02-01-2014 дата публикации
Номер: US20140000380A1
Принадлежит:
A method is provided for measuring geometry deformations of a turbine component, rotor groove or blade root. The method includes providing the turbine component, rotor groove or blade root, respectively, with at least one measuring mark; using the at least one mark as a reference point in determining, in a first measurement, a length on the turbine component or rotor groove or blade root, respectively, before placing the turbine into service. The method also includes operating the turbine for a period of time; determining, in a second measurement, the length on the turbine component, rotor groove or blade root, using the at least one measuring mark as a reference point, after said operating period; comparing the measured lengths of the first and second measurements; and determining an amount of creep deformation in the turbine component, rotor groove or blade root, respectively, based on a difference between the measured lengths. 114. A method for measuring geometry deformations of a turbine component () , rotor groove or blade root , the method comprising the steps of:{'b': 14', '20, 'providing the turbine component (), or rotor groove or blade root, respectively, with at least one measuring mark ();'}{'b': 20', '1', '2', '14, 'using the at least one measuring mark () as a reference point in determining, in a first measurement, a length (L, L) on said turbine component () or rotor groove or blade root, respectively, prior to the turbine being placed into service;'}operating the turbine for a period of time;{'b': 1', '2', '14', '20, 'determining, in a second measurement, said length (L, L) on said turbine component () or rotor groove or blade root, respectively, using again said at least one measuring mark () as a reference point, after said operating period;'}{'b': 1', '2, 'comparing the measured lengths (L, L) of said first and second measurements; and'}{'b': '14', 'determining an amount of creep deformation in said turbine component () or rotor groove or blade ...
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