EP2823153A1 - Impeller for a rotor of a turbomachine, and rotor and turbomachine having an impeller of said type - Google Patents
Impeller for a rotor of a turbomachine, and rotor and turbomachine having an impeller of said typeInfo
- Publication number
- EP2823153A1 EP2823153A1 EP13706262.6A EP13706262A EP2823153A1 EP 2823153 A1 EP2823153 A1 EP 2823153A1 EP 13706262 A EP13706262 A EP 13706262A EP 2823153 A1 EP2823153 A1 EP 2823153A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- blade
- impeller
- groove
- wheel disc
- rotor
- 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
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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/025—Fixing blade carrying members on shafts
-
- 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
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/326—Locking of axial insertion type blades by other means
Definitions
- Impeller for a rotor of a turbomachine as well
- the invention relates to a trained according to the preamble of claim 1 impeller for a rotor of a turbomachine, equipped with such an impeller rotor for a turbomachine and a turbomachine with a rotor equipped with such an impeller.
- the blades are each fixed by means of a rivet both axially and radially in their respective axial groove.
- a rivet requires widening of a closing head of the rivet when mounting the respective blade, and dismantling (e.g., drilling away) the closing head when disassembling the respective blade.
- the invention has for its object to provide an impeller according to the preamble of claim 1, so that the blades are assembled and disassembled with less time and can be fixed with defined radial tension in their respective axial grooves.
- the invention is also based on the object to provide a rotor equipped with such an impeller for a turbomachine and a turbomachine with a rotor equipped with such an impeller.
- an impeller for a rotor of a turbomachine comprising: a wheel disc to be provided on a rotor shaft of the rotor and having a plurality of grooves distributed along an outer circumference of the wheel disc and which each extend in an axially extending the rotor shaft thickness direction of the wheel disc; wherein at two mutually parallel to the thickness direction extending opposite groove sides of each groove a tooth profile is formed; a plurality of blades, each of which has a
- Blade root with two mutually remote parallel to the thickness direction extending blade root sides, on each of which a tooth profile is formed; wherein each blade is inserted into a respective one of the grooves to form a blade-groove combination with its blade root so that the tooth profiles of the blade root sides engage with the tooth profiles of the groove sides; and wherein each blade-groove combination a
- Fixing device which is arranged, the blade in the groove in both the thickness direction and in a radial direction of the wheel against
- the impeller according to the invention is characterized in that each fixing device on both sides at least in the thickness direction
- the bolt provides in the locking position for the side walls of the recess a double-sided stop in the thickness direction, so that the blade is fixed in the thickness direction against movement.
- Blade under application to a predetermined biasing force in the radial direction (radially outward) fixed in this direction against movement.
- the controlled adjustment of the bolt, the predetermined force or the predetermined biasing force (radial strain) can be predefined radially outward in a simple and repeatable manner.
- Formed recess in the form of a circumferentially surrounded by material of the blade sink in the bottom of the blade, wherein a provided for engagement in the recess radially outermost end of the bolt is formed complementary to the recess.
- the recess is formed as a negative to the outer contour of a spherical cap, wherein the radially outermost end of the bolt has a shape corresponding to the outer contour of this spherical cap.
- this embodiment of the impeller according to the invention is advantageously a self-centering of the bolt in the recess and thus a more accurate fixation of the blade and easier insertion of the bolt realized in the recess.
- each fixing device in the wheel disc on a first radial passage in the first passage which opens at a first longitudinal end of this in the groove and in which the bolt is preferably fitted with clearance fit.
- the first passage provides in a simple and robust way a sliding guide for moving the bolt.
- the first passage is designed as an easy-to-make hole.
- each fixing device on an adjusting device which is arranged at a second longitudinal end of the first passage for the controlled adjustment of the bolt, wherein the adjusting device is arranged so that it faces from a pointing in the thickness direction lateral side of the wheel disc for adjusting the bolt is controlled.
- the adjusting device can be activated from the lateral side of the wheel disc, this driving position is easily accessible to a person to be mounted or dismantled, as a result of which the respective expenditure of time is further reduced and the precision of the execution further improved.
- the adjusting device has a second passage, which is formed in the thickness direction of the wheel disc running in this with internal thread, so that the first passage opens with its second longitudinal end in the second passage and a first
- Longitudinal end of the second passage in the lateral side of the wheel disc opens, and a screw member which is screwed from the lateral side of the wheel disc in the second passage and which is in contact with a radially innermost end of the bolt, so that a displacement of the screw member causes a displacement of the bolt in the radial direction in the thickness direction of the wheel disc.
- Screw element is particularly simple and robust, so that the
- Manufacturing costs for the adjusting device are relatively low and their life and reliability are high.
- a provided for contact with the bolt longitudinal end of the screw member is formed with a first conical shape, wherein the radially innermost end of the bolt is formed with a second conical shape, so that between each lateral surfaces of the first and the second cone shape line contact is realized.
- the first conical shape has a cone angle of about 20 degrees. This size of the cone angle provides a particularly advantageous compromise between self-locking, actuating force and travel of the adjusting device.
- a rotor for a turbomachine having at least one impeller in any conceivable combination according to one, several or all of the previously described embodiments of the invention.
- a turbomachine with a rotor having at least one impeller in any conceivable combination according to one, several or all of the previously described embodiments of the invention.
- FIG. 1 shows a partial sectional view of an impeller of a rotor
- Turbomachine according to an embodiment of the invention, viewed in an axial direction of the rotor.
- FIG. 2 shows a view of the impeller of FIG. 1, seen as a section along a section line AA in FIG. 1 and 2 show partial sectional views of an impeller 20 of a rotor 10 of a turbomachine 1 according to an embodiment of the invention.
- the rotor 10 has a rotor shaft (not labeled) on which a plurality of impellers 20 as shown in FIGS. 1 and 2 are arranged one behind the other in an axial direction AR of the rotor shaft.
- the turbomachine 1 having the rotor 10 is preferably a turbine, such as a turbine. as a steam turbine, or designed as a turbo compressor. In addition, the turbomachine 1 is preferred as
- each impeller 20 includes a wheel disc 30, a plurality of blades 40 (only one shown), and a plurality of
- Fixing devices 50 (only one shown) on.
- the wheel disc 30 is arranged either integral therewith or as a separate part rotationally fixed to the rotor shaft of the rotor 10 and has a plurality of grooves 32 (only one shown), which are arranged distributed uniformly along an outer periphery 31 of the wheel disc 30 and which in each case in an axial direction of the rotor shaft extending thickness direction (which corresponds to the axial direction AR) of the wheel disc 30 extend.
- each groove 32 has a tooth profile 33rd
- Each blade 40 has a blade root 41 with two from each other
- each blade 40 is inserted with a blade-groove combination with its blade root 41 in a respective one of the grooves 32, so that the tooth profiles 43 of the Schaufelfußrich with the tooth profiles 33 of the groove sides are engaged. In this way, the rotor blades 40 are resiliently held on the wheel disc 30 in a radial direction RR of the wheel disc 30 or of the rotor shaft.
- the tooth profiles 33, 43 of the groove sides and the blade root sides are preferably designed as multi-toothed tooth profiles. More preferably, the blade roots 41 of the respective blades 40 are each formed in technical language as a fir tree root known blade foot 41. Accordingly, the grooves 32 of the wheel disc 30 are formed in their shape more preferably as a hull contour or negative to the shape of a Christmas tree foot.
- Each combination of groove 32 and blade 40 fitted therein has one of the fixators 50.
- Each fixing device 50 is adapted to fix the associated blade 40 in the associated groove 32 in the thickness direction or in the axial direction AR as well as in the radial direction RR of the wheel disc 30 against movement.
- each fixing device 50 has an at least in the thickness direction or axial direction AR closed on both sides recess 51 in a bottom 32a of the groove 32 facing bottom 44 of the blade 40 and a preferably designed in the form of a circular cylindrical pin latch 52 which in the bottom 32a the groove 32 is received movable or displaceable.
- Each fixing device 50 also has in the wheel disc 30 in an
- Each fixing device 50 furthermore has an adjusting device 60, which is arranged on a second longitudinal end 53b of the first passage 53 for the controlled adjustment of the bolt 52.
- the adjusting device 60 is set up so that it can be actuated by a lateral side 30a of the wheel disc 30 pointing in the direction of thickness or in the axial direction AR for adjusting the bolt 52.
- the adjusting device 60 has a second passage 61, which is formed in the thickness direction or axial direction AR of the wheel disc 30 extending in this with internal thread (not designated), so that the first passage 53 with its second longitudinal end 53b in the second Passage 61 opens and a first longitudinal end 61 a of the second passage 61 in the lateral side 30 a of the wheel disc 30 opens.
- the adjusting device 60 also has a screw element 62 designed in the form of a hexagon socket screw (not designated), which is screwed from the lateral side 30a of the wheel disc 30 into the second passage 61 and which has a radially innermost end of the wheel Bolt 52b is in sliding contact, so that a displacement of the screw member 62 in the thickness direction or axial direction AR of the wheel disc 30 causes a displacement of the bolt 52 in the radial direction RR.
- a screw element 62 designed in the form of a hexagon socket screw (not designated), which is screwed from the lateral side 30a of the wheel disc 30 into the second passage 61 and which has a radially innermost end of the wheel Bolt 52b is in sliding contact, so that a displacement of the screw member 62 in the thickness direction or axial direction AR of the wheel disc 30 causes a displacement of the bolt 52 in the radial direction RR.
- a longitudinal end 62a of the screw member 62 provided for contact with the latch 52 is formed in a first tapered shape, and the radially innermost end 52b of the latch 52 is formed with a second tapered shape such that between respective circumferential surfaces of the first and second
- the first conical shape has a cone angle ⁇ of about 20 degrees.
- the second cone shape preferably has a cone angle (not designated) of about 70 degrees.
- the latch 52 is controllably controlled in the radial direction RR between an unlocking position (not shown in FIGS. 1 and 2) in which the latch 52 does not engage the recess 51 of the blade 40 and a latching position (as in FIGS 1 and 2), in which the latch 52 radially engages the recess 51 of the blade 40 so that it pushes the blade 40 radially outward with a predetermined force.
- Axial direction AR is closed on both sides with side walls, the bolt 52 provides in the locking position for the side walls of the recess 51 a two-sided stop in the thickness direction or axial direction AR, so that the blade 40 is fixed in the thickness direction or axial direction AR against movement.
- the blade 40 presses with a predetermined force radially outward, a game provided in the tooth profiles 33, 43 of the groove sides and the Schaufelfußdus for mounting and dismounting of the blade 40 in the groove 32 game and thus the blade under the action of a predetermined biasing force in
- Radial direction RR (radially outward) fixed in this direction against movement.
- the predetermined force or the predetermined prestressing force can be displaced radially outwards in a simple and repeatable manner, e.g. predefined by means of a torque wrench for actuating the screw member 62.
- the recess 51 is preferably formed in the form of an all-round material of the blade 40 and sidewalls delimited sink in the bottom 44 of the blade 40, wherein a provided for engagement in the recess 51 radially extreme end 52a of the bolt 52 is formed in its shape complementary to the shape of the recess 51.
- the recess 51 is formed as a Hüllkontur or negative to the outer contour of a spherical cap (or ball segment or ball portion), wherein the radially outermost end 52a of the bolt 52 one of the outer contour of this
- Recess 51 is formed as a spherical seat for the approximately hemispherical radially outermost end 52 a of the bolt 52.
- the impeller 20 is configured such that its moving blades 40 can be mounted and dismounted with less expenditure of time and can be fixed in their respective axially extending grooves 32 with a defined radial tension.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102012203606A DE102012203606A1 (en) | 2012-03-07 | 2012-03-07 | Impeller for a rotor of a turbomachine and rotor and turbomachine with such an impeller |
PCT/EP2013/053738 WO2013131774A1 (en) | 2012-03-07 | 2013-02-25 | Impeller for a rotor of a turbomachine, and rotor and turbomachine having an impeller of said type |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2823153A1 true EP2823153A1 (en) | 2015-01-14 |
EP2823153B1 EP2823153B1 (en) | 2018-07-25 |
Family
ID=47750694
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13706262.6A Not-in-force EP2823153B1 (en) | 2012-03-07 | 2013-02-25 | Impeller for a rotor of a turbomachine, and rotor and turbomachine having an impeller of said type |
Country Status (6)
Country | Link |
---|---|
US (1) | US9903205B2 (en) |
EP (1) | EP2823153B1 (en) |
JP (1) | JP6121455B2 (en) |
CN (1) | CN104160113B (en) |
DE (1) | DE102012203606A1 (en) |
WO (1) | WO2013131774A1 (en) |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB790350A (en) * | 1956-06-12 | 1958-02-05 | Gen Motors Corp | Improvements relating to elastic-fluid turbine wheels and the attachment of blades thereto |
US2807436A (en) * | 1952-03-25 | 1957-09-24 | Gen Motors Corp | Turbine wheel and bucket assembly |
US2846183A (en) * | 1952-07-18 | 1958-08-05 | William C Morgan | Retaining devices for turbine blades |
BE537113A (en) * | 1954-04-05 | |||
FR2120499A5 (en) * | 1971-01-06 | 1972-08-18 | Snecma | |
JPS59192801A (en) * | 1983-04-15 | 1984-11-01 | Hitachi Ltd | Easily detachable moving blade fixing method |
US4820127A (en) * | 1988-01-29 | 1989-04-11 | Westinghouse Electric Corp. | Blade support and blade assembly |
DE19603388C1 (en) * | 1996-01-31 | 1997-07-24 | Mtu Muenchen Gmbh | Device for fixing the blades on the impeller, in particular a turbine of a gas turbine engine, by riveting |
EP1619354B1 (en) * | 2004-07-22 | 2008-04-09 | Siemens Aktiengesellschaft | Device for fixing a blade on a rotor disc of a turbomachine, turbomachine and method to assemble and disassemble a blade on a rotor disc of a turbomachine. |
US8182230B2 (en) * | 2009-01-21 | 2012-05-22 | Pratt & Whitney Canada Corp. | Fan blade preloading arrangement and method |
-
2012
- 2012-03-07 DE DE102012203606A patent/DE102012203606A1/en not_active Withdrawn
-
2013
- 2013-02-25 US US14/383,369 patent/US9903205B2/en not_active Expired - Fee Related
- 2013-02-25 WO PCT/EP2013/053738 patent/WO2013131774A1/en active Application Filing
- 2013-02-25 CN CN201380012928.5A patent/CN104160113B/en not_active Expired - Fee Related
- 2013-02-25 EP EP13706262.6A patent/EP2823153B1/en not_active Not-in-force
- 2013-02-25 JP JP2014560303A patent/JP6121455B2/en active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2013131774A1 * |
Also Published As
Publication number | Publication date |
---|---|
CN104160113A (en) | 2014-11-19 |
US20150030456A1 (en) | 2015-01-29 |
EP2823153B1 (en) | 2018-07-25 |
WO2013131774A1 (en) | 2013-09-12 |
JP2015513032A (en) | 2015-04-30 |
US9903205B2 (en) | 2018-02-27 |
CN104160113B (en) | 2016-03-02 |
JP6121455B2 (en) | 2017-04-26 |
DE102012203606A1 (en) | 2013-09-12 |
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