Method and device for implementing simulated test of centrifugal stress in turbine blade

{
  "publication_number": "US2010288052A1",
  "country": "US",
  "kind": "A1",
  "title": "Method and device for implementing simulated test of centrifugal stress in turbine blade",
  "abstract": "The object is to provide a method and device to detect internal defect in the weld overlaid portion of erosion resistant material in the border portion between the blade profile and the shroud of a turbine blade with high accuracy by a static test method for an individual turbine blade applying a resultant pressing force, corresponding to centrifugal force and untwisting force of the turbine blade 10 in operation of the turbine, to the shroud 12 with installing the blade root 18 of the turbine blade 10 to the blade root retainer 20 and applying a force in the direction of centrifugal force on the blade root 18 from outside of the blade root retainer 20 to eliminate backlash between the blade root 18 and blade root retainer 20, retaining securely the shroud 12 on the side opposite to the portion which is applied the pressing force, and implementing simulated test of centrifugal stress in the weld-overlaid portion by applying the resultant pressing force, corresponding to centrifugal force and untwisting force of the turbine blade 10 in operation of the turbine, to the shroud 12.",
  "claims": [
    "1. A method of implementing simulated test of centrifugal stress in a turbine blade, which has a shroud on a tip of blade profile part of the turbine blade and a blade root on the attaching side to a turbine rotor with weld-overlaid portion on the border portion between the shroud an the tip of the blade for the purpose of simulating influence of centrifugal force on the weld-overlaid portion by using a test device, the method comprising; applying a resultant pressing force, corresponding to centrifugal force and untwisting force of the turbine blade in operation of the turbine, to the shroud on the weld-overlaid portion side with installing the blade root of the turbine blade to the blade root retainer and applying a force in the direction of centrifugal force on the blade root from outside of the blade root retainer to eliminate backlash between the blade root and blade root retainer, and retaining securely the shroud on the side opposite to the portion which is applied the pressing force. 2. A method of implementing simulated test of centrifugal stress in a turbine blade according to claim 1, wherein said weld-overlaid portion is formed on the working fluid entrance side, said resultant pressing force corresponding to centrifugal force and untwisting force of the turbine blade in operation of the turbine is applied to said working fluid entrance side of the shroud, and the working fluid exit side of the shroud is retained securely. 3. A method of implementing simulated test of centrifugal stress in a turbine blade according to claim 2, wherein said turbine blade has stubs formed on both sides at a longitudinal intermediate part of the blade, each stub being brought into contact with a stub of adjacent blade by untwisting force exerting on the turbine blades in operation of the turbine, and said pressing force is applied to the shroud in a state said stubs are retained securely. 4. A device for implementing simulated test of centrifugal stress in a turbine blade, which has a shroud on the tip of the blade profile part of the turbine blade and a blade root on the attaching side to a turbine rotor with weld-overlaid portion on the border portion between the shroud and the tip of the blade profile part of the turbine blade for the purpose of simulating influence of centrifugal stress on the weld-overlaid portion, the test device comprising; a blade root retainer, in which said blade root is installed, a first hydraulic device for applying a force in direction of centrifugal pressing force on the blade root from outside of the blade root retainer to eliminate backlash between the blade root and blade root retainer, a second hydraulic device for applying resultant pressing force corresponding to centrifugal force and untwisting force of the turbine blade in operation, to the shroud on the weld-overlaid portion side, a first retaining device for retaining securely the shroud on the side opposite to the portion which is applied the pressing force, and a first and second column supports extending parallel to the longitudinal direction of the turbine blade, which is installed on the blade root retainer, with said second hydraulic device and first retaining device attached respectively to each of the column supports, whereby stress created in the weld overlaid portion in operation of the steam turbine is simulated. 5. A device for implementing simulated test of centrifugal stress in a turbine blade according to claim 4, wherein said weld-overlaid portion is formed on the working fluid entrance side, said first retaining device is disposed at the working fluid exit side of the shroud, said second hydraulic device is disposed at the working fluid entrance side of the shroud such that it pushes the shroud in direction of force of centrifugal force and untwisting force of the turbine blade. 6. A device for implementing simulated test of centrifugal stress in a turbine blade according to claim 5, wherein said turbine blade has stubs formed on both sides at a longitudinal intermediate part of the blade, each stub being brought into contact with a stub of adjacent blade by untwisting force in the operation, and second retaining devices for securely retaining the stubs are attached to the first and second column supports respectively"
  ],
  "cpc": [
    "F01D 25/285",
    "F01D 25/00",
    "F01D 5/20",
    "F01D 5/22",
    "F05D 2260/94",
    "F05D 2270/114",
    "G01M 15/14"
  ],
  "assignees": [
    "TANAKA TAKESHI",
    "ASAKA HARUHIKO",
    "MICHINISHI JUNYA",
    "MIYAJIMA KEIICHIRO",
    "MORI KAZUSHI"
  ],
  "filing_date": "2010-03-24",
  "publication_date": "2010-11-18",
  "priority_date": "2009-05-12",
  "application_number": "US-73041610-A",
  "family_id": "43067411",
  "citations": [
    "US2006222490A1",
    "US5511948A",
    "US6250166B1",
    "US6718833B2"
  ]
}