CN106761949A - The configuration structure and its assembly method of a kind of hollow blade cooling medium restricting orifice - Google Patents
The configuration structure and its assembly method of a kind of hollow blade cooling medium restricting orifice Download PDFInfo
- Publication number
- CN106761949A CN106761949A CN201611212476.7A CN201611212476A CN106761949A CN 106761949 A CN106761949 A CN 106761949A CN 201611212476 A CN201611212476 A CN 201611212476A CN 106761949 A CN106761949 A CN 106761949A
- Authority
- CN
- China
- Prior art keywords
- orifice plate
- fitting recess
- cooling medium
- blade
- blade 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.)
- Pending
Links
Classifications
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The present invention discloses a kind of configuration structure of hollow blade cooling medium restricting orifice, the hollow blade is by its blade root in the race of impeller, the race has cooling medium input channel, the cooling medium entrance of the hollow blade is located at blade root bottom surface, cooling medium input channel with race is corresponding, restricting orifice is provided with the cooling medium entrance of hollow blade, for limiting cooling medium consumption;The orifice plate configures the joint portion in blade root and race using assembling mode, and uses locking key by orifice plate limitation locking.
Description
Technical field
Invention is related to high-temperature turbine(Turbine)Hollow blade, and in particular to the hollow blade cooling medium restricting orifice is matched somebody with somebody
Put structure and its assembly method.
Background technology
Hollow blade is the core component of ground gas turbine and aero-engine, because operating temperature is very high, to be passed through
Cooling medium is cooled down, and coolant guiding channel is provided with rotor main shaft and impeller, and blade abdominal cavity is led to through blade root, blade
Cooling medium inlet is located on blade root bottom surface, and the import is furnished with restricting orifice, and cooling medium is limited by the flow area of orifice plate
Flow, makes the operating temperature stabilization of blade in design load.
In the past, the configuration structure of the orifice plate was that orifice plate is directly welded on blade root bottom surface, the structure exist problem be,
It is determined that during hollow blade cooling medium consumption, theoretical calculation can only obtain coarse value, also need to simulate blade operating mode, by experiment
Means could obtain the exact value of cooling medium consumption.That is, the flow area of orifice plate cannot be predefined, it is necessary in reality
Constantly changed during testing, it usually needs repeatedly modification can just find the cooling medium stream value for meeting blade working temperature, this
It is accomplished by repeatedly welding, cuts orifice plate, time-consuming, operating efficiency is very low, and easily damage orifice plate and blade, causes experiment
Data precision declines, and cooling medium consumption is inaccurate.
The content of the invention
For problem above, the present invention provides configuration structure and its assembling of a kind of hollow blade cooling medium restricting orifice
Method, its technical solution is:A kind of configuration structure of hollow blade cooling medium restricting orifice, the hollow blade passes through
In the race of impeller, the cooling medium that the impeller has cooling medium input channel, the hollow blade enters its blade root
Mouth is located at blade root bottom surface, and the cooling medium input channel with impeller is corresponding, and section is provided with the cooling medium entrance of hollow blade
Discharge orifice plate, for limiting cooling medium consumption;Characterized in that, the orifice plate is configured in blade root and race using assembling mode
Joint portion, and locking key is used by orifice plate limitation locking;The orifice plate has integrally-built main body and a hook, and the hook is from hole
One end of plate main body is extended, upward back-shaped bending;The blade root bottom surface is provided with orifice plate main body fitting recess and locking key fitting recess,
Blade root side is provided with orifice plate hook fitting recess;The orifice plate fitting recess is axial horizontal opening groove, and opening is located at the one of blade root
Side, orifice plate loads in its fitting recess from the opening, consistent with the direction that blade root loads impeller race;When orifice plate main body loads its dress
During with groove, orifice plate hook is also synchronous to load hook fitting recess, and orifice plate is suspended on blade root by its hook;The locking key fitting recess
It is radial direction vertical opening groove, notch under, put into its fitting recess from bottom to top by locking key;After locking key is assembled in place, its left end
Face is alignd with the right side of orifice plate and is contacted, and by orifice plate limitation locking, orifice plate is not scurried out from impeller race, and by orifice plate master
The opening closure of body fitting recess and orifice plate hook fitting recess, seals, it is to avoid cooling medium is from the opening of orifice plate fitting recess
Release.
The assembly method of above-mentioned hollow blade cooling medium restricting orifice, including step:
A, elder generation load orifice plate in its fitting recess;
B, again the blade root of blade together with the race of orifice plate impulse impeller, do not shift position onto, the installation operation for reserving locking key is empty
Between;
C, locking key is put into its fitting recess;
D, continue the race together with restricting orifice, locking key in the lump impulse impeller the blade root of experiment blade, until in place.
Beneficial effects of the present invention:
Because orifice plate uses assembling structure, convenient disassembly saves test period, improves experiment work efficiency, and avoid because welding repeatedly
Damage orifice plate and blade root are connect, causes it to deform, it is ensured that experimental data is accurate, true and reliable.
Brief description of the drawings
Fig. 1 is AND DEWATERING FOR ORIFICE STRUCTURE figure of the invention
Fig. 2 is leaf and root structure figure of the invention
Fig. 3 is locking key structure chart of the invention
Fig. 4 to Fig. 7 is orifice plate of the invention, locking key assembling process schematic diagram.
Specific embodiment
Referring to Fig. 1, Fig. 2, Fig. 3, Fig. 4 to Fig. 7:The configuration structure of this hollow blade cooling medium restricting orifice, the sky
By its blade root 2 in the race of impeller 4, the impeller 4 has cooling medium input channel, the hollow blade to lobus cardiacus piece
Cooling medium entrance 2-2 be located at the bottom surface of blade root 2, the cooling medium input channel with impeller is corresponding, in hollow blade
Cooling medium entrance 2-2 is provided with restricting orifice 1, for limiting cooling medium consumption.The orifice plate 1 is configured using assembling mode
Blade root 2 and the joint portion of the race of impeller 4, and locking key 3 is used by the limitation locking of orifice plate 1.The orifice plate 1 has integrally-built master
Body and hook 1-2, the center of orifice plate 1 have throttle orifice 1-1, the hook 1-2 to extend from the right-hand member of the main body of orifice plate 1, upwards
Back-shaped bending;The bottom surface of the blade root 2 is provided with orifice plate main body fitting recess 2-1 and locking key fitting recess 2-3, is set on the right flank of blade root 2
Abacus hook fitting recess 2-4, the orifice plate main body fitting recess 2-1 are axial horizontal opening grooves, and opening is positioned at the right side of blade root 2
Side, orifice plate 1 loads in its fitting recess 2-1 from right to left, and the direction with the race that blade root 2 loads impeller 4 is consistent;When orifice plate main body
When loading its fitting recess 2-1, orifice plate hook 1-1 also synchronously loads its fitting recess 2-4, and orifice plate 1 links up with 1-2 and is suspended on leaf by it
On root 2;The locking key fitting recess 2-3 is located at the right part of blade root 2, and its left wall face flushes with the right side of orifice plate 1, locking key dress
It is radial direction vertical opening groove with groove 2-3, notch under, put into its fitting recess 2-3 from bottom to top by locking key 3;When locking key 3 is assembled to
Behind position, its left side contacts with the right side of orifice plate 1, by the limitation locking of orifice plate 1, orifice plate 1 is not altered from the race of impeller 4
Go out, and by the opening closure of orifice plate main body fitting recess 2-1 and orifice plate hook fitting recess 2-4, seal, it is to avoid cooling medium
Released from the opening of orifice plate fitting recess.
The assembly method of above-mentioned hollow blade cooling medium restricting orifice, including step:
A, elder generation load orifice plate 1 in its fitting recess in 2-1,2-4, as shown in Figure 4;
B, again the blade root 2 of blade together with the race of the impulse impeller 4 from right to left of orifice plate 1, do not shift position onto, reserve locking key 3
Installation operation space, as shown in Figure 5;
C, locking key 3 is put into its fitting recess 2-3, as shown in Figure 6;
D, continue the race together with restricting orifice 1, locking key 3 in the lump impulse impeller 4 the blade root 2 of blade, until in place, such as Fig. 7
It is shown.
Demounting procedure is opposite with above-mentioned steps.
Claims (2)
1. a kind of configuration structure of hollow blade cooling medium restricting orifice, the hollow blade is by its blade root mounted in impeller
In race, the cooling medium entrance that the impeller has cooling medium input channel, the hollow blade is located at blade root bottom surface, with
The cooling medium input channel of impeller is corresponding, and restricting orifice is provided with the cooling medium entrance of hollow blade, cold for limiting
But rate-of flow;Characterized in that, the orifice plate configures the joint portion in blade root and race using assembling mode, and use locking key
By orifice plate limitation locking;The orifice plate has integrally-built main body and hook, and the hook extends from one end of orifice plate main body
And go out, upward back-shaped bending;The blade root bottom surface is provided with orifice plate main body fitting recess and locking key fitting recess, and blade root side is provided with hole
Plate links up with fitting recess;The orifice plate fitting recess is axial horizontal opening groove, and opening fills positioned at the side of blade root, orifice plate from the opening
Enter in its fitting recess, it is consistent with the direction that blade root loads impeller race;When orifice plate main body loads its fitting recess, orifice plate hook
Synchronous to load hook fitting recess, orifice plate is suspended on blade root by its hook;The locking key fitting recess is radial direction vertical opening groove,
Notch under, put into its fitting recess from bottom to top by locking key;After locking key is assembled in place, the right side pair of its left side and orifice plate
Neat contact, by orifice plate limitation locking, makes orifice plate not scurried out from impeller race, and orifice plate main body fitting recess and orifice plate are linked up with
The opening closure of fitting recess, seals, it is to avoid cooling medium releases from the opening of orifice plate fitting recess.
2. the assembly method of hollow blade cooling medium restricting orifice described in claim 1, including step:
A, elder generation load orifice plate in its fitting recess;
B, again the blade root of blade together with the race of orifice plate impulse impeller, do not shift position onto, the installation operation for reserving locking key is empty
Between;
C, locking key is put into its fitting recess;
D, continue the race together with restricting orifice, locking key in the lump impulse impeller the blade root of experiment blade, until in place.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201611212476.7A CN106761949A (en) | 2016-12-25 | 2016-12-25 | The configuration structure and its assembly method of a kind of hollow blade cooling medium restricting orifice |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201611212476.7A CN106761949A (en) | 2016-12-25 | 2016-12-25 | The configuration structure and its assembly method of a kind of hollow blade cooling medium restricting orifice |
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CN106761949A true CN106761949A (en) | 2017-05-31 |
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CN201611212476.7A Pending CN106761949A (en) | 2016-12-25 | 2016-12-25 | The configuration structure and its assembly method of a kind of hollow blade cooling medium restricting orifice |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002303101A (en) * | 2001-04-05 | 2002-10-18 | Ishikawajima Harima Heavy Ind Co Ltd | Cooling air adjusting structure of turbin blade |
EP2312124A2 (en) * | 2009-10-14 | 2011-04-20 | Kawasaki Jukogyo Kabushiki Kaisha | Sealing arrangement for use with gas turbine engine |
CN102197193A (en) * | 2008-10-22 | 2011-09-21 | 斯奈克玛 | Turbine blade equipped with means of adjusting its cooling fluid flow rate |
EP2438273B1 (en) * | 2009-06-04 | 2015-08-05 | Ansaldo Energia S.p.A. | Turbine blade |
-
2016
- 2016-12-25 CN CN201611212476.7A patent/CN106761949A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002303101A (en) * | 2001-04-05 | 2002-10-18 | Ishikawajima Harima Heavy Ind Co Ltd | Cooling air adjusting structure of turbin blade |
CN102197193A (en) * | 2008-10-22 | 2011-09-21 | 斯奈克玛 | Turbine blade equipped with means of adjusting its cooling fluid flow rate |
EP2438273B1 (en) * | 2009-06-04 | 2015-08-05 | Ansaldo Energia S.p.A. | Turbine blade |
EP2312124A2 (en) * | 2009-10-14 | 2011-04-20 | Kawasaki Jukogyo Kabushiki Kaisha | Sealing arrangement for use with gas turbine engine |
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Application publication date: 20170531 |
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