GB2066904A - Blade locking system - Google Patents
Blade locking system Download PDFInfo
- Publication number
- GB2066904A GB2066904A GB8041018A GB8041018A GB2066904A GB 2066904 A GB2066904 A GB 2066904A GB 8041018 A GB8041018 A GB 8041018A GB 8041018 A GB8041018 A GB 8041018A GB 2066904 A GB2066904 A GB 2066904A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pins
- locking system
- balls
- axial
- pin
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Abstract
Axial displacement of the pins (3) connecting the webs (1) of a rotor rim with the roots of blades (7) is prevented by at least one locking system formed from balls (4) in complementary annular grooves (5) in the pin (3) and the web (1). The balls may be inserted into each groove through an aperture which is then plugged. The pin may be prestressed. <IMAGE>
Description
SPECIFICATION
Lockingsystem to prevent axial displacement of pins connecting the webs of a rotor disc and blade roots in turbines and similar machines
This invention relates to a locking system to prevent axial displacement of pins connecting the webs of a rotor disc rim and the tenon roots of the moving blades of a turbine and similar machines.
Axial locking arrangements are known in which the pins are riveted. While riveting has proved successful in many instances, it presents difficulties in the case of larger pins, especially because of the material used. Another method of locking the pins axially is caulking or deforming the outer edges of the holes.
An object of the present invention is to provide an axial locking system without riveting or caulking so as to obtain a connection between the pins and the outer wheel disc webs which is effective in both axial directions and which will resist the bending moments and axial forces arising.
The invention provides a locking system to prevent axial displacement of pins connecting the webs of a wheel disc ring and tenon roots of moving blades in turbines, compressors and similar machines, wherein each pin is held in its respective hole by at least one form-locking system comprising an annular peripheral groove in the pin, a complementary annular groove in the hole, and a plurality of balls engaging both holes thereby preventing axial movement of the pin in the hole.
Not only is axial locating of the pins obtained, but the line contact between the balls and the annular grooves will compensate for any non-uniform stresses - occurring due to eccentric force application - by local plastic flow. Furthermore, there is now a great selection of materials for the pins, because riveting is dispensed with.
Preferably, each pin is held by two form-locking systems each comprising the complementary grooves and the balls in the outer webs of the wheel disc. Thus axial spreading of the wheel head and/or outward bending of the outer wheel webs and loosening of the root fixing is prevented.
Since the annular grooves acting as ball races will deform plastically under high loads, there would be some play between the balls and their allied race as stress is increased. In order to obviate such play, the pins maybe prestressed. This anticipates expected plastification.
Preferably, the or each locking system comprises a filler groove through which the balls may be inserted into the complementary annular grooves, the or each filler groove being closable after insertion of the balls. This prevents the balls dropping out during transport or similar operations.
Two embodiments of the invention will now be described with reference to the accompanying drawings, in which:
Figure 1 is a cut-out of a side view of a lowpressure rotor disc provided with a locking system in accordance with the invention,
Figure 2 is a section taken along the line A-A in
Figure 1, and
Figure 3 is a section similarto Figure 2 of a rotor disc and blade provided with two locking systems.
A wheel disc rim 1 has webs provided with cylindrical holes 2 through which cylindrical pins 3 are inserted to fix the tenon roots of the moving blades at the base. The pins 3 are locked axially by a form-locking system using small balls 4 of, say, 3 to 5 mm diameter which are arranged in corresponding annular grooves 5 lying perpendicular to the pin axis. The annular grooves 5 are each formed by two semi-circular grooves, one of which is provided in the pin 3 and the other of which is provided in the outer web of the wheel disc rim 1. The balls 4 are inserted into the grooves via a filler groove 6 arranged parallel to the corresponding hole axis.
This filler groove 6 is closable by a plugging fastener, e.g. a notched pin (not shown). As a rule, the annular grooves 5 are completely filled with balls 4.
In order to lock the pins 3 against axial displacement, it is only necessary to provide the formlocking system on one side. However, to avoid spreading of the wheel head rim the form-locking system may be used on both sides, i.e. in at least both of the outer webs as shown in Figure 3. Here the interlocking of the base of the blade 7 with the webs 1 is clearly shown.
In addition, the pins 3 may be prestressed in a manner known per se (axially), for instance, as in the case of bolted joints.
Such a locking system may be used in axial-flow turbines or compressors whose moving blades are subjected to high centrifugal stresses, e.g. long exhaust blades of the low-pressure elements of steam turbines of a high unit output, moving blades of gas turbines, axial-flow compressors in jet engines and similar machines.
1. A locking system to prevent axial displacement of pins connecting the webs of a wheel disc ring and tenon roots of moving blades in turbines, compressors and similar machines, wherein each pin is held in its respective hole by at least one form-locking system comprising an annular peripheral groove in the pin, a complementary annular groove in the hole, and a plurality of balls engaging both holes thereby preventing axial movement of the pin in the hole.
2. A locking system as claimed in Claim 1, wherein each pin is held by two form-locking systems each comprising the complementary grooves and the balls in the outer webs of the wheel disc.
3. An axial locking system as claimed in Claim 1 or 2, wherein the pins are prestressed.
4. An axial locking system as claimed in Claim 1, 2 or 3, wherein the or each locking system comprises a filler groove through which the balls may be inserted into the complementary annular grooves, the or each filler groove being closable after insertion of the balls.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (5)
1. A locking system to prevent axial displacement of pins connecting the webs of a wheel disc ring and tenon roots of moving blades in turbines, compressors and similar machines, wherein each pin is held in its respective hole by at least one form-locking system comprising an annular peripheral groove in the pin, a complementary annular groove in the hole, and a plurality of balls engaging both holes thereby preventing axial movement of the pin in the hole.
2. A locking system as claimed in Claim 1, wherein each pin is held by two form-locking systems each comprising the complementary grooves and the balls in the outer webs of the wheel disc.
3. An axial locking system as claimed in Claim 1 or 2, wherein the pins are prestressed.
4. An axial locking system as claimed in Claim 1, 2 or 3, wherein the or each locking system comprises a filler groove through which the balls may be inserted into the complementary annular grooves, the or each filler groove being closable after insertion of the balls.
5. An axial locking system substantially as herein described with reference to Figures 1 and 2, or
Figure 3 of the accompanying drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19792951838 DE2951838C2 (en) | 1979-12-21 | 1979-12-21 | Axial securing of a collarless bolt in the bores of the wheel disk head webs and the blade plug-in feet of axial steam turbines and the like. |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2066904A true GB2066904A (en) | 1981-07-15 |
GB2066904B GB2066904B (en) | 1984-01-11 |
Family
ID=6089306
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8041018A Expired GB2066904B (en) | 1979-12-21 | 1980-12-22 | Blade locking system |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPS56101005A (en) |
CH (1) | CH650835A5 (en) |
DD (1) | DD155445A1 (en) |
DE (1) | DE2951838C2 (en) |
FR (1) | FR2484530B1 (en) |
GB (1) | GB2066904B (en) |
SE (1) | SE446281B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2622643A1 (en) * | 1987-11-02 | 1989-05-05 | Mitsubishi Electric Corp | MEANS FOR STOPPING A GEAR OF A MOTOR STARTER |
US5062769A (en) * | 1989-11-22 | 1991-11-05 | Ortolano Ralph J | Connector for turbine element |
US6422667B2 (en) | 1999-06-28 | 2002-07-23 | Komatsu Limited | Link-and-pin fixing structure for a crawler chain |
US20110110786A1 (en) * | 2008-07-04 | 2011-05-12 | Man Diesel & Turbo Se | Rotor Blade and Flow Engine Comprising a Rotor Blade |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191517310A (en) * | 1915-12-09 | 1916-11-23 | Edward Sydney Luard | Improvements in and relating to Means for Coupling together Shafts and other Parts. |
US3043563A (en) * | 1957-04-16 | 1962-07-10 | Aerpat Ag | Turbine rotor mounting |
GB911370A (en) * | 1958-01-06 | 1962-11-28 | D W Price Corp | Improvements in and relating to locking devices |
GB929039A (en) * | 1959-09-07 | 1963-06-19 | Aerpat Ag | Improvements in and relating to releasable locking devices |
DE1500655A1 (en) * | 1966-04-30 | 1969-11-27 | Bosch Gmbh Robert | Detachable connection of machine parts |
FR1598815A (en) * | 1968-01-31 | 1970-07-06 | ||
US3507532A (en) * | 1968-04-04 | 1970-04-21 | Us Navy | Closure means |
DE2757570A1 (en) * | 1977-12-23 | 1979-06-28 | Mahle Gmbh | Oil guide bush contained in gudgeon pin - is fixed by its own recesses and recesses in gudgeon pin wall accommodating ball or wire retainers |
FR2438193A1 (en) * | 1978-10-03 | 1980-04-30 | Bedue Abel | Plug-type sealed pressure joint - in which O=rings are located axially by row of balls inserted in split groove |
-
1979
- 1979-12-21 DE DE19792951838 patent/DE2951838C2/en not_active Expired
-
1980
- 1980-11-15 CH CH846580A patent/CH650835A5/en not_active IP Right Cessation
- 1980-11-26 FR FR8025038A patent/FR2484530B1/en not_active Expired
- 1980-12-18 SE SE8008960A patent/SE446281B/en not_active IP Right Cessation
- 1980-12-18 DD DD22626480A patent/DD155445A1/en unknown
- 1980-12-19 JP JP17910080A patent/JPS56101005A/en active Pending
- 1980-12-22 GB GB8041018A patent/GB2066904B/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2622643A1 (en) * | 1987-11-02 | 1989-05-05 | Mitsubishi Electric Corp | MEANS FOR STOPPING A GEAR OF A MOTOR STARTER |
US5062769A (en) * | 1989-11-22 | 1991-11-05 | Ortolano Ralph J | Connector for turbine element |
US6422667B2 (en) | 1999-06-28 | 2002-07-23 | Komatsu Limited | Link-and-pin fixing structure for a crawler chain |
US20110110786A1 (en) * | 2008-07-04 | 2011-05-12 | Man Diesel & Turbo Se | Rotor Blade and Flow Engine Comprising a Rotor Blade |
US8974187B2 (en) * | 2008-07-04 | 2015-03-10 | Man Diesel & Turbo Se | Rotor blade and flow engine comprising a rotor blade |
Also Published As
Publication number | Publication date |
---|---|
DE2951838A1 (en) | 1981-09-03 |
CH650835A5 (en) | 1985-08-15 |
JPS56101005A (en) | 1981-08-13 |
SE8008960L (en) | 1981-06-22 |
DD155445A1 (en) | 1982-06-09 |
FR2484530B1 (en) | 1985-11-22 |
FR2484530A1 (en) | 1981-12-18 |
GB2066904B (en) | 1984-01-11 |
SE446281B (en) | 1986-08-25 |
DE2951838C2 (en) | 1982-12-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |