US3077811A - Continuous retaining ring adapted for radial expansion - Google Patents
Continuous retaining ring adapted for radial expansion Download PDFInfo
- Publication number
- US3077811A US3077811A US4825460A US3077811A US 3077811 A US3077811 A US 3077811A US 4825460 A US4825460 A US 4825460A US 3077811 A US3077811 A US 3077811A
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- United States
- Prior art keywords
- annulus
- portions
- working edge
- plastically deformable
- expanded
- 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 - Lifetime
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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
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/326—Locking of axial insertion type blades by other means
-
- 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
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- 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
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49908—Joining by deforming
- Y10T29/49938—Radially expanding part in cavity, aperture, or hollow body
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T292/00—Closure fasteners
- Y10T292/20—Clamps
- Y10T292/205—Ring
- Y10T292/212—With expanding or contracting means
Definitions
- This invention relates to a retaining ring for use in the assembly of mechanical parts.
- the preferred form of ring which will be described in detail below to exemplify the invention has been developed as a retaining ring especially suited for securing the blades in turbine and compressor rotors, but, as will also be evident from the description which follows, the retaining ring of the invention is inherently capable of establishing other mechanical connections that can be formed by a retaining ring adapted for expansion and contraction as desired.
- retaining ring used in the past is the resilient ring that can be snapped into locking position.
- resilient members and devices have the disadvantage that they are unsuitable under certain environmental conditions. Normal spring steel loses its temper and resilience when subjected to radioactive radiation, for example. The same result flows from exposure of the steel to high temperatures or to the thermal fatigue of operation over a large temperature range.
- a retaining ring as a continuous annulus defining a main plane extending transverse to the axis about which the annulus is described, said annulus having a peripheral working edge and a plurality of mutually circumferentially spaced expansion zones disposed around the annulus, each of said zones comprising a portion of the annulus spaced radially from the working edge, said portions being plastically deformable between contracted and expanded conditions, the expanded condition being such that the plastically deformable portions all lie in said main plane and the working edge is in an expanded condition of maximum circumference, and the contracted condition being such that the plastically deformable portions are each displaced axially from said main plane and the working edge is in a contracted condition of lesser circumference than such maximum circumference.
- FIGURE 1 is a front elevation view of a first form of retaining ring according to the invention, showing the ring in its contracted condition;
- FIGURE 2 is an enlarged view of a small zone of the ring shown in FIGURE 1;
- FIGURE 3 is a section on the line IIIIII in FIG- URE 2;
- FIGURE 4 is a section on the line IV-IV in FIG- URE 2;
- FIGURES 5, 6 and 7 correspond respectively to FIG- URES 2, 3 and 4, but show the ring in its expanded condition, FIGURES 6 and 7 being sections on the lines VIVI and VII-VII respectively in FIGURE 5;
- FIGURE 8 is a front view of a portion of the ring of FIGURES 1 to 7 shown in its expanded condition in a turbine rotor;
- FIGURE 9 is a view on the line IX--IX in FIG- URE 8.
- FIGURE 10 is a view of a portion of an alternative construction of retaining ring, showing the ring in its expanded condition;
- FIGURE 11 is a further view of the portion of ring shown in FIGURE 10, but in the contracted condition.
- FIGURES l to 4. show a retaining ring in the form of a continuous annulus 10.
- the steel of which the annulus is constructed is generally rectangular in cross-section, and the annulus may be said to define a single main plane P extending transversely of the central axis about which the annulus is described.
- the annulus 10 has a substan tially continuous, working," outer peripheral edge 11 which is designed to be expanded into an inwardly facing slot, as will later appear.
- Disposed around the annulus 10 at convenient, spaced intervals is a series of expansion zones, one of which is shown within the rectangle R of FIGURE 1 and on a large scale in FIGURES 2 to 7.
- expansion zones are all alike, and each comprises a portion 12 which is spaced radially inwardly from the working edge 11 and which is plastically deformable between an expanded and contracted condition.
- Each portion 12 is shown in its contracted condition in FIGURES 1 to 4 and in its expanded condition in FIGURES 5 to 7.
- the contracted condition is such that the plastically deformable portion 12 is displaced axially from the main plane P (as FIGURES 3 and 4 demonstrate).
- the working edge 11 is also in a contracted condition of minimum circumference.
- auxiliary edge portions 13 which about one another in the contracted condition of the annulus to render the working edge 11 effectively continuous.
- all the deformable portions 12 are hammered or otherwise forced to lie in the main plane P (FIGS. 5 to 7), which action separates the ends of the auxiliary edge portions 13 and causes the working edge 11 to adopt a maximum effective circumference.
- the reference to an expanded and a contracted condition thus refers principally to the condition of the annulus as a whole, and in particular to its working edge 11; however, for convenience of description, the deformable portions 12 are considered each to have an expanded and a contracted condition corresponding respectively to the expanded and contracted conditions of the annulus.
- the metal of which the annulus 10 is constructed must necessarily be plastically deformable, and one of the readily available, comparatively ductile mild steels is well suited to the purpose. Any tendency to springiness or resiliency in the material should be avoided, since, as explained above, one of the essential advantages of the present invention is that it does not depend on the maintenance of resilience in the metal.
- annulus 10 An important practical consideration in the construction of the annulus 10 is the maintenance of a substantially uniform cross-section around the periphery, or at least a cross-section having no sudden or sharp changes in shape or area. Undesirable stress concentrations are avoided in this way and distortion of the ring under extreme temperature conditions is not experienced. It should be noted that, in determining the effective cross-section of the annulus 10 at any point around its periphery, the auxiliary edge portions 13 should be ignored, since they do not 3 form part of the continuous, stress-transmitting metal of the annulus. The proper comparison is between the cross-section of the deformable portions 12 and the crosssection of the intermediate portions 15 which extend between each of the expansion zones.
- the annulus is relieved (cut away) in circumferential alignment with the deformable portions 12 to render the cross-section of the intermediate portions less than it would otherwise be.
- FIG- URES 8 and 9 One convenient manner in which the ring of FIGURES l to 7 may be employed in practice, is illustrated in FIG- URES 8 and 9 where the annulus it ⁇ is shown in expanded condition with its working edge 11 expanded into a slot 16 formed beneath the overhanging ends 17 of rotor members 18 between which slots are formed to receive and retain the blade roots 19. Radial movement of the blades out of the slots is prevented by the undercut shape of the slots, in the usual way, the retaining rings 1% serving to prevent axial sliding of the blade roots 19 out of these slots.
- each of the deformable portions 12 is struck a blow or series of blows to deform it plastically into its expanded condition.
- all the expansion zones are expanded simultaneously, this being accomplished by using a specially constructed annular punch to engage all the deformable portions .12 simultaneously, hammer blows or other thrust on this punch forcing all the portions 12 axially substantially simultaneously.
- each portion 12 may be deformed independently using simply a hammer and punch.
- FIGURES l0 and 11 the ring consists of an annulus 20 formed with a working edge 21 which this time is formed at the inner periphery instead of the outer periphery where the working edge 11 appeared.
- the annulus 20 is provided around its periphery with a series of expansion zones, only one of which is shown in FIGURES 10 and 11.
- Each such expansion zone comprises a plastically deformable portion 22 generally similar to the plastically deformable portions 12.
- FIGURE 10 shows a portion 22 in its expanded condition, lying flat in the main plane P, while FIGURE 11 shows a portion 22 deformed into its contracted condition distorted axially from said main plane.
- Auxiliary edge portions 23 are provided, as before, and these are separated from the deformable portion 22 by a slot 24.
- Intermediate portions 25 interconnect adjacent expansion zones.
- each of the deformable portions 22 is moved from its expanded to its contracted condition, after the ring has been placed in position with the parts requiring to be retained, whereas the deformable portions 12 of the first embodiment of the invention are each moved from contracted to expanded condition when the ring is used for its intended function.
- Such deformation of portions 22 to their contracted conditions will preferably also be carried out simultaneously by the application of the necessary thrust applied through a tool designed to bear simultaneously on each such portion 22 only of the ring 29.
- each portion 22 may be deformed independently by the application of a suitable vice grip.
- a retaining ring according to the invention is merely intended to illustrate one possible application.
- the device hasapplication in any assembly in which parts are to be held in place by means of a ring that can be moved between a locking and a release position by being expanded and contracted, or vice versa.
- the ring may either be expanded or contracted into its locking position.
- a retaining ring comprising a continuous annulus defining a main plane extending transverse to the axis about which the annulus is described, said annulus having a peripheral working edge and a plurality of mutaily circumferentially spaced expansion zones disposed around the annulus, each of said zones comprising a portion of the annulus spaced radially from the working edge, said portions being plastically deformable between contracted and expanded conditions, a pair of auxiliary edge portions located at each expansion zone and lying in said main plane radially spaced from the plastically deformable portion of said expansion zone, said auxiliary edge portions projecting towards each other from the portions of said annulus on each side of the plastically deformable portion of said expansion zone andforrning continuations of said working edge whereby to render the same nearly continuous even in the expanded condition, the expanded condition being such that the plastically deformable portions all lie in the same main plane and the working edge is in an expanded condition of maximum circumference, and the contracted condition being such that the plastically deformable portions are displaced axially
- a retaining ring according to claim 1 wherein said working edge is the outer peripheral edge of the annulus, said plastically deformable portions being spaced radially inwardly from said edge.
- a retaining ring according to claim 1 wherein said working edge is the inner peripheral edge of the annulus, said plastically deformable portions being spaced radially outwardly from said edge.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Description
Feb. 19, 1963 E. SQFMOORE I 3,077,811
CONTINUOUS RETAINING Rm ADAPTED FOR RADIAL EXPANSION Filed Aug. 8. 1960 2 Sheets-Sheet 1 Feb. 19, 1963 E. s. MOORE 3,077,811
CONTINUOUS RETAINING RING ADAPTED FOR RADIAL EXPANSION Filed Aug. 8, 1960 2 Sheets-Sheet 2 Amway United States Patent Office 3,077,811 Patented Feb. 19, 1963 3,077,811 CONTINUOUS RETAINING RING ADAPTED FOR RADIAL EXPANSION Ernest S. Moore, Ottawa, Ontario, Canada, assignor to National Research Council, Ottawa, Ontario, Canada,
a body corporate of Canada Filed Aug. 8, 1960, Ser. No. 48,254 Claims. (Cl. 858.6)
This invention relates to a retaining ring for use in the assembly of mechanical parts.
The preferred form of ring which will be described in detail below to exemplify the invention has been developed as a retaining ring especially suited for securing the blades in turbine and compressor rotors, but, as will also be evident from the description which follows, the retaining ring of the invention is inherently capable of establishing other mechanical connections that can be formed by a retaining ring adapted for expansion and contraction as desired.
The most common form of retaining ring used in the past is the resilient ring that can be snapped into locking position. However, resilient members and devices have the disadvantage that they are unsuitable under certain environmental conditions. Normal spring steel loses its temper and resilience when subjected to radioactive radiation, for example. The same result flows from exposure of the steel to high temperatures or to the thermal fatigue of operation over a large temperature range.
In order to provide a retaining ring not subject to these disadvantages, it is the primary object of the present invention to construct a device which, while performing satisfactorily as a retaining ring, is constructed of an essentially non-resilient material.
This object is achieved according to the invention by forming a retaining ring as a continuous annulus defining a main plane extending transverse to the axis about which the annulus is described, said annulus having a peripheral working edge and a plurality of mutually circumferentially spaced expansion zones disposed around the annulus, each of said zones comprising a portion of the annulus spaced radially from the working edge, said portions being plastically deformable between contracted and expanded conditions, the expanded condition being such that the plastically deformable portions all lie in said main plane and the working edge is in an expanded condition of maximum circumference, and the contracted condition being such that the plastically deformable portions are each displaced axially from said main plane and the working edge is in a contracted condition of lesser circumference than such maximum circumference.
Further features of the invention will appear from the specific description below of two forms of retaining ring constructed in accordance with the present invention. In connection with such specific description, reference should be made to the accompanying drawings, in which:
FIGURE 1 is a front elevation view of a first form of retaining ring according to the invention, showing the ring in its contracted condition;
FIGURE 2 is an enlarged view of a small zone of the ring shown in FIGURE 1;
FIGURE 3 is a section on the line IIIIII in FIG- URE 2;
FIGURE 4 is a section on the line IV-IV in FIG- URE 2;
FIGURES 5, 6 and 7 correspond respectively to FIG- URES 2, 3 and 4, but show the ring in its expanded condition, FIGURES 6 and 7 being sections on the lines VIVI and VII-VII respectively in FIGURE 5;
FIGURE 8 is a front view of a portion of the ring of FIGURES 1 to 7 shown in its expanded condition in a turbine rotor;
FIGURE 9 is a view on the line IX--IX in FIG- URE 8;
FIGURE 10 is a view of a portion of an alternative construction of retaining ring, showing the ring in its expanded condition; and
FIGURE 11 is a further view of the portion of ring shown in FIGURE 10, but in the contracted condition.
Reference will first be made to FIGURES l to 4. These figures show a retaining ring in the form of a continuous annulus 10. The steel of which the annulus is constructed is generally rectangular in cross-section, and the annulus may be said to define a single main plane P extending transversely of the central axis about which the annulus is described. The annulus 10 has a substan tially continuous, working," outer peripheral edge 11 which is designed to be expanded into an inwardly facing slot, as will later appear. Disposed around the annulus 10 at convenient, spaced intervals, is a series of expansion zones, one of which is shown within the rectangle R of FIGURE 1 and on a large scale in FIGURES 2 to 7.
These expansion zones are all alike, and each comprises a portion 12 which is spaced radially inwardly from the working edge 11 and which is plastically deformable between an expanded and contracted condition. Each portion 12 is shown in its contracted condition in FIGURES 1 to 4 and in its expanded condition in FIGURES 5 to 7. The contracted condition is such that the plastically deformable portion 12 is displaced axially from the main plane P (as FIGURES 3 and 4 demonstrate). As a result, the working edge 11 is also in a contracted condition of minimum circumference.
So that the working edge 11 will always form an almost completely continuous circle, notwithstanding the fact that the deformable portions 12 are radially inwardly spaced from it, there is arranged outwardly of each of the deformable portions 12 a pair of auxiliary edge portions 13 which about one another in the contracted condition of the annulus to render the working edge 11 effectively continuous. These auxiliary edge portions 13 lie at all times in the main plane P, being separated from their associated deformable portion 12 by a slot 14.
To bring the working edge 11 to the expanded condition, all the deformable portions 12 are hammered or otherwise forced to lie in the main plane P (FIGS. 5 to 7), which action separates the ends of the auxiliary edge portions 13 and causes the working edge 11 to adopt a maximum effective circumference. The reference to an expanded and a contracted condition thus refers principally to the condition of the annulus as a whole, and in particular to its working edge 11; however, for convenience of description, the deformable portions 12 are considered each to have an expanded and a contracted condition corresponding respectively to the expanded and contracted conditions of the annulus.
The metal of which the annulus 10 is constructed must necessarily be plastically deformable, and one of the readily available, comparatively ductile mild steels is well suited to the purpose. Any tendency to springiness or resiliency in the material should be avoided, since, as explained above, one of the essential advantages of the present invention is that it does not depend on the maintenance of resilience in the metal.
An important practical consideration in the construction of the annulus 10 is the maintenance of a substantially uniform cross-section around the periphery, or at least a cross-section having no sudden or sharp changes in shape or area. Undesirable stress concentrations are avoided in this way and distortion of the ring under extreme temperature conditions is not experienced. It should be noted that, in determining the effective cross-section of the annulus 10 at any point around its periphery, the auxiliary edge portions 13 should be ignored, since they do not 3 form part of the continuous, stress-transmitting metal of the annulus. The proper comparison is between the cross-section of the deformable portions 12 and the crosssection of the intermediate portions 15 which extend between each of the expansion zones.
As FIGURES 2 and 5 demonstrate, the annulus is relieved (cut away) in circumferential alignment with the deformable portions 12 to render the cross-section of the intermediate portions less than it would otherwise be.
One convenient manner in which the ring of FIGURES l to 7 may be employed in practice, is illustrated in FIG- URES 8 and 9 where the annulus it} is shown in expanded condition with its working edge 11 expanded into a slot 16 formed beneath the overhanging ends 17 of rotor members 18 between which slots are formed to receive and retain the blade roots 19. Radial movement of the blades out of the slots is prevented by the undercut shape of the slots, in the usual way, the retaining rings 1% serving to prevent axial sliding of the blade roots 19 out of these slots.
To assemble the ring with the other parts, it is brought into alignment with the slot 16 while still in its contracted condition, and then each of the deformable portions 12 is struck a blow or series of blows to deform it plastically into its expanded condition. Preferably all the expansion zones are expanded simultaneously, this being accomplished by using a specially constructed annular punch to engage all the deformable portions .12 simultaneously, hammer blows or other thrust on this punch forcing all the portions 12 axially substantially simultaneously. Alternatively, each portion 12 may be deformed independently using simply a hammer and punch.
The embodiment of the invention so far described invoives a retaining ring which is expanded into its locking position, and this will be the more usual form of retaining ring required in practice. It is nevertheless within the scope of the present invention for a retaining ring to be contracted into its working position and a section of such an alternative form of ring is shown in FIGURES l0 and 11. Here, the ring consists of an annulus 20 formed with a working edge 21 which this time is formed at the inner periphery instead of the outer periphery where the working edge 11 appeared. As in the case of the annulus 10, the annulus 20 is provided around its periphery with a series of expansion zones, only one of which is shown in FIGURES 10 and 11. Each such expansion zone comprises a plastically deformable portion 22 generally similar to the plastically deformable portions 12. FIGURE 10 shows a portion 22 in its expanded condition, lying flat in the main plane P, while FIGURE 11 shows a portion 22 deformed into its contracted condition distorted axially from said main plane. Auxiliary edge portions 23 are provided, as before, and these are separated from the deformable portion 22 by a slot 24. Intermediate portions 25 interconnect adjacent expansion zones.
In addition to its reversal of structure, the alternative form of ring shown in FIGURES 10 and 11 is differently used in practice, since each of the deformable portions 22 is moved from its expanded to its contracted condition, after the ring has been placed in position with the parts requiring to be retained, whereas the deformable portions 12 of the first embodiment of the invention are each moved from contracted to expanded condition when the ring is used for its intended function. Such deformation of portions 22 to their contracted conditions will preferably also be carried out simultaneously by the application of the necessary thrust applied through a tool designed to bear simultaneously on each such portion 22 only of the ring 29. Alternatively, each portion 22 may be deformed independently by the application of a suitable vice grip.
The example given herein of one practical use of a retaining ring according to the invention is merely intended to illustrate one possible application. The device hasapplication in any assembly in which parts are to be held in place by means of a ring that can be moved between a locking and a release position by being expanded and contracted, or vice versa. Depending on which peripheral edge is chosen as the working edge, the ring may either be expanded or contracted into its locking position. Thus, in referring herein, and in the appended claims, to the deformable portions, and hence the annulus as a whole, being movable between contracted and expanded conditions, movement in both directions (i.e. both towards expanded, and towards contracted) is contemplated.
I claim:
1. A retaining ring comprising a continuous annulus defining a main plane extending transverse to the axis about which the annulus is described, said annulus having a peripheral working edge and a plurality of mutaily circumferentially spaced expansion zones disposed around the annulus, each of said zones comprising a portion of the annulus spaced radially from the working edge, said portions being plastically deformable between contracted and expanded conditions, a pair of auxiliary edge portions located at each expansion zone and lying in said main plane radially spaced from the plastically deformable portion of said expansion zone, said auxiliary edge portions projecting towards each other from the portions of said annulus on each side of the plastically deformable portion of said expansion zone andforrning continuations of said working edge whereby to render the same nearly continuous even in the expanded condition, the expanded condition being such that the plastically deformable portions all lie in the same main plane and the working edge is in an expanded condition of maximum circumference, and the contracted condition being such that the plastically deformable portions are displaced axially from said main plane and the working edge is in a contracted condition of lesser circumference than such maximum circumference 2. A retaining ring according to claim 1, wherein the effective, stress-transmitting cross-section of said annulus is substantially constant around its entire extent, and is free from sudden changes of shape.
3. A retaining ring according to claim 1, wherein said working edge is the outer peripheral edge of the annulus, said plastically deformable portions being spaced radially inwardly from said edge.
4. A retaining ring according to claim 1, wherein said working edge is the inner peripheral edge of the annulus, said plastically deformable portions being spaced radially outwardly from said edge.
'5. A retaining ring according to claim 1, wherein the intermediate portions of said annulus lying between the expansion zones are relieved in circumferential alignment with said deformable portions.
References Cited in the file of this patent UNITED STATES PATENTS
Claims (1)
1. A RETAINING RING COMPRISING A CONTINUOUS ANNULUS DEFINING A MAIN PLANE EXTENDING TRANSVERSE TO THE AXIS ABOUT WHICH THE ANNULUS IS DESCRIBED, SAID ANNULUS HAVING A PERIPHERAL WORKING EDGE AND A PLURALITY OF MUTALLY CIRCUMFERENTIALLY SPACED EXPANSION ZONES DISPOSED AROUND THE ANNULUS, EACH OF SAID ZONES COMPRISING A PORTION OF THE ANNULUS SPACED RADIALLY FROM THE WORKING EDGE, SAID PORTIONS BEING PLASTICALLY DEFORMABLE BETWEEN CONTRACTED AND EXPANDED CONDITIONS, A PAIR OF AUXILIARY EDGE PORTIONS LOCATED AT EACH EXPANSION ZONE AND LYING IN SAID MAIN PLANE RADIALLY SPACED FROM THE PLASTICALLY DEFORMABLE PORTION OF SAID EXPANSION ZONE, SAID AUXILIARY EDGE PORTIONS PROJECTING TOWARDS EACH OTHER FROM THE PORTIONS OF SAID ANNULUS ON EACH SIDE OF THE PLASTICALLY DEFORMABLE PORTION OF SAID EXPANSION ZONE AND FORMING CONTINUATIONS OF SAID WORKING EDGE WHEREBY TO RENDER THE SAME NEARLY CONTINUOUS EVEN IN THE EXPANDED CONDITION, THE EXPANDED CONDITION BEING SUCH THAT THE PLASTICALLY DEFORMABLE PORTIONS ALL LIE IN THE SAME MAIN PLANE AND THE WORKING EDGE IS IN AN EXPANDED CONDITION OF MAXIMUM CIRCUMFERENCE, AND THE CONTRACTED CONDITION BEING SUCH THAT THE PLASTICALLY DEFORMABLE PORTIONS ARE DISPLACED AXIALLY FROM SAID MAIN PLANE AND THE WORKING EDGE IS IN A CONTRACTED CONDITION OF LESSER CIRCUMFERENCE THAN SUCH MAXIMUM CIRCUMFERENCE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US4825460 US3077811A (en) | 1960-08-08 | 1960-08-08 | Continuous retaining ring adapted for radial expansion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US4825460 US3077811A (en) | 1960-08-08 | 1960-08-08 | Continuous retaining ring adapted for radial expansion |
Publications (1)
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US3077811A true US3077811A (en) | 1963-02-19 |
Family
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US4825460 Expired - Lifetime US3077811A (en) | 1960-08-08 | 1960-08-08 | Continuous retaining ring adapted for radial expansion |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3853413A (en) * | 1974-02-07 | 1974-12-10 | Gen Motors Corp | Snap ring locking device |
US3874675A (en) * | 1973-08-20 | 1975-04-01 | Dana Corp | Metallic gasket assembly |
US4326835A (en) * | 1979-10-29 | 1982-04-27 | General Motors Corporation | Blade platform seal for ceramic/metal rotor assembly |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US4566857A (en) * | 1980-12-19 | 1986-01-28 | United Technologies Corporation | Locking of rotor blades on a rotor disk |
US4767276A (en) * | 1986-12-19 | 1988-08-30 | General Electric Company | Retainer ring |
US4781534A (en) * | 1987-02-27 | 1988-11-01 | Westinghouse Electric Corp. | Apparatus and method for reducing windage and leakage in steam turbine incorporating axial entry blade |
US4836750A (en) * | 1988-06-15 | 1989-06-06 | Pratt & Whitney Canada Inc. | Rotor assembly |
US5082454A (en) * | 1989-09-28 | 1992-01-21 | Joslyn Corporation | Two-piece retaining ring |
EP0609979A1 (en) * | 1993-02-03 | 1994-08-10 | ROLLS-ROYCE plc | Balanced rotor for a gas turbine engine |
FR2729709A1 (en) * | 1995-01-25 | 1996-07-26 | Snecma | Turbine rotor seal and retainer |
US20060225257A1 (en) * | 2005-04-08 | 2006-10-12 | John Michelon | Snap ring |
US20080253895A1 (en) * | 2007-04-12 | 2008-10-16 | Eugene Gekht | Blade retention system for use in a gas turbine engine |
US20130156590A1 (en) * | 2010-06-25 | 2013-06-20 | Snecma | Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping |
US20140030100A1 (en) * | 2008-11-25 | 2014-01-30 | Gaurav K. Joshi | Axial retention of a platform seal |
US20220268163A1 (en) * | 2019-05-20 | 2022-08-25 | Cross Manufacturing Company (1938) Limited | Ring fastener |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1694354A (en) * | 1927-10-13 | 1928-12-04 | Wheeling Steel Corp | Shipping drum |
US2860540A (en) * | 1957-03-20 | 1958-11-18 | Gadget Of The Month Club Inc | Continuous bearing retainer ring adapted for radial expansion |
-
1960
- 1960-08-08 US US4825460 patent/US3077811A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US1694354A (en) * | 1927-10-13 | 1928-12-04 | Wheeling Steel Corp | Shipping drum |
US2860540A (en) * | 1957-03-20 | 1958-11-18 | Gadget Of The Month Club Inc | Continuous bearing retainer ring adapted for radial expansion |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874675A (en) * | 1973-08-20 | 1975-04-01 | Dana Corp | Metallic gasket assembly |
US3853413A (en) * | 1974-02-07 | 1974-12-10 | Gen Motors Corp | Snap ring locking device |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US4326835A (en) * | 1979-10-29 | 1982-04-27 | General Motors Corporation | Blade platform seal for ceramic/metal rotor assembly |
US4566857A (en) * | 1980-12-19 | 1986-01-28 | United Technologies Corporation | Locking of rotor blades on a rotor disk |
US4767276A (en) * | 1986-12-19 | 1988-08-30 | General Electric Company | Retainer ring |
US4781534A (en) * | 1987-02-27 | 1988-11-01 | Westinghouse Electric Corp. | Apparatus and method for reducing windage and leakage in steam turbine incorporating axial entry blade |
US4836750A (en) * | 1988-06-15 | 1989-06-06 | Pratt & Whitney Canada Inc. | Rotor assembly |
US5082454A (en) * | 1989-09-28 | 1992-01-21 | Joslyn Corporation | Two-piece retaining ring |
EP0609979A1 (en) * | 1993-02-03 | 1994-08-10 | ROLLS-ROYCE plc | Balanced rotor for a gas turbine engine |
FR2729709A1 (en) * | 1995-01-25 | 1996-07-26 | Snecma | Turbine rotor seal and retainer |
US20060225257A1 (en) * | 2005-04-08 | 2006-10-12 | John Michelon | Snap ring |
US20080253895A1 (en) * | 2007-04-12 | 2008-10-16 | Eugene Gekht | Blade retention system for use in a gas turbine engine |
US7806662B2 (en) | 2007-04-12 | 2010-10-05 | Pratt & Whitney Canada Corp. | Blade retention system for use in a gas turbine engine |
US20140030100A1 (en) * | 2008-11-25 | 2014-01-30 | Gaurav K. Joshi | Axial retention of a platform seal |
US9840931B2 (en) * | 2008-11-25 | 2017-12-12 | Ansaldo Energia Ip Uk Limited | Axial retention of a platform seal |
US20130156590A1 (en) * | 2010-06-25 | 2013-06-20 | Snecma | Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping |
US9422818B2 (en) * | 2010-06-25 | 2016-08-23 | Snecma | Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping |
US20220268163A1 (en) * | 2019-05-20 | 2022-08-25 | Cross Manufacturing Company (1938) Limited | Ring fastener |
US11512603B2 (en) * | 2019-05-20 | 2022-11-29 | Cross Manufacturing Company (1938) Limited | Ring fastener |
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