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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M13/00—Testing of machine parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing 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.
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)
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)
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 |
-
1968
- 1968-05-25 DE DE19681773500 patent/DE1773500B2/en not_active Withdrawn
-
1969
- 1969-04-24 CH CH621769A patent/CH480627A/en not_active IP Right Cessation
- 1969-05-23 GB GB1226894D patent/GB1226894A/en not_active Expired
- 1969-06-26 US US827537A patent/US3603143A/en not_active Expired - Lifetime
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 |