达涡轮叶片载体，以便将燃烧器机械地连接到涡轮叶片载体。