公开(公告)号：US20110214430A1

公开(公告)日：2011-09-08

申请号：US13030288

申请日：2011-02-18

申请人： Ernst Pauli ,  Alexander Derksen

发明人： Ernst Pauli ,  Alexander Derksen

IPC分类号： F02C1/00 ,  F02C7/12

CPC分类号： F02C7/12 ,  F01D21/06 ,  F01D25/08

摘要： In a method for the fast cooling down of a gas turbine (1) after its operation, and also in a gas turbine (1) useful for carrying out the method, subsequent to the operation of a gas turbine (1), the rotor (8) is operated at low cooling speed (n) in order to cool down the gas turbine (1) which is heated up as a result of operation. This allows service or maintenance operations to be started early and therefore to reduce the shutdown periods of a gas turbine (1). After the operation of the gas turbine (1), cooling is not carried out a constant low cooling speed (n), but the cooling speed (n) is controlled as a function of at least one critical temperature (Tk) and/or of time (t). The cooling speed (n) in this case, in dependence upon the critical temperature (Tk), is kept as high as the resulting thermal and/or cyclic load allows for realizing a fast cool-down.

摘要翻译： 在用于燃气轮机（1）在其运行之后快速冷却的方法以及在用于执行该方法的燃气轮机（1）中，在燃气轮机（1）的操作之后，转子 8）以低冷却速度（n）运行，以便冷却由于操作而被加热的燃气轮机（1）。 这允许提前启动维修或维护操作，从而减少燃气轮机（1）的停机时间。 在燃气轮机（1）的运转之后，冷却不进行恒定的低冷却速度（n），但是冷却速度（n）被控制为至少一个临界温度（Tk）和/或 时间（t）。 在这种情况下，根据临界温度（Tk）的冷却速度（n）保持高达所得到的热和/或循环负载允许实现快速冷却。