CN108019237A - A kind of bionical blade profile of steam turbine for suppressing flow separation - Google Patents

A kind of bionical blade profile of steam turbine for suppressing flow separation Download PDF

Info

Publication number
CN108019237A
CN108019237A CN201711219592.6A CN201711219592A CN108019237A CN 108019237 A CN108019237 A CN 108019237A CN 201711219592 A CN201711219592 A CN 201711219592A CN 108019237 A CN108019237 A CN 108019237A
Authority
CN
China
Prior art keywords
steam turbine
blade profile
blade
flow separation
smooth
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.)
Pending
Application number
CN201711219592.6A
Other languages
Chinese (zh)
Inventor
谢诞梅
陈桐
张敬
杜海芬
梅子岳
张恒良
岳亚楠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuhan University WHU
Original Assignee
Wuhan University WHU
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 by Wuhan University WHU filed Critical Wuhan University WHU
Priority to CN201711219592.6A priority Critical patent/CN108019237A/en
Publication of CN108019237A publication Critical patent/CN108019237A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/145Means for influencing boundary layers or secondary circulations

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)

Abstract

The invention discloses a kind of bionical blade profile of steam turbine for suppressing flow separation, realized by being designed on the basis of original blade profile leading edge repairing type, edge control line is equipped with the smooth projection that multiple height are d in front of the blade, smooth projection uses radius to be seamlessly transitted for the sphere of r with blade inlet edge surface, which is l, a height of h of leaf.In power station steam turbine band operation at part load, blade is under negative angle of attack state and works, the smooth projection blade profile of imitation biochemistry can apply fluid more disturbances, promote energy exchange between fluid and mainstream fluid in leaf grating leading edge separated region, accelerate fluid attaching process again, so as to suppress the phenomenon that negative angle of attack causes pressure face flow separation, efficiency and security of the blade profile in variable working condition are improved.

Description

A kind of bionical blade profile of steam turbine for suppressing flow separation
Technical field
The invention belongs to electrical circuitry equipment manufacture and energy-saving and emission-reduction field, it is related to a kind of power station steam turbine blade profile, and in particular to A kind of bionical blade profile of steam turbine for suppressing flow separation.
Background technology
In the end of the year 2016, in China's capacity of installed generator, thermal power generation unit and nuclear energy power generation unit account for about 66.32%, These units are all using steam turbine as prime mover.For coordinate peak load regulation network operation, Large-scale fire-electricity unit have to often in Varying duty state is run;To coordinate the access of regenerative resource, nuclear power generating sets even also face the demand of peak regulation.As power station Energy conversion key device, steam turbine performance especially variable working condition when performance have to the economy and security in power plant Tremendous influence.Therefore, efficiency and its security of the large-size steam turbine under variable parameter operation state are improved, to lifting Chinese large-sized The autonomous Design and manufacturing capacity of power-equipment have important practical significance.At the same time, bionical Airfoil Design is in the ascendant, Its application on the outflow hydrodynamics component such as rudder for ship, aircraft wing, fan blade has good result, is that current hot topic is ground Study carefully problem.However, existing literature has no the application of bionical aerofoil profile flow device in power station steam turbine etc..
The content of the invention
For above-mentioned background present situation, the purpose of the present invention is devise a kind of power station steam turbine leaf based on bionics principle Type, steam flow flow separation during by suppressing variable parameter operation, so as to improve the efficiency and its security of large-size steam turbine.
Another object of the present invention is to provide one kind and carries out the improved method of imitation biochemistry to existing steam turbine blade profile, can solve Existing steam turbine blade profile the problem of efficiency is relatively low under varying load condition.
To achieve the above object, the technical solution adopted by the present invention is as follows:
A kind of bionical blade profile of steam turbine for suppressing flow separation, it is characterised in that:Edge control line is equipped with more in front of the blade A height is the smooth projection of d, and smooth projection uses radius to be seamlessly transitted for the sphere of r with blade inlet edge surface, which puts down Equal chord length is l, a height of h of leaf.
As an improvement, the smooth rising height d meets that 3%l≤d≤8%l, smooth projection spacing m meet 3%h≤m ≤ 12%h.
As an improvement, the smooth tangent connection of circular arc that radius of curvature r is used between projection and leading edge control line, is formed new Leading edge control line, radius of curvature r meet 7%l≤r≤20%l.
As an improvement, smooth projection and the spherical radius r of blade surface smooth blend meet 7%l≤r≤20%l.
As an improvement, multiple smooth projections are uniformly distributed on edge control line in front of the blade.
The beneficial effects of the invention are as follows:
The present invention uses for reference the protrusion of the biological fin leading edge of whale etc. in natural environment on the basis of existing steam turbine blade profile Shape structure, by carrying out imitation biochemistry design to blade inlet edge, so as to reach the mesh of steam flow flow separation when suppressing variable parameter operation 's.Due to without significantly being adjusted to existing blade profile, with the R&D cycle is short, cost is low, with prophyll type security feature phase Like etc. advantage.Simplation verification improves blade profile in low- load conditions by delaying flow separation the results show that opposite prophyll type Occur, so as to reach the internal efficiency ratio of higher.
Brief description of the drawings
Fig. 1 is the bionical leaf structure schematic diagram of steam turbine of the present invention.
Fig. 2 is that size annotates schematic diagram in the bionical blade profile of steam turbine of the present invention.
Fig. 3 is specific embodiment of the invention Central Plains blade profile cascade flow field schematic diagram.
Fig. 4 is the bionical blade profile cascade flow field schematic diagram of steam turbine that bionics principle is used in the specific embodiment of the invention 1.
1- trailing edge control lines, 2- leading edge control lines, the smooth projections of 3-, 4- blades.
Embodiment
Below with reference to the embodiments and with reference to the accompanying drawing the technical solutions of the present invention will be further described.
Embodiment 1:
Present embodiment provides a kind of bionical blade profile of steam turbine for suppressing flow separation, this blade profile is by trailing edge control line 1st, leading edge control line 2 and smooth projection 3 are formed.
As depicted in figs. 1 and 2, it is the local leaf structure schematic diagram of blade 4 in Fig. 1, in schematic diagram, is in mean chord Several smooth projections, smooth rising height d=5%l, smooth projection are evenly arranged on the steam turbine blade profile leading edge control line of l Between spacing m=10%h, the tangent connection of circular arc of radius of curvature r=10%l is used between smooth projection and leading edge control line, Form new leading edge control line.It is same to use radius of curvature r=10%l's to make smooth projection and leaf grating smooth surface transition Sphere closes the region.
By the bionical blade profile of steam turbine of the present invention in power station steam turbine band operation at part load, blade is in negative angle of attack state Lower work, the smooth projection blade profile of imitation biochemistry can apply fluid more disturbances, promote in leaf grating leading edge separated region fluid with Energy exchange between mainstream fluid, accelerates fluid attaching process again, so that suppress the phenomenon that negative angle of attack causes pressure face flow separation, Improve efficiency and security of the blade profile in variable working condition.
Fig. 3 and Fig. 4 is respectively the high section cascade flow of prophyll type and bionics principle blade profile 50% leaf in 12.5% load Field schematic diagram, the mechanism of flow separation is illustrated when this two width figure suppresses variable parameter operation to bionics blade profile.From Fig. 3 with And can see in Fig. 4, under 12.5% load condition, since negative angle of attack is excessive, there is stream in leaf grating pressure face leading edge The separated region that body can not adhere to.Difference is that Fig. 3 Central Plains blade profile pressure face leading edge separated region shows enclosed separation The characteristics of, fluid and external fluid quality, momentum-exchange are less in separated region, therefore rarer streamline is extended into this region Portion;And the quality momentum between fluid and the external world in separated region is strengthened since bionical blade profile is to the perturbation action of fluid in Fig. 4 Exchange so that fluid can faster obtain energy and be attached to blade surface again in separated region, and then improve flow efficiency.Separately On the one hand, due to the bionical leading edge design of blade profile introducing in Fig. 4, reduce due to separation vortex shedding and trigger unsteady exciting force Possibility, and then the hidden danger of fatigue damage occurs for leaf grating during mitigation variable parameter operation, improves the security of leaf grating.
Embodiment 2:
Several smooth projections, smooth projection are evenly arranged on the steam turbine blade profile leading edge control line that mean chord is l Height d=3%l, smooth projection spacing m=3%h, using radius of curvature r=7%l's between smooth projection and leading edge control line The tangent connection of circular arc, forms new leading edge control line.To make smooth projection and leaf grating smooth surface transition, equally using curvature half The sphere of footpath r=7%l closes the region.
Embodiment 3:
Several smooth projections, smooth projection are evenly arranged on the steam turbine blade profile leading edge control line that mean chord is l Height d=12%l, smooth projection spacing m=8%h, use radius of curvature r=20%l between smooth projection and leading edge control line The tangent connection of circular arc, form new leading edge control line.To make smooth projection and leaf grating smooth surface transition, equally using curvature The sphere of radius r=20%l closes the region.
Specific embodiment described herein is only to spirit explanation for example of the invention.Technology belonging to the present invention is led The technical staff in domain can do various modifications or additions to described specific embodiment or replace in a similar way Generation, but without departing from spirit of the invention or beyond the scope of the appended claims.

Claims (5)

  1. A kind of 1. bionical blade profile of steam turbine for suppressing flow separation, it is characterised in that:Edge control line is equipped with multiple in front of the blade Highly it is the smooth projection of d, smooth projection uses radius to be seamlessly transitted for the sphere of r with blade inlet edge surface, which is averaged Chord length is l, a height of h of leaf.
  2. A kind of 2. bionical blade profile of steam turbine for suppressing flow separation according to claim 1, it is characterised in that:It is described smooth Rising height d meets that 3%l≤d≤8%l, smooth projection spacing m meet 3%h≤m≤12%h.
  3. A kind of 3. bionical blade profile of steam turbine for suppressing flow separation according to claim 1, it is characterised in that:Smooth projection The tangent connection of circular arc of radius of curvature r is used between leading edge control line, forms new leading edge control line, radius of curvature r meets 7%l≤r≤20%l.
  4. A kind of 4. bionical blade profile of steam turbine for suppressing flow separation according to claim 1, it is characterised in that:Smooth projection Meet 7%l≤r≤20%l with the spherical radius r of blade surface smooth blend.
  5. A kind of 5. bionical blade profile of steam turbine for suppressing flow separation according to claim 1, it is characterised in that:It is multiple smooth Projection is uniformly distributed on edge control line in front of the blade.
CN201711219592.6A 2017-11-28 2017-11-28 A kind of bionical blade profile of steam turbine for suppressing flow separation Pending CN108019237A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711219592.6A CN108019237A (en) 2017-11-28 2017-11-28 A kind of bionical blade profile of steam turbine for suppressing flow separation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711219592.6A CN108019237A (en) 2017-11-28 2017-11-28 A kind of bionical blade profile of steam turbine for suppressing flow separation

Publications (1)

Publication Number Publication Date
CN108019237A true CN108019237A (en) 2018-05-11

Family

ID=62077387

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711219592.6A Pending CN108019237A (en) 2017-11-28 2017-11-28 A kind of bionical blade profile of steam turbine for suppressing flow separation

Country Status (1)

Country Link
CN (1) CN108019237A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111622808A (en) * 2020-05-25 2020-09-04 武汉大学 Bionic blade based on existing steam turbine blade profile transformation and design method
CN115081138A (en) * 2022-06-22 2022-09-20 武汉大学 Guide vane design method for improving operation stability of pump turbine and pump turbine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB789883A (en) * 1954-08-20 1958-01-29 Power Jets Res & Dev Ltd High speed aerofoil
JP2000104501A (en) * 1998-09-28 2000-04-11 Hitachi Ltd Turbine moving blade, gas turbine and steam turbine
CN104114815A (en) * 2011-12-22 2014-10-22 通用电气公司 Airfoils and corresponding fabricating method
CN104612758A (en) * 2014-12-19 2015-05-13 中国民航大学 Low-pressure turbine blade with low loss
CN105626159A (en) * 2016-03-03 2016-06-01 哈尔滨工程大学 Variable geometry turbine with wavy concaved structures on front edges of movable blades
CN105298924B (en) * 2015-10-23 2017-09-15 上海交通大学 Compressor bionics stator blade and its implementation based on humpback flipper

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB789883A (en) * 1954-08-20 1958-01-29 Power Jets Res & Dev Ltd High speed aerofoil
JP2000104501A (en) * 1998-09-28 2000-04-11 Hitachi Ltd Turbine moving blade, gas turbine and steam turbine
CN104114815A (en) * 2011-12-22 2014-10-22 通用电气公司 Airfoils and corresponding fabricating method
CN104612758A (en) * 2014-12-19 2015-05-13 中国民航大学 Low-pressure turbine blade with low loss
CN105298924B (en) * 2015-10-23 2017-09-15 上海交通大学 Compressor bionics stator blade and its implementation based on humpback flipper
CN105626159A (en) * 2016-03-03 2016-06-01 哈尔滨工程大学 Variable geometry turbine with wavy concaved structures on front edges of movable blades

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111622808A (en) * 2020-05-25 2020-09-04 武汉大学 Bionic blade based on existing steam turbine blade profile transformation and design method
CN115081138A (en) * 2022-06-22 2022-09-20 武汉大学 Guide vane design method for improving operation stability of pump turbine and pump turbine
CN115081138B (en) * 2022-06-22 2024-05-31 武汉大学 Guide vane design method for improving running stability of water pump turbine and water pump turbine

Similar Documents

Publication Publication Date Title
CN103422912A (en) Turbine with moving blades with pits at blade tops
Sun et al. Hydrodynamic and energy extraction properties of oscillating hydrofoils with a trailing edge flap
CN108019237A (en) A kind of bionical blade profile of steam turbine for suppressing flow separation
CN103291561A (en) Wind turbine blade with split winglet at apex
CN205779470U (en) A kind of blunt trailing edge wind mill airfoil circulation control device
CN102720622A (en) Vortex generator for turbine draft tube
CN112926132B (en) Fixed wing airfoil aerodynamic shape design method considering influence of three-dimensional effect
CN104018998B (en) 21%-thickness main airfoil for megawatt wind turbine blade
CN204007275U (en) With the H shape finned tube of long direction eddy generator
Zhang et al. Bionic shark fin combined airfoil blade optimal design and numerical simulation of horizontal axis tidal current turbine
CN103883483B (en) A kind of 100W blade of wind-driven generator
Rehman et al. A review of darrieus water turbines
CN207701280U (en) A kind of airfoil wind sail and wind turbine of adaptive liter of resistance regulation
CN204126820U (en) A kind of small-sized wind power generator blade
CN214660605U (en) High-lift wind turbine wing section
CN111622808B (en) Bionic blade based on steam turbine blade profile transformation and design method
CN109117552B (en) Turbine blade variable load flow pattern design method
CN109101722B (en) Composite forming design method for turbine blade
CN110566400B (en) Horizontal shaft wind turbine blade
CN203770019U (en) 100-W wind turbine blade
CN106704092A (en) Synergistic spoiler blade
Yang et al. Study on influence of V-groove on flow field distribution and aerodynamic performance of blunt trailing edge airfoil
CN206522215U (en) Synergy spoiler blade
Su et al. Investigation of Spanwise Wavy Configuration for Performance Improvement of a Vertical Axis Wind Turbine
CN114576065B (en) Water pump turbine runner with turn-around characteristic

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20180511

RJ01 Rejection of invention patent application after publication