CN104389641A - Forked blade root locking structure of moving blades in high-temperature section of steam turbine - Google Patents
Forked blade root locking structure of moving blades in high-temperature section of steam turbine Download PDFInfo
- Publication number
- CN104389641A CN104389641A CN201410656673.2A CN201410656673A CN104389641A CN 104389641 A CN104389641 A CN 104389641A CN 201410656673 A CN201410656673 A CN 201410656673A CN 104389641 A CN104389641 A CN 104389641A
- Authority
- CN
- China
- Prior art keywords
- pin
- blade root
- impeller
- moving vane
- moving blades
- 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.)
- Granted
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The invention discloses a forked blade root locking structure of moving blades in a high-temperature section of a steam turbine. The forked blade root structure comprises an impeller and the moving blades, wherein the moving blades are arranged on the impeller, blade roots of the moving blades are forked blade roots, assembling grooves which are matched with the forked blade roots are formed in the circumferential surface of the impeller, the blade roots of the moving blades are arranged in the assembling grooves, the moving blades are fixedly locked on the impeller by enabling a pin to penetrate through the blade roots and the impeller, and the pin is called as a core through pin and is positioned at the center positions of the blade roots; a blade root connecting seam of two adjacent moving blades is also provided with a pin, the pin penetrates through the blade roots and the impeller, and the pin which is arranged in the two adjacent blades in a crossing way is called as a seam crossing pin. According to the forked blade root locking structure of the moving blades in the high-temperature section of the steam turbine, disclosed by the invention, the heat stress can be reduced, and the safety of the blades is enhanced.
Description
Technical field
The present invention relates to steam turbine blade, specifically, is a kind of high temperature section moving vane fork type blade root locking mechanism.
Background technique
At the moving vane of steam turbine high-temperature section, the governing-stage moving blade that especially operating temperature is the highest, its blade root is fork type blade root, and blade is worn pin with one and run through blade root, impeller, fastened on impeller by blade lock after loading impeller.The material used because of moving vane, impeller and pin is each different, and thermal expansion coefficient there are differences, and at high temperature, pin, blade root, impeller connecting part can produce very large thermal stress, pin may be cut off, cause leaf abscission, lead to a disaster.
Summary of the invention
For the problems referred to above, the invention provides a kind of high temperature section moving vane fork type blade root locking mechanism, can thermal stress be reduced, strengthen the Security of blade.Its technical solution is:
A kind of steam turbine high-temperature section moving vane fork type blade root locking mechanism, comprise impeller and be arranged on the moving vane on impeller, the blade root of described moving vane is fork type blade root, described impeller side face has the fitting recess with fork type blade root adaptation, the blade root of described moving vane is contained in this groove, runs through blade root, impeller, be locked by moving vane on impeller by a pin, this pin is called that logical core pin is followed closely, and is positioned at blade root central authorities; It is characterized in that, in the blade root seam of adjacent moving vane, be also provided with pin, this pin runs through blade root, impeller, straddles the blade root of adjacent two blades, is called junction of the edges of two sheets of paper pin.
The Pitch radius at described junction of the edges of two sheets of paper pin place is less than the Pitch radius at logical core pin nail place, and the line of centres of described logical core pin nail, left adjacent junction of the edges of two sheets of paper pin, right adjacent junction of the edges of two sheets of paper pin three is isosceles triangle.
Beneficial effect of the present invention:
Substitute a traditional pin with three pins, as long as the sectional area sum of three pins is not less than the sectional area of a former pin, just can ensure join strength, and the diameter of three pins can do little, swell increment is little, and thermal stress is just corresponding reduction also; And because junction of the edges of two sheets of paper pin 4 is located in the blade root seam of adjacent moving vane, seam can receive expansion, reduce pin-and-hole thermal stress, this just substantially increases the Security of blade.
Because logical core pin nail, left adjacent junction of the edges of two sheets of paper pin, right adjacent junction of the edges of two sheets of paper pin are that isosceles triangle is arranged, blade root, impeller cooperation have three strong points, and its relative positional accuracy is higher, and linkage structure is more stable, and during rotor operation, the vibration of blade is less.
Accompanying drawing explanation
Fig. 1 is the plan view of this structure
Fig. 2 is the A-A view of Fig. 1.
Embodiment
See Fig. 1, Fig. 2:
This steam turbine high-temperature section moving vane fork type blade root locking mechanism, the moving vane 1 comprising impeller 2 and be arranged on impeller 2, the blade root of described moving vane 1 is fork type blade root, the side face of described impeller 2 has the fitting recess with fork type blade root adaptation, the blade root of described moving vane 1 is contained in this groove, runs through blade root, impeller, be locked by moving vane on impeller by a pin 3, this pin 3 is called that logical core pin is followed closely, and is positioned at blade root central authorities; In the blade root seam of adjacent moving vane, be also provided with pin 4, this pin 4 runs through blade root, impeller, straddles the blade root of adjacent two blades, is called junction of the edges of two sheets of paper pin.Like this, substitute a traditional pin with three pins, as long as the sectional area sum of three pins is not less than the sectional area of a former pin, just can ensure join strength, and the diameter of three pins can do little, swell increment is little, and thermal stress is just corresponding reduction also; And because junction of the edges of two sheets of paper pin 4 is located in the blade root seam of adjacent moving vane, seam can receive expansion, eliminate thermal stress.This just substantially increases the Security of blade.
The Pitch radius at described junction of the edges of two sheets of paper pin 4 place is less than the Pitch radius that logical core pin follows closely 3 places, and the line of centres of described logical core pin nail, left adjacent junction of the edges of two sheets of paper pin, right adjacent junction of the edges of two sheets of paper pin three is isosceles triangle.Like this, blade root, impeller cooperation have three strong points, and the relative positional accuracy of blade root, impeller is higher, and linkage structure is more stable, and during rotor operation, the vibration of blade is less.
Claims (2)
1. a steam turbine high-temperature section moving vane fork type blade root locking mechanism, comprise impeller and be arranged on the moving vane on impeller, the blade root of described moving vane is fork type blade root, described impeller side face has the fitting recess with fork type blade root adaptation, the blade root of described moving vane is contained in this groove, runs through blade root, impeller, be locked by moving vane on impeller by a pin, this pin is called that logical core pin is followed closely, and is positioned at blade root central authorities; It is characterized in that, in the blade root seam of adjacent moving vane, be also provided with pin, this pin runs through blade root, impeller, straddles the blade root of adjacent two blades, is called junction of the edges of two sheets of paper pin.
2. steam turbine high-temperature section moving vane fork type blade root locking mechanism as claimed in claim 1, it is characterized in that, the Pitch radius at described junction of the edges of two sheets of paper pin place is less than the Pitch radius at logical core pin nail place, and the line of centres of described logical core pin nail, left adjacent junction of the edges of two sheets of paper pin, right adjacent junction of the edges of two sheets of paper pin three is isosceles triangle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410656673.2A CN104389641B (en) | 2014-11-18 | 2014-11-18 | Steam turbine high-temperature section moving vane fork type blade root locking mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410656673.2A CN104389641B (en) | 2014-11-18 | 2014-11-18 | Steam turbine high-temperature section moving vane fork type blade root locking mechanism |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104389641A true CN104389641A (en) | 2015-03-04 |
CN104389641B CN104389641B (en) | 2016-02-17 |
Family
ID=52607590
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410656673.2A Active CN104389641B (en) | 2014-11-18 | 2014-11-18 | Steam turbine high-temperature section moving vane fork type blade root locking mechanism |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104389641B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110145372A (en) * | 2019-05-25 | 2019-08-20 | 立德动力设备(浙江)有限公司 | A kind of turbine rotor fork-shaped blade installation structure and its installation method |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000161006A (en) * | 1998-11-25 | 2000-06-13 | Hitachi Ltd | Steam turbine blade, steam turbine using it, steam turbine power generating plant, and high strength martensite steel |
EP1067206A2 (en) * | 1999-07-09 | 2001-01-10 | Hitachi, Ltd. | Steam turbine blade, and steam turbine and steam turbine power plant using the same |
CN2479214Y (en) * | 2001-06-12 | 2002-02-27 | 东方汽轮机厂 | Final blade of large steam turbine |
CN2828322Y (en) * | 2005-10-12 | 2006-10-18 | 哈尔滨汽轮机厂有限责任公司 | Final stage, penultimate vane of large full speed steam turbine |
CN2903393Y (en) * | 2006-03-20 | 2007-05-23 | 陕西鼓风机(集团)有限公司 | Blade base structure of moving blade for blast furnace gas energy recovering turbine apparatus |
CN201934148U (en) * | 2010-12-20 | 2011-08-17 | 杭州汽轮机股份有限公司 | Low-pressure last stage blade of variable-speed industrial turbine |
-
2014
- 2014-11-18 CN CN201410656673.2A patent/CN104389641B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000161006A (en) * | 1998-11-25 | 2000-06-13 | Hitachi Ltd | Steam turbine blade, steam turbine using it, steam turbine power generating plant, and high strength martensite steel |
EP1067206A2 (en) * | 1999-07-09 | 2001-01-10 | Hitachi, Ltd. | Steam turbine blade, and steam turbine and steam turbine power plant using the same |
CN2479214Y (en) * | 2001-06-12 | 2002-02-27 | 东方汽轮机厂 | Final blade of large steam turbine |
CN2828322Y (en) * | 2005-10-12 | 2006-10-18 | 哈尔滨汽轮机厂有限责任公司 | Final stage, penultimate vane of large full speed steam turbine |
CN2903393Y (en) * | 2006-03-20 | 2007-05-23 | 陕西鼓风机(集团)有限公司 | Blade base structure of moving blade for blast furnace gas energy recovering turbine apparatus |
CN201934148U (en) * | 2010-12-20 | 2011-08-17 | 杭州汽轮机股份有限公司 | Low-pressure last stage blade of variable-speed industrial turbine |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110145372A (en) * | 2019-05-25 | 2019-08-20 | 立德动力设备(浙江)有限公司 | A kind of turbine rotor fork-shaped blade installation structure and its installation method |
CN110145372B (en) * | 2019-05-25 | 2021-08-10 | 立德动力设备(浙江)有限公司 | Steam turbine rotor forked blade mounting structure and mounting method thereof |
Also Published As
Publication number | Publication date |
---|---|
CN104389641B (en) | 2016-02-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101482091B (en) | Rotor blade | |
WO2009112775A3 (en) | Blade with non-axisymmetric platform | |
WO2009112776A3 (en) | Blade with non-axisymmetric platform: recess and boss on the extrados | |
EP2932041A1 (en) | Turbomachine blade, corresponding turbomachine and method of manufacturing a turbine blade | |
IL193127A (en) | Durable blade | |
WO2014163709A3 (en) | Interblade metal platform for ceramic matrix composite turbine blades | |
WO2009112774A3 (en) | Blade with 3d platform comprising an inter-blade bulb | |
FR2961846B1 (en) | TURBOMACHINE TURBOMACHINE WITH COMPLEMENTARY ASYMMETRIC GEOMETRY | |
WO2014155293A8 (en) | Wind turbine blade root and process for manufacturing a wind turbine blade root | |
BR112015012273B1 (en) | METHOD FOR MANUFACTURING A TURBINE ENGINE SHOVEL BASE, TURBINE ENGINE SHOVEL BASE, AND TURBINE ENGINE SHOVEL | |
BR102014005477B1 (en) | TOOL AND METHOD FOR SCARFING A ROTOR BLADE SEGMENT | |
CL2014003280A1 (en) | A wind turbine rotor blade assembly comprises at least two blade sections, one of said sections has at least one cavity in a joint end portion, and the other section has at least one projection; method; a blade for a wind turbine rotor; a rotor; and a turbine | |
WO2015000862A3 (en) | Rotor for a camshaft adjuster having improved geometry | |
CN104389641B (en) | Steam turbine high-temperature section moving vane fork type blade root locking mechanism | |
MX2015016039A (en) | Turbomachine rotor assembly and method. | |
CN203308525U (en) | Fir tree-shaped tenon structure | |
CN105637182B (en) | Turbo blade and gas turbine | |
RU2014139125A (en) | Diaphragm ring for stator blades, turbomachine and method | |
CN205908314U (en) | Pair high pressure turbine vane | |
JP4939613B2 (en) | Turbine blade | |
CN107208652A (en) | Electric fan | |
CN204716304U (en) | Steam turbine blade lock catch device, steam turbine blade and steam turbine | |
MX2021004920A (en) | Wind turbine jointed rotor blade having a hollow chord-wise extending pin. | |
BR112015029362A2 (en) | method for manufacturing a rotating part of a hydraulic machine, rotating part manufactured according to this method, hydraulic machine and power conversion installation | |
JP2013170577A5 (en) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |