CN204738902U - Impacted style or inclined jet turbine nozzle - Google Patents

Impacted style or inclined jet turbine nozzle Download PDF

Info

Publication number
CN204738902U
CN204738902U CN201520463699.5U CN201520463699U CN204738902U CN 204738902 U CN204738902 U CN 204738902U CN 201520463699 U CN201520463699 U CN 201520463699U CN 204738902 U CN204738902 U CN 204738902U
Authority
CN
China
Prior art keywords
nozzle
needle
jet turbine
stable section
impact type
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 - Fee Related
Application number
CN201520463699.5U
Other languages
Chinese (zh)
Inventor
肖炳生
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201520463699.5U priority Critical patent/CN204738902U/en
Application granted granted Critical
Publication of CN204738902U publication Critical patent/CN204738902U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Landscapes

  • Hydraulic Turbines (AREA)

Abstract

The utility model discloses an impacted style or inclined jet turbine nozzle, including nozzle body and nozzle needle, the needle point cone angle of nozzle needle is 36-38, and the best needle point cone angle is 37. According to impacted style or inclined jet turbine nozzle, life is markedly increased, is about 2-3 times at former nozzle, and the efflux is concentrated, and the unit is exerted oneself stably, and efficiency increases approximately 5-10%, and especially when non - full load, the effect is obvious, and maintenance and dismantle conveniently, and significantly reduce nozzle needle and nozzle maintenance duration improve the power station benefit.

Description

Impact type or inclined-jet turbine nozzle
Technical field
The present invention relates to hydroelectric machine field, specifically a kind of impact type or inclined-jet turbine nozzle.
Background technique
China is the country that a water resources is abundant.As the energy conversion water turbine utilizing water resources, be mainly divided into two types, one is reaction turbine, and another kind is impulse turbine.For impulse turbine, the service behaviour of nozzle has great importance for water turbine, and the quality of the service behaviour of nozzle is then determined by the shape of nozzle.Existing water turbine nozzle needle is all based on 45 ~ 67 ° of schemes, nozzle needle surface of contact is 2 ~ 3mm, there is no fluid stable section, damage by easily causing nozzle and nozzle needle during nozzle when unit operation runs into foreign material, thus cause jet instability and unit output decrease in efficiency, occur with the most common failure such as runner water dumping and bearing water inlet simultaneously.And nozzle adopts most built-in type, maintain and replace is very difficult.
Summary of the invention
The object of this invention is to provide a kind of impact type or inclined-jet turbine nozzle, improving working life by improving nozzle, ensureing that unit output is stablized, maintenance and convenient disassembly.
The present invention's adopted technological scheme of dealing with problems is: a kind of nozzle of impulse water turbine, comprises nozzle body and nozzle needle, and the needle point cone angle of described nozzle needle is 36 ~ 38 °, and best needle point cone angle is 37 °.
Described nozzle needle back segment is straightway, and this planarea is consistent with the angle that nozzle inner face is formed and nozzle needle wedge angle, general scope of design 36 ~ 38 °, best angle 37 °.
The fluid stable section of described nozzle comprises outer stable section and interior stable section, and outer stable section length is 10mm; Interior stable section length is 10 ~ 20mm, and adapt with nozzle needle shape, gradient is identical, the water surface also.
Described nozzle is crossed water engaging surface and is adopted stainless steel veneer, thickness 2 ~ 3mm, described nozzle needle front end and adopt stainless steel veneer with nozzle surface of contact, thickness 2 ~ 3mm.
Described nozzle needle needle point excessive portion chamfering, cutting removes.
Described nozzle arrangements is external mounted, and nozzle is by being contained on nozzle carrier outside bolt.
In the high head run-off river power station running of mountain area, carry out adjustment owing to there is no reservoir to run, carry out the water yield to change with natural runoff, unit adjusts the amount of overcoming at any time and remains on the situation that high head operation prevents forebay emptying, therefore unit proposes high requirement to adjustment, and the key position regulated is nozzle, nozzle needle.Existing unit (about 50%) when insufficient water sources is exerted oneself less just there will be following problem: impeller water dumping appears in unit, affects bearing water inlet and damages, to exert oneself and efficiency sharply declines.Main cause is that injection stream dispersion is not concentrated, and part current inject directly to bucket edge or outside.And cause the main cause of spray dispersion be 45 ° of-67 ° of nozzle needles (mouth) when producing jet because of angle comparatively mass-flow mutually collide, without jet stability section, and distance runner wheel is far away, no matter refer to jet schematic diagram, from Fig. 2,3,4, be 45 ° of nozzle needles, or 67 ° of nozzle needles, all have amplification after its jet delivery nozzle, the jet of 37 ° of nozzle needles then without amplification, substantially linearly.
The applicant is by carrying out the discovery of water turbine Maintenance And Test for many years by the highest and not fragile for nozzle needle and nozzle angle correction turbine efficiency about 37 ° time.Increase nozzle fluid stable section to ensure nozzle intensity and fluid stable performance simultaneously.Adopted by water engaging surface stainless steel veneer 2 ~ 3mm to solve nozzle needle, nozzle wear and corrosion, and ensure that sealing face length degree is 10 ~ 20mm, to ensure stagnant water effect.Nozzle arrangements is that external mounted is to facilitate nozzle needle to keep in repair and to change.Because nozzle needle angle reduces to cause length of needlepoint to increase, nozzle needle excessive portion chamfering, cutting is removed, to ensure that jet deflector can normally use, ensure unit safety, refer to jet schematic diagram.According to impact type of the present invention or inclined-jet turbine nozzle, working life obviously increases, be about 2 ~ 3 times, former nozzle, jet is concentrated, and unit output is stablized, efficiency increases about 5 ~ 10%, especially non-at full capacity time, effect obviously, and maintenance and convenient disassembly, greatly reduce nozzle needle and nozzle engineering time, improve power generation.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the present invention is described in further detail.
Fig. 1 is structural representation of the present invention, is shown as state when nozzle needle and nozzle close.
Fig. 2 is the present invention's 37 ° of nozzle needle jet schematic diagram used.
Fig. 3 is 45 ° of nozzle needle jet schematic diagram.
Fig. 4 is 67 ° of nozzle needle jet schematic diagram.
Embodiment
Embodiment: with reference to Fig. 1, a kind of impact type or inclined-jet turbine nozzle, include nozzle body and be arranged on the nozzle needle 9 in nozzle.Described nozzle is adopted as external mounted, comprises nozzle carrier 1 and nozzle 6, designs bolt hole 4 outside nozzle carrier 1, and nozzle 6 is by being contained in outside bolt on nozzle carrier 1.Described nozzle 6 front end arranges fluid stable section, and fluid stable section comprises outer stable section 8 and interior stable section 7, and outer stable section 8 length is 10mm; Interior stable section 7 length is 10 ~ 20mm, and shape and nozzle needle shape adapt, and gradient is identical, sealing face when being also simultaneously closed state, arranging of double fluid state stable section ensures nozzle intensity and fluid stable performance, and sealing face length degree is 10 ~ 20mm, ensures stagnant water effect.Cross water engaging surface at nozzle 6 and adopt stainless steel veneer, thickness 2 ~ 3mm, solve nozzle needle, nozzle wear and corrosion.Described nozzle needle 9 is installed and is connected connecting rod 2, and needle point cone angle 10 scope of design of nozzle needle 9 is 36 ~ 38 °, and optimal needle pointed cone angle is 37 °; Described nozzle needle 9 back segment 3 is straight line, and this face, straightway place is consistent with the needle point cone angle 10 of nozzle needle with the angle 5 that nozzle inner face is formed, and namely scope of design is 36 ~ 38 °, and best needle point cone angle is 37 °.Nozzle needle front end 11 and adopt stainless steel veneer with nozzle surface of contact, thickness 2 ~ 3mm; Because nozzle needle angle reduces to cause length of needlepoint to increase, nozzle needle front end 11 excessive portion chamfering, cutting is removed, to ensure that jet deflector can normally use, ensure unit safety.
The present invention is applied in water power plant, spunyarn hole, and this water power plant is positioned at spunyarn hole village, Huang Mao garden town, Xupu County, Hunan Province, design 2x400KW, design head 200 meters, rated head 180 meters, the maximum service capacity 400KW of unit, water turbine model is CJA237-W-55/1*9 orifice size 92mm.In in November, 2014 power generation.New unit operation half a year, No. 1 machine drops to 380KW, and No. 2 machines drop to 345KW, takes water turbine apart and finds, No. 1 machine nozzle is without apparent damage, and No. 2 machine nozzle seriously corrodeds, simultaneously with unit bearing heating, noise vibration obviously increases.By by following parameter: orifice size is contracted to 87mm, nozzle needle angle changes 37 ° into, scabble nozzle needle and be greater than 97mm with external taper (namely nozzle needle back segment is for straightway), nozzle needle flow surface edge stainless steel, after transforming nozzle needle and nozzle, nozzle needle full-gear unit output reaches 400kw, and unit noise, vibrations, letdown flow all obviously reduce.

Claims (10)

1. impact type or an inclined-jet turbine nozzle, comprises nozzle body and nozzle needle, it is characterized in that: the needle point cone angle of described nozzle needle is 36 ~ 38 °.
2. impact type according to claim 1 or inclined-jet turbine nozzle, is characterized in that: the needle point cone angle of described nozzle needle is 37 °.
3. impact type according to claim 1 and 2 or inclined-jet turbine nozzle, is characterized in that: described nozzle needle back segment is straightway, and this straightway place plane is consistent with the angle that nozzle inner face is formed and nozzle needle wedge angle, is 36 ~ 38 °.
4. impact type according to claim 1 and 2 or inclined-jet turbine nozzle, is characterized in that: described nozzle needle back segment is straightway, and this straightway place plane is consistent with the angle that nozzle inner face is formed and nozzle needle wedge angle, is 37 °.
5. impact type according to claim 1 and 2 or inclined-jet turbine nozzle, is characterized in that: the fluid stable section of described nozzle comprises outer stable section and interior stable section, and outer stable section length is 10mm; Interior stable section length is 10 ~ 20mm, and adapt with nozzle needle shape, gradient is identical, the water surface also.
6. impact type according to claim 3 or inclined-jet turbine nozzle, is characterized in that: the fluid stable section of described nozzle comprises outer stable section and interior stable section, and outer stable section length is 10mm; Interior stable section length is 10 ~ 20mm, and adapt with nozzle needle shape, gradient is identical, the water surface also.
7. impact type according to claim 1 and 2 or inclined-jet turbine nozzle, is characterized in that: described nozzle is crossed water engaging surface and adopted stainless steel veneer, thickness 2 ~ 3mm, described nozzle needle front end and adopt stainless steel veneer with nozzle surface of contact, thickness 2 ~ 3mm.
8. impact type according to claim 3 or inclined-jet turbine nozzle, is characterized in that: described nozzle is crossed water engaging surface and adopted stainless steel veneer, thickness 2 ~ 3mm, described nozzle needle front end and adopt stainless steel veneer with nozzle surface of contact, thickness 2 ~ 3mm.
9. impact type according to claim 1 and 2 or inclined-jet turbine nozzle, is characterized in that: described nozzle needle needle point excessive portion chamfering, cutting removes.
10. impact type according to claim 1 and 2 or inclined-jet turbine nozzle, is characterized in that: described nozzle arrangements is external mounted, and nozzle is by being contained on nozzle carrier outside bolt.
CN201520463699.5U 2015-07-01 2015-07-01 Impacted style or inclined jet turbine nozzle Expired - Fee Related CN204738902U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520463699.5U CN204738902U (en) 2015-07-01 2015-07-01 Impacted style or inclined jet turbine nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520463699.5U CN204738902U (en) 2015-07-01 2015-07-01 Impacted style or inclined jet turbine nozzle

Publications (1)

Publication Number Publication Date
CN204738902U true CN204738902U (en) 2015-11-04

Family

ID=54420642

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520463699.5U Expired - Fee Related CN204738902U (en) 2015-07-01 2015-07-01 Impacted style or inclined jet turbine nozzle

Country Status (1)

Country Link
CN (1) CN204738902U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104912718A (en) * 2015-07-01 2015-09-16 肖炳生 Impact type or inclined water turbine nozzle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104912718A (en) * 2015-07-01 2015-09-16 肖炳生 Impact type or inclined water turbine nozzle

Similar Documents

Publication Publication Date Title
AR059697A1 (en) CONTROL JET FOR A HYDRAULIC TURBINE
CN207049062U (en) A kind of new drop cavitation impeller
CN201511304U (en) Cooling component provided with bundled high-pressure nozzle
CN104912718B (en) Nozzle of impulse water turbine
CN204738902U (en) Impacted style or inclined jet turbine nozzle
CN103912434B (en) A kind of small power station's axial flow water turbine equipment
CN204783418U (en) Pelton turbine equipment
CN201202576Y (en) Bucket impulse turbine
CN108119283A (en) A kind of new impulse turbine nozzle arrangements
CN104389299A (en) Aeration structure for Longluowei flood discharging tunnel
CN103042053B (en) A kind of water system parallel for ultrafast cold-peace section cooling dual system
CN211922550U (en) Improve power station tailrace tunnel open-full flow influence's adverse slope weir structure
CN201460990U (en) Moving blade of steam turbine
CN204900140U (en) Hydraulic turbine inhalant canal
CN204419603U (en) A kind of adjustable pump chamber backplate Pulp pump
CN203257475U (en) Self-adjusting blade type steam seal
CN204167338U (en) A kind of Novel photovoltaic solar energy silver slurry adds tool
CN201992227U (en) Greenhouse ground pipeline connecting structure
CN104499466A (en) Tailrace tunnel with variable crest elevation
CN201599207U (en) Rotary regulation-type pump inlet complementary energy device
CN110700209A (en) Improve power station tailrace tunnel open-full flow influence's adverse slope weir structure
CN201802542U (en) Impact water wheel unit for low water head hydroelectric power generation
CN204844354U (en) A nozzle for water cutting equipment
CN205310077U (en) Modular sand blasting machine nozzle
CN201815407U (en) Glue-injection nozzle of glue-injection machine

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20151104

Termination date: 20170701

CF01 Termination of patent right due to non-payment of annual fee