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GB1226894A - - Google Patents

Info

Publication number
GB1226894A
GB1226894A GB1226894DA GB1226894A GB 1226894 A GB1226894 A GB 1226894A GB 1226894D A GB1226894D A GB 1226894DA GB 1226894 A GB1226894 A GB 1226894A
Authority
GB
United Kingdom
Prior art keywords
blade
yoke
rotor segment
secured
root
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of GB1226894A publication Critical patent/GB1226894A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Turbines (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,226,894. Turbines. LICENTIA PATENTVERWALTUNGS - G. m. b. H. May 19, 1969 [May 25, 1968], No. 26526/69. Heading F1T. [Also in Division G2] A test rig for simulating the working loads acting on a steam turbine rotor blade 2 to enable examination of the behaviour at the connection between the blade root and the rotor periphery comprises an upper yoke 5 supported from a lower yoke 8 and a hydraulic device 15 for applying a tension force to the blade 2 and to a rotor segment 3 to which the blade is secured by a straddle type root fixing. The region of the fixing can be heated. The blade 2 is secured to the yoke 5 by welding the tip shroud 18 to a plate 19 which is bolted to the yoke 5. The rotor segment 3 is secured to a rod 4 which in turn is attached to a threaded tensioning rod 16 connected to hydraulic device 15. The rod 4 is guided in a bush 17 secured to yoke 8. The latter supports yoke 5 by way of sleeves 12, 14 and spring members 11, 13 consisting of stacks of metal and rubber sheets. The hydraulic device 15 can thus apply to the blade 2 and rotor segment 3 loads corresponding to the centrifugal loads experienced during turbine operation. Loads corresponding to axial and/or circumferential steam loads, depending on the position of the blade 2 in relation to the yoke 5, can be applied to the blade by a metal cable 31 having a loop 30 around the blade. The cable 31 is anchored at both ends and includes a spring 33, adjuster 32 and a device comprising a rotating disc 36 and an arm 35 for applying a cyclically varying force to the cable 31, e.g. at a frequency of 3 cycles/sec. A second such device may be provided at the other end of the cable 31 for applying a similar force in the opposite direction. Any slippage, tilting, or deformation of the blade root in relation to the rotor segment 3 can be detected by an optical system, Figs. 3, 4 (not shown), and dial gauges. The optical system comprises mirrors (20, 21) on the sides of the blade root and rotor segment respectively and a calibrated screen (23) upon which images of a light source (22) are reflected by the mirrors. If any relative movement between the root and rotor segment occurs, then the images on screen (23) move apart.
GB1226894D 1968-05-25 1969-05-23 Expired GB1226894A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19681773500 DE1773500B2 (en) 1968-05-25 1968-05-25 TEST DEVICE FOR DETERMINING THE FORCE CLOSURE AND DEFORMATION AND WEAKNESS POINTS OF THE BLADE FIXING OF TURBINE BLADES

Publications (1)

Publication Number Publication Date
GB1226894A true GB1226894A (en) 1971-03-31

Family

ID=5701711

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1226894D Expired GB1226894A (en) 1968-05-25 1969-05-23

Country Status (4)

Country Link
US (1) US3603143A (en)
CH (1) CH480627A (en)
DE (1) DE1773500B2 (en)
GB (1) GB1226894A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH514834A (en) * 1969-04-09 1971-10-31 Licentia Gmbh Test device for determining the force fit, deformation and weak points of the blade attachment of turbine blades
US3802255A (en) * 1972-03-08 1974-04-09 Us Air Force Fixture for tensile and stress rupture testing of turbine blades
DE3139864C2 (en) * 1981-10-07 1987-04-30 Daimler-Benz Ag, 7000 Stuttgart Method for determining the deformation of a valve train on an internal combustion engine
US6718833B2 (en) 2001-03-05 2004-04-13 Adtech Systems Research, Inc. Multiaxial high cycle fatigue test system
DE102005016307B4 (en) * 2005-04-09 2010-10-07 Mtu Aero Engines Gmbh Device for sample testing
US7668769B2 (en) * 2005-10-04 2010-02-23 Basepoint Analytics, LLC System and method of detecting fraud
GB0906342D0 (en) * 2009-04-15 2009-05-20 Rolls Royce Plc Apparatus and method for simulating lifetime of and/or stress experienced by a rotor blade and rotor disc fixture
EP3198255B1 (en) * 2014-09-26 2019-01-09 Vestas Wind Systems A/S Fatigue testing of a wind turbine blade
CN104792606A (en) * 2015-02-01 2015-07-22 山东科技大学 Anchor rod anchoring quality detection method
CN108426783B (en) * 2017-02-14 2020-08-07 中国石油天然气集团公司 Micro-shear test device
CN108279122B (en) * 2018-02-11 2023-08-01 厦门大学嘉庚学院 Spring riveting reliability testing device and using method
CN111398063B (en) * 2020-03-31 2021-04-27 中国地质大学(武汉) Prediction Method of Shear Load-Shear Displacement Curve of Anchor Joint Surface Based on Axial Dynamometer

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1409842A (en) * 1916-01-08 1922-03-14 Tinius Olsen Testing Mach Co Testing machine
US1485835A (en) * 1922-03-09 1924-03-04 Bothezat George De Machine for testing sheet metal for vibration
US2007286A (en) * 1932-05-25 1935-07-09 Schopper Alfred Flexure testing machine
US2496632A (en) * 1944-12-14 1950-02-07 Baldwin Locomotive Works Vibration testing apparatus
US2469346A (en) * 1945-06-14 1949-05-03 Budd Co Fatigue-testing machine
US2984110A (en) * 1955-02-12 1961-05-16 Simek Jiri Optical vibrometer
US2917918A (en) * 1956-10-03 1959-12-22 Jules E Jenkins Vibration measuring and recording apparatus

Also Published As

Publication number Publication date
DE1773500B2 (en) 1971-11-25
US3603143A (en) 1971-09-07
DE1773500A1 (en) 1970-11-12
CH480627A (en) 1969-10-31

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
435 Patent endorsed 'licences of right' on the date specified (sect. 35/1949)
PCNP Patent ceased through non-payment of renewal fee