GB2030269A - Shaft coupling - Google Patents
Shaft coupling Download PDFInfo
- Publication number
- GB2030269A GB2030269A GB7929749A GB7929749A GB2030269A GB 2030269 A GB2030269 A GB 2030269A GB 7929749 A GB7929749 A GB 7929749A GB 7929749 A GB7929749 A GB 7929749A GB 2030269 A GB2030269 A GB 2030269A
- Authority
- GB
- United Kingdom
- Prior art keywords
- splines
- shaft
- hub
- members
- coupling according
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
- F16D1/08—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key
- F16D1/0876—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key with axial keys and no other radial clamping
-
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/10—Quick-acting couplings in which the parts are connected by simply bringing them together axially
- F16D2001/103—Quick-acting couplings in which the parts are connected by simply bringing them together axially the torque is transmitted via splined connections
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
In a coupling (9) between a hub (10) and a shaft (11) internal splines (12) of the hub are interdigitated with external splines (13) of the shaft. The splines are helical. The hub and shaft are further connected by axial pins (14) arranged in bores (15) which are parallel to the common axis (16) of the hub and the shaft and which intersect the interdigitated splines. A screw (21) in the hub engages an end (24) of the shaft. When the screw is tightened the hub is drawn along the shaft. The different helix angles of the splines and pins (the latter having a helix angle of zero) result in that the hub becomes locked against axial movement on the shaft and the splines of the hub are urged circumferentially into engagement with the splines of the shaft thereby to take up circumferential clearance between them. The force applied by the screw applies compression to the shaft and tension to the hub so that Poisson's Law operates to close radial clearance between the hub and the shaft. Alternative constructions using fingered or splined rings instead of the pins (14) are described. <IMAGE>
Description
SPECIFICATION
Shaft coupling
This invention relates to shaft couplings.
It is known to provide a coupling between a hub and a shaft comprising axial splines having flanks which transmit torque between the hub and the shaft, and further comprising a shoulder on the shaft at one end of the hub and a nut on the shaft at the other end of the hub whereby to clamp the hub axially against the shoulder. In such a coupling it is not always possible to establish firm contact between the torque-transmitting flanks of the splines. It is an object of this invention to reduce or overcome this difficulty.
According to this invention there is provided a shaft coupling comprising two relatively inner and outer members having a common axis, means defining first surfaces provided on the respective members in circumferentially confronting relationship, means defining second surface provided on the respective members in circumferentially confronting relationship, the first and second surfaces extending at different helix angles relative said axis, urging means for urging the members relatively axially, said first and second surfaces co-operating to lock the members against relative axial movement and to impart to the members opposing circumferential forces urging the members into engagement at said first and second surfaces respectively.
A particular difficulty of the known arrangement is that the force applied by the nut places the shaft into tension and the hub into compression. Under these circumstances the diameter of the shaft ends to reduce in accordance with Poisson's Law. This may result in radial separation between the hub and the shaft. If the spline flanks are inclined to the radial, said radial separation also results in circumferential separation of the flanks of the splines and further increases the difficulty of establishing firm contact between those flanks. The nut has to be done up with high torque to ensure safety against release, and the greater that torque the greater the separation of the flanks. It is a particular object of this invention to overcome this difficulty.
Accordingly, the invention includes a coupling in which the said means for urging the members relatively axially are arranged to place the outer member into tension and the inner member into compression.
Other more specific aspects of the invention will become apparent from the following description and claims.
Examples of this invention will now be described with reference to the accompanying drawings wherein: Fig. lisa diagrammatic side elevation of a gas turbine power plant embodying a shaft coupling according to this invention.
Fig. 2 is an enlarged sectional detail of Fig. 1 and shows a first example of the coupling.
Fig. 3 is a developed section on the line Ill-Ill in Fig. 1.
Fig. 4 is a section on the line IV--IV in Fig. 1 further enlarged.
Fig. 5 is a view similar to Fig. 2 but showing a second example of the coupling.
Fig. 6 is a developed section on the line VI--VI in Fig. 5.
Fig. 7 is a view similar to Fig. 2 but showing a third example of the coupling.
Fig. 8 is a developed section on the line VIll-VIll in Fig. 7.
Fig. 9 is a developed section on the line IX-IX in Fig. 7.
Figs. 1 0 and 11 are views similar to Figs. 8 and 9, respectively, but showing a modification.
Referring to Fig. 1, the power plant comprises a gas turbine engine 7 having an output 11 connected to drive a fan 8 through a coupling 9.
Referring now also to Figs. 2 to 4, the coupling 9 comprises an outer member or hub 10 having
internal helical splines 1 2 interdigitated with external helical splines 13 of an inner member constitued by the shaft 11. The members 1 0, 11 have a first pair of confronting surfaces being
respectively helical surfaces 1 2A of the splines 1 2
and helical surfaces 1 3A of the splines 13. The surfaces 1 2A, 1 3A are in direct engagement and transmit the torque of the shaft 11 to the hub 10.
The surfaces 1 2A, 1 3A have a helix angle a with the common axis 16 of the members 10,11. At
least three cylindrical intermediate members on
pins 1 4 are arranged in respective bores 1 5 which
are parallel to the axis 1 6 and which intersect the
splines 1 2, 13. The members 10, 11 have a
second pair of confronting surfaces being the
surfaces 12B, of the bores 15 lying
respectively in the splines 12, 13. The surfaces 1 2B, 1 3B are spaced circumferentially from the
surfaces 1 2A, 1 3A and are or course separated by
the intermediate members 14.A screw 21
arranged in a nut thread 22 in the hub 10 has an
end 23 abutting a confronting end 24 of the shaft
11 so that when the screw is tightened it applies
an axial force F 1 against the shaft end and an
opposite force F2 urging the hub 10 axially along
the shaft in a direction toward the end 24. In view
of the different helix angles of the surface 1 2A,
1 3A and 12B, 1 3B (the helix angle of the surfaces 1 2B, 1 3B is of course zero) the forces F1, F2 co
operate to wedge the hub against the axial
movement on the shaft.As a result there occurs a
circumferential component force F3 urging the
surfaces 1 2A of the hub against the surface 1 3A
of the shaft and an opposite circumferential force
F4 transmitted through the pins 1 4 between the
surfaces 1 2B, 1 2B. The forces F3, F4 eliminate
any circumferential clearance betwen the splines 12, 13, in particular between the driving surfaces 1 2A, 1 3A. A circumferential force F5 applied by
the shaft to rotate the fan can therefore act on the
hub without encountering any said clearance. A
force F6 being the aerodynamic load on the fan 8
acts in the same sense as the force F2 applied by
the screw and reinforces the effect thereof, i.e.
contributes to the firmness of engagement of the
driving surface 1 2A, 1 3A. This means that the screw need only be tightened with a relatively moderate pre-load torque to produce an initial loading of the surfaces 12A, 13A. Nevertheless, when the stresses produced by the screw 21 are taken into account it will be noted that the screw places the shaft 11 into compression and the hub
10 into tension. This means that the outside diameter of the shaft tends to increase while the inside diameter of the hub tends to decrease thereby to improve the engagement between the splines 12, 13 especially insofar as the flanks of these splines, i.e. the surfaces 12A, 12B, are inclined to the radial as shown by the angle p in
Fig. 4.The screw 21 is connected to the hub by a conventional locking device, not shown, to prevent release of the screw due to vibration. However, if it should happen that the screw is accidentally released, the hub is still retained on the shaft by the pins 14. A shoulder 1 9 and a circular clip 20 both on the hub 10, retain the pins 14 against sliding from the bores 1 5. For disassembly, when the screw 10, clip 20 and pins 14 are removed, the hub 10 can be drawn readily over the end 24 of the shaft, the reverse operations appiying for reassembly.
To aid illustration, regions where there is no pressure between surfaces due to the forces Fl, F2 are indicated to an exaggerated extent as clearances, e.g. at 1 8, 1 8A in Fig. 3.
Referring to the example shown in Figs. 5 and 6, a coupling 109 comprises a hub 110 having internal splines 112 interdigitated with external splines 113 of a shaft 111.
The spines 112 have helical first surfaces 1 12A confronting and engaging helical first surfaces 1 of the splines 113. The surfaces 11 2A, 11 3A have a helix angle a. Further the splines 112 have axial second surfaces 11 2B confronting axial second surfaces 1 13B of the splines 113 in spaced apart relationship thereto.
Being axial, the surfaces 1 12B, 11 3B, may be regarded as having a zero helix angle. Each two confronting axial surfaces 11 2B, 11 3B are separated by an axially extending intermediate member 114 required to make possible assembly and dis-assembly of the hub as explained later hereinbelow. The members 114 are integral with a ring 117 abutting an end 124 of the shaft and retained in position by a clip 120. When a screw 121 in the hub 110 is tightened against the ring 117 the hub 110 is urged axially along the shaft 111 and toward the end 1 24 thereof by a force
F2.The different helix angles of the surfaces 112A, 113Aand li2B, 112B,113B co-operate to wedge the splines 11 2 between the splines 113 and the members 114. As a result there occurs a circumferential force F3 urging the surfaces 11 2A against the surfaces 1 13A and an opposite circumferential force F4 transmitted by the members 114 between the surfaces 1 12B, 1 13B.
A circumferential force F5 applied by the shaft 111 to rotate the fan 1 8 can therefore act on the hub without encountering any clearance between the driving surfaces, i.e. the surfaces 1 12A, 1 13A of the splines. The aerodynamic force F6 on the fan 18 acts in the same sense as the force F2 applied by the screw, and combines with that force to maintain the wedging action and thus retain firm engagement at the surfaces 11 2A, 11 3A. As in the example of Figs. 2 to 4, the screw 121 applies compression to the shaft 111 and tension to the hub 110 with the beneficial effects stated.
Removal of the hub 110 from the shaft 111 requires removal of the screw 121 and clip 120, and withdrawal of the ring 117 together with the inserts 114. The hub 110 is then free to be slid from the shaft over the end 124 thereof. It will be seen that each spiine 112 is a wedge having a wide and a narrow end 112W and 11 2N situated respectively remote from and adjacent to the end
124 of the shaft. The removal of the members 114 enables the wide ends 112W to pass, as shown in chain-dotted lines (Fig. 6), through the relatively narrow clearance between the splines
113 at the end 1 24 of the shaft.Correspondingly, on assemly, the inserts 114 are necessary for filling the clearance which unavoidably occurs between the splines 112,113 when the hub is in the assembled position shown in full line.
Referring to the example shown in Figs. 7 to 10, a coupling 209 comprises a hub 210 having internal splines 212 interdigitated with external helical splines 213 of a shaft 211. The splines 212 have helical first surfaces 21 2A confronting and engaging helical first surfaces 21 3A of the splines 213. The surfaces 21 2A, 21 3A have a helix angle . Further the hub 210 has internal axial splines 230 interdigitated with external splines 231 of an annular intermediate member 214 which has internal axial splines 232 interdigited with external splines 233 of the shaft 211. The splines 230, 231 are spaced axially from the splines 212,213 and have confronting and engaging second surfaces 212B,213B. The shaft 211 has an end 224 engaged by a screw 221 in the hub 210.
When the screw is tightened the hub 210 is urged axially along the shaft toward the end 224 thereof by a force F2. The different helix angles of the surfaces 212A, 213A and 212B, 213B cause the hub to be locked axially on the shaft 211 and generate a circumferential force F3 urging the surfaces 21 2A against the surfaces 213A. A corresponding opposite force F4 occurs at the surfaces 21 2B, 21 3B. The forces F3, F4 eliminate any clearance between the driving surfaces, i.e.
the surfaces 21 2A, 21 3A of the hub and the shaft.
The member 214, having axial splines, is easily removed or inserted during dis-assembly or assembly of the hub. Effectively, the member 21 4 forms part of the shaft 211, the splines 232, 233 being provided to make possible withdrawal and insertion of the member 214 for purposes of disassembly and re-assembly. The splines 232,233 may be replaced by any convenient form of securing the member 214 to the shaft 211. It is also to be noted that the intermediate member 21 4 is located in position between the screw 221 and the end 214 of the shaft although a clip 220 is provided as an additional safeguard for retaining the member 214.
In the modification shown in Figs. 11 and 12, the helical splines 212, 213 of Figs. 7 to 10 are replaced by axial splines 312, 313 and the axial splines 230, 231, of Figs. 7 to 10 are replaced by helical splines 330, 331.
Claims (10)
1. Shaft coupling comprising two relatively inner and outer members having a common axis, means defining first surfaces provided on the respective members in circumferentially confronting relationship, means defining second surfaces provided on the respective members in circumferentially confronting relationship, the first and second surfaces extending at different helix angles relative to said axis, urging means for urging the members relatively axially, said first and second surfaces co-operating to lock the members against relative axial movement and to impart to the members opposing circumferential forces urging the members into engagment at said first and second surfaces respectively.
2. Coupling according to claim 1 wherein the means for urging the members relatively axially are arranged to place the outer member into tension and the inner member into compression.
3. Coupling according to claim 1 wherein the helix angle of one of said first and second surfaces is zero.
4. Coupling according to claim 1 wherein said first and second surfaces are arranged in circumferentially spaced relationship.
5. Coupling according to claim 1 wherein said first and second surfaces are arranged in axially spaced relationship.
6. Coupling according to claim 4 comprising an intermediate member situated between said second surfaces.
7. Coupling according to claim 6 comprising internal splines provided in the outer member, external splines provided on the inner member and interdigitated with the internal spiines, said first surfaces being constituted by confronting helical surfaces of the inner and outer splines, said second surfaces being defined by confronting but circumferentially spaced apart axial surfaces of the splines, and said intermediate member being situated between said axial surfaces.
8. Coupling according to claim 6 wherein the first surfaces are defined by helical splines and the second surfaces are defined by opposite sides of an axial opening intersecting the first surfaces and containing said intermediate member. Figs. 2 to 4.
9. Coupling according to claim 5 comprising an intermediate member releasably supported on the inner member against rotation relative thereto, and said second surfaces being defined respectively on the inner member and the intermediate member.
10. Coupling according to claim 9 comprising first spline means arranged to connect the members and defining said first surfaces, second spline means spaced axially from the first spline means and arranged to connect the outer member to said intermediate member and defining said second surfaces, and means for releasably securing the intermediate member to the inner member.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7929749A GB2030269B (en) | 1978-09-19 | 1979-08-28 | Shaft coupliner |
IT7925769A IT1123193B (en) | 1978-09-19 | 1979-09-17 | COUPLING JOINT FOR SHAFTS |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7837310 | 1978-09-19 | ||
GB7929749A GB2030269B (en) | 1978-09-19 | 1979-08-28 | Shaft coupliner |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2030269A true GB2030269A (en) | 1980-04-02 |
GB2030269B GB2030269B (en) | 1983-04-27 |
Family
ID=26268898
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7929749A Expired GB2030269B (en) | 1978-09-19 | 1979-08-28 | Shaft coupliner |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB2030269B (en) |
IT (1) | IT1123193B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2309504A (en) * | 1996-01-26 | 1997-07-30 | Fichtel & Sachs Ag | Stabiliser means for a motor vehicle suspension |
US7008191B2 (en) | 2002-10-24 | 2006-03-07 | Holset Engineering Company, Limited | Compressor wheel assembly |
RU2506428C1 (en) * | 2012-10-15 | 2014-02-10 | Открытое акционерное общество "Авиадвигатель" | Multistage gas turbine |
US8864406B2 (en) | 2008-10-07 | 2014-10-21 | Rolls-Royce Plc | Splined couplings |
-
1979
- 1979-08-28 GB GB7929749A patent/GB2030269B/en not_active Expired
- 1979-09-17 IT IT7925769A patent/IT1123193B/en active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2309504A (en) * | 1996-01-26 | 1997-07-30 | Fichtel & Sachs Ag | Stabiliser means for a motor vehicle suspension |
GB2309504B (en) * | 1996-01-26 | 2000-09-13 | Fichtel & Sachs Ag | Stabiliser means for a motor vehicle suspension |
US7008191B2 (en) | 2002-10-24 | 2006-03-07 | Holset Engineering Company, Limited | Compressor wheel assembly |
US8864406B2 (en) | 2008-10-07 | 2014-10-21 | Rolls-Royce Plc | Splined couplings |
RU2506428C1 (en) * | 2012-10-15 | 2014-02-10 | Открытое акционерное общество "Авиадвигатель" | Multistage gas turbine |
Also Published As
Publication number | Publication date |
---|---|
GB2030269B (en) | 1983-04-27 |
IT7925769A0 (en) | 1979-09-17 |
IT1123193B (en) | 1986-04-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4292001A (en) | Shaft coupling | |
US4268185A (en) | Mounting attachment | |
US4367053A (en) | Clamping device | |
US4134699A (en) | Coupling for shafts and the like | |
JP3577610B2 (en) | Pin type synchronizer mechanism | |
US3366208A (en) | Synchronizer | |
US2550580A (en) | Flexible coupling for shafts and the like | |
GB2026650A (en) | Mounting Parts on Shafts | |
US3717367A (en) | Unitary hub-shaft interconnection assembly | |
US4134700A (en) | Zero clearance spline coupling | |
EP1053413B1 (en) | Improvements in power sharing gear sets | |
KR920011797A (en) | Synchronizer with Deep Spline and Improved Ramp | |
US4395247A (en) | Shaft coupling | |
US6648763B2 (en) | Reduction of axial thrust reaction in toothed shear-type flexible couplings | |
US5131782A (en) | Shaft coupling for gas turbine engine | |
GB2030269A (en) | Shaft coupling | |
US4701068A (en) | Spline anti-backlash device | |
US10697489B1 (en) | Snap ring having retention feature | |
US3524665A (en) | Shaft coupling | |
US3760605A (en) | Toothed disk coupling of a shaft to a hub | |
US6419063B1 (en) | Self-energizing synchronizer | |
US4619150A (en) | Sliding gear for speed-changing transmission | |
KR19980024642A (en) | Pin Synchronizer | |
US3720429A (en) | Coupling | |
KR19980024639A (en) | Pin Synchronizer |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |