1. Field of the Invention
This invention relates in general to railcars and, more particularly, to railcar yokes for a coupler system.
2. Brief Description of the Related Art
Railcar couplers are disposed at each end of a railway car to enable joining one end of such railway car to an adjacently disposed end of another railway car. The engageable portion of each of these couplers is known in the railway art as a knuckle. For example, railway freight car coupler knuckles are taught in U.S. Pat. Nos. 4,024,958; 4,206,849; 4,605,133; and 5,582,307.
Typically, adjacent railway cars are joined by heavy shafts extending from each car, known as couplers, and, generally, each coupler is engaged with a yoke housing a shock-absorbing element referred to as the draft gear. The type-E coupler is the standard coupler for railway freight cars. The type-E coupler has standard specifications such that producers making a type-E coupler adhere to a standard specification, so that the standard railway car couplers are completely interchangeable, regardless of the manufacturer. In addition, adherence to a standard also enables couplers from any one manufacturer to be able to be readily joined to couplers from any other domestic manufacturer. The Association of American Railroads (“AAR”) has adopted standards for railway couplers. The coupler must include specific geometry and dimensions that allow it to receive a knuckle, and the geometry must be such that the knuckle is allowed to freely operate when coupling and uncoupling railway cars. These dimensions and features of the coupler may be checked for compliance with AAR standards by using gauges, which are applied to the coupler to verify the coupler dimensions or parameters are within an allowable variation or tolerance range.
Couplers have a particular life, and in instances may fail. In many cases when a railcar coupler fails, a replacement coupler must be carried from the locomotive at least some of the length of the train, which may be up to 25, 50 or even 100 railroad cars in length. The repair of a failed coupler can be labor intensive, can sometimes take place in very inclement weather and can cause train delays.
The yoke is a generally elongated structure having two side sections that extend from and join with a tail portion. The side sections are also known and referred to as “straps”. The side sections or straps are joined at the opposite end by a head portion where the yoke is joined to the coupler with a securing component, such as a key or pin. The yoke generally has a pocket formed by the straps and a rear wall, and a draft gear is positioned between the straps of the yoke, and between the tail portion and the head portion. The best-known yokes are the E-type and F-type. The E-type yoke is governed by AAR standards that include the AAR S-143 Standard, SY 40AE, Y40 or YS93AE, for a 24⅝ inch gear pocket, although there are some tolerances that the pocket may have, as permitted by the standards. A typical E-type yoke has straps that are 5 inches. The F-type yoke is governed by the S-149 standard and the Y45 standard. Although there are other differences between E-type and F-type yokes, a primary difference is the design and orientation of the pin or key used to join the coupler to the yoke.
Typical yokes contain apertures in the yoke head portion, which also may be known as the key slots or pin bores by which a coupler is joined to the yoke with the installation of a key or pin through the slot or bore to connect the yoke and coupler. Adjacent railcars, when coupled together and in motion, place tension on the yoke and compressive forces are transferred to bearing surfaces at opposed ends of the yoke where the draft gear is housed.
Adjacent freight cars are separated in accordance with standard specifications which includes an allowance for a specified yoke length. In accordance with applicable AAR standards, typically, E-type and F-type yokes, respectively, may have a length of 41⅛″ or 37½″.
The present invention provides a railcar yoke for use in a coupler system.
A railcar coupler typically includes a coupler head portion extending from a shank portion. A yoke is designed to mount onto the sill of a railway vehicle and connect to the coupler shank portion. The coupler head portion is configured to couple to a first coupler knuckle for coupling the railcar coupler to a second railcar coupler of an adjacent railcar. The coupler head portion comprises a nose portion and a gathering face extending from the nose portion for engaging a second coupler knuckle coupled to the second railcar coupler.
Another object of the invention is to provide a lightweight yoke for use with railway couplers.
According to a preferred embodiment, a lightweight yoke is provided and is constructed from a material that is stronger than grade E cast steel. Is a further object to accomplish the above objects by providing a yoke that is constructed from a material that is at least as strong, or even stronger, than grade E cast steel but which is lighter in weight than grade E cast steel.
According to embodiments of the present invention, the yoke is stronger and more fatigue resistant than prior yokes of the same weight. According to one preferred embodiment, the yoke is lighter in weight than prior yokes (such as those constructed from grade E cast steel) and is both stronger and more fatigue resistant. According to a second preferred embodiment, the yoke possesses or exceeds the strength and fatigue resistance of prior yokes (such as those constructed from grade E cast steel) but is lighter in weight. According to a third preferred embodiment, the yoke is constructed having the same weight as prior yokes (such as those constructed from grade E cast steel), but with improved strength and fatigue resistance.
It is another object of the invention to accomplish the above objects by providing a yoke with an interior and/or exterior geometry that has one or more of coring (i.e., cavities) and ribs, or combinations thereof. Another object of the invention is to construct the yoke so that the maximum wall thickness preferably is about 1.25″ or less, and more preferably about 1.15″ or less, and with the yoke being constructed from a material that is lighter and of similar or greater strength than grade E cast steel. Preferred thicknesses for the yoke walls, according to some embodiments, are from about 0.25 inch to about 1.25 inches. According to preferred embodiments, the maximum wall thickness is defined as the maximum diameter of a sphere that can fit within the thickness of the part, such as, a wall of the yoke.
It is an object of the invention to provide a yoke that is constructed from an austempered metal. In a preferred embodiment, the austempered metal is austempered ductile iron (ADI). In another preferred embodiment the austempered metal is austempered steel, such as austempered alloy steel, and, according to other embodiments the coupler and yoke may be constructed from an austempered metal alloy.
The austempered ductile iron (ADI) yoke is produced by a suitable austempering process. For example, austempering of ductile iron may be accomplished by heat-treating cast ductile iron to which specific amounts of nickel, molybdenum, manganese or copper, or combinations thereof have been added to improve hardenability; the quantities of the elements needed to produce the ADI from ductile iron are related to the coupler configurations and, for example, may depend on the thickest cross-sectional area of the coupler or the yoke. Austempered steel and other austempered metals and austempered metal alloys, may be produced by any suitable austempering process. The yoke may be produced by casting, including sand casting or investment casting, or other suitable method. The casting of the yoke or formed yoke is austenitized by applying an austempering process on the yoke. For example, the yoke may be formed from a casting of ductile iron, and the ductile iron yoke casting austempered.
According to one embodiment, it is another object of the invention to provide an improved lightweight yoke that is lighter in weight than existing current yokes, but without additional coring or modifications to the interior of the yoke geometry, by constructing a yoke from an ADI having a density of about 0.26 lbs/in^3, which is less than that of grade E cast steel, 0.283 lbs/in^3. According to one embodiment, a casting of the same shape will be lighter and stronger when constructed from ADI versus grade E cast steel. According to a preferred embodiment, there is a weight reduction of about 8% using the ADI as the preferred material for the yoke versus using grade E cast steel.
Another benefit of the present invention is to provide a yoke, and process for producing the yoke that provides economic benefits of conservation of materials, without sacrificing strength. For example, the utilization of a preferred ADI material improves handling efficiencies (as iron is easier to pour than steel), and improves material usage, as the ADI material increases in volume, slightly, as the metal yoke casting cools compared to steel which shrinks. Accordingly, embodiments of the present invention provide a more efficient use of the materials, meaning less metal may be used to make the same final shape (for a yoke having substantially the same or greater strength as if a greater amount of metal were used), as a way of reducing the yoke weight.
In another preferred embodiment, the austempered metal is austempered steel.
Austempered steel is produced by a suitable austempering process. For example, austempering of steel may be accomplished by heat-treating cast steel to which specific amounts of chromium, magnesium, manganese, nickel, molybdenum, or copper, or combinations thereof have been added to improve hardenability; the quantities of the elements needed to produce the austempered steel from the cast alloy steel are related to the yoke configurations and, for example, may depend on the thickest cross-sectional area of the yoke.
According to another embodiment, a lighter weight yoke is constructed by selectively coring out material in thick load bearing areas (or alternatively otherwise reducing material in these areas when cores are not used) to provide an alternate interior and/or exterior geometry for the yoke so maximum wall thickness for the yoke is preferably about 1.15″ or less, and more preferably about 0.75″ or less.
According to preferred embodiments, the yoke may be reduced in thickness in a given zone or area, such as a wall and the strength to weight ratio may remain the same as or greater than prior yokes having thicker walls, and even being heavier in weight. According to some preferred embodiments, the maximum wall thickness of the yoke may be about 1.15 inches, and, according to some embodiments, the yoke may have walls with thicknesses about 0.75″ or less. According to some preferred embodiments, the yoke wall thickness may be in a range from about 0.25 inches to about 1.25 inches. The present yoke, when used in a coupling assembly, also may improve payload to weight ratios, as a lightweight yoke may allow for more weight to be cargo or other payload, especially where a locomotive is pulling a great number of cars that have lightweight yokes.
According to some preferred embodiments, the weight reduction may be made at the back, nose end sections or straps of the yoke, and may be accomplished with coring, such as, for example, exterior coring. Embodiments may be produced with reduced weight by providing exterior coring on the side and back sections of the keyslot walls, straps or rear or nose sections.
According to embodiments, the yoke may have one or more zones of coring and ribs, or apertures, bores and/or divots, where the coupler or yoke has areas or walls of a maximum cross-sectional thickness and other areas that are less than the maximum cross-sectional thickness.
The arrangement of coring (or cavities), ribs and wall thickness, may be provided to produce a yoke that is lighter in weight, but possesses sufficient strength, including meeting or exceeding railroad standards, such as AAR standards for yokes. In addition, the embodiments of the yoke may be produced from an austempered metal, such as, for example, austempered ductile iron, which is lighter in weight than grade E cast steel, but provides equal or greater strength, to provide a lightweight yoke that preferably is constructed from ADI and has an arrangement of ribs and/or coring (i.e., cavities).
According to another embodiment, a yoke may be provided having one or more zones of residual compressive stresses. According to one embodiment, a zone, or zones, of residual compressive stresses may be created on the entire inside and outside surface of any of the above embodiments of the lightweight yoke, while according to alternate embodiments, zones of residual compressive stresses may be created only in areas that show high tensile stress when the part is used, or combinations thereof in the areas that show high tensile stresses. For example, according to a preferred embodiment, a yoke is provided with zones of residual compressive stresses in the main areas that exhibit high tensile stress during use. According to some preferred embodiments, the yoke is configured having zones of residual compressive stresses which, according to preferred embodiments, may be in the location of the key slot, the side walls transitions in the front and back and the back tail section, or combinations of these locations.
According to one embodiment, a preferred method for creating residual compressive stresses is by shot peening. Shot peening involves impacting the surface with small media projected at high speeds at the desired surfaces. According to embodiments of the invention, an engineered surface is provided, such as, for example, by subjecting the surface to a treatment process, such as, for example, shot peening, in order to provide the yoke with an improved ability to counteract tensile stresses that are applied during use that may otherwise tend to cause crack initiation. The provisioning of the residual compressive stresses on the yoke, such as, for example, using the shot peening procedure to impart impacts on the surfaces of the yoke at one or more desired locations, increases fatigue life and performance without the need to increase the overall strength of materials or of the part.
The lightweight yokes according to the invention may be used with standard knuckles or lightweight knuckles, including, such as, for example, the lightweight knuckles disclosed in our co-pending U.S. patent application Ser. Nos. 13/378,021 and 13/842,229, for a lightweight fatigue resistant knuckle, the complete contents of which are herein incorporated by reference.
According to some implementations, the lightweight yokes may be used together with lightweight couplers, such as, for example, lightweight couplers disclosed in our co-pending U.S. patent application Ser. No. 13/678,203, the complete contents of which are herein incorporated by reference. Further a lightweight coupler knuckle may be used with one or more of the lightweight yoke and lightweight coupler to provide a lightweight coupling system.
Moreover, while specific advantages have been enumerated above, various embodiments may include all, some or none of the enumerated advantages.
The present invention provides improved yokes which have improved strength and fatigue life. One way in which embodiments of the invention accomplish this is by providing coring (i.e., cavities) that may include interior coring, external coring, or both. The coring referred to may be cavities formed by traditional methods (where cores are used and placed in a mold) or cavities formed using other methods for producing the yoke or coupler). Another way in which embodiments of the invention accomplish this is by constructing the yoke from a material that is stronger than the grade E cast steel currently used. A further way in which embodiments of the invention accomplish this is by utilizing a material to construct the yoke that is stronger and lighter than the grade E cast steel currently used, while other embodiments provide a lightweight yoke by providing a unique geometry and using a material that is lighter than the current cast steel and/or stronger than the current cast steel. The embodiments also may include ribs provided for strengthening areas or zones of the yoke, which, according to preferred embodiments, may be done in conjunction with coring (e.g., forming of cavities).
Referring to
According to one embodiment, a type F coupler yoke 210 is provided having a top strap 220 and bottom strap 221. The top strap 220 is shown having a head portion 222, and the bottom strap 221 also has a head portion 223. A rear portion 225 connects the top strap 220 and bottom strap 221 to form a central pocket 226 within the yoke 210. The pocket 226 is shown open at the two sides between the top and bottom straps 220, 221. A first pin hole 230 is provided extending through the head portion 222 of the top strap 220 and a second pin hole 231 is provided extending through the head portion 223 of the bottom strap 221. The pin holes 230, 231 are configured to receive a pin (not shown), and a draft gear (not shown) is provided and seated within the pocket 226. The yoke 210 may be installed by securing a coupler shank (not shown) to the yoke 210 with a pin (not shown) that is installed in the pin holes 230, 231. The yoke 210 preferably has lightener pockets 214, 215 at the rear portion 225. The yoke 210 has a draft gear seat 216 with a planar surface 217.
According to another preferred embodiment, an alternate configuration of yoke 310 is shown configured as a type E yoke. The yoke 310 has a butt end portion 313, and also preferably has lightener pockets 314, 315. A draft gear seat 316 is shown having a substantially planar face 317. Connected to the butt end portion 313 are top and bottom straps 320, 321, which span to the yoke head 322. The yoke 310 illustrated in
The yoke 310 may be configured with standard yoke contour dimensions for E-Type couplers (such as Y40 and Y41). According to preferred configurations, a yoke configured with the Y40 yoke dimension preferably has a draft gear pocket length of 25⅝ inches, and for a Y41 yoke configuration, the draft gear pocket length is 36⅜ inches long.
Alternate configurations may be made to the yoke 310 and yoke 210, including providing wall thicknesses that are reduced compared to current existing yokes, providing ribs or combinations of reduced wall thicknesses and ribs. The yokes 210 and 310 are shown as examples, and other configurations, preferably, yoke constructions meeting the standard geometries of AAR coupler yoke standards may be provided and produced in accordance with the present invention, including constructing the yoke to be lighter in weight and/or have thinner walls or wall portions, and more preferably, constructing the yokes from austempered metal.
Referring to
In
Referring to
A weight reduction zone “z3” preferably is provided in the rear of the yoke 410. The boxed area z3 illustrates a preferred location or zone of the yoke 410 where one or more weight reduction features are provided. The weight reduction zone z3 preferably is provided in the tail section of the yoke 410. According to one preferred embodiment, the wall thickness of the yoke 410 in the zone of weight reduction z3, and preferably in one or more, any or all, of the rear wall 419, draft gear seat 416, and strap portions 420,421 connecting with the rear wall 419, is preferably configured having a maximum thickness, measured corresponding with the spherical dimension, of a maximum spherical diameter of less than about 1.25 inches, more preferably, less than about 1.2 to 1.15 inches, and most preferred about or less than 0.75 inches. According to one embodiment, the weight reduction zone z3 includes a plurality of dimples, such as those dimples 481,482 shown in the top of the yoke 410, and the dimples 483,484, 485,486 shown in the wall 490 of the rib 413. Although the exemplary embodiment illustrated in
According to an alternate embodiment, ribs may be provided in the rear section of the yoke 410. For example, the weight reduction zone z3 may include a plurality of ribs in the locations at the top or bottom surfaces of the walls, such as, for example, the rear wall 419, the draft gear seat 416, or both. According to one embodiment, U-shaped ribs are provided running in the direction of the yoke, which in some embodiments may include crossing ribs that cross each other. A plurality of ribs may be provided in the tail section of the yoke 410.
Referring to
The yoke 510 may be configured with standard yoke contour dimensions for E-Type couplers (such as Y40 and Y41). According to preferred configurations, according to one exemplary embodiment, a yoke configured with the Y40 yoke dimension preferably has a draft gear pocket length of 24⅝ inches, and for a Y41 yoke configuration, the draft gear pocket length is 36 inches long. According to preferred embodiments, the draft gear pocket 526 preferably is sized and dimensioned in accordance with AAR specifications and standards to accommodate a draft gear and/or other components that may be installed for the coupling assembly. According to a preferred embodiment, the E-type yoke may have a preferred length of 41⅛″.
According to a preferred embodiment illustrated, openings 535,536 are provided in the respective straps 520,521. The openings 535,536 in the straps 520,521 preferably oppose each other. According to a preferred embodiment, the openings 535,536 are elongated to span across the straps 520,521. The openings 535,536 are shown having radiused ends and a straight elongated portion. The straps 520,521 may be constructed in accordance with an AAR standard, which in some preferred embodiments is 5 inches in height. The openings 535,536 are preferably provided within the 5 inches of strap height. According to a preferred embodiment, the height H1 of the openings 535,536 preferably are up to about one half of the strap height H2, as depicted according to a preferred embodiment shown in
According to one embodiment, the draft gear pocket 526 may be 25 inches (measured from a plane of the rear surface 513a to a plane of the draft gear pocket front walls 522,523). According to one preferred embodiment, the openings 535,536 are provided at a central location of the straps 520,521, relative to the strap height. According to one embodiment, the openings preferably are provided to be located within about 1.5 inches from the edge of a strap wall.
Referring to
According to a preferred embodiment, the thickness of the yoke walls preferably may be constructed to be from about 1.25 inches to about 0.25 inch. For example, the thickness of the walls forming the straps 520,521 may be from about 1 inch to 1.25 inches, with a preferred thickness of about 1.125 inches. According to some embodiments, the top and bottom walls 531,532 of the head portion 511 may have a wall thickness that is similar to the walls of the straps 520,521. Preferably the thickness of the keyslot walls 515,516 may be provided to be about 1.25 inches or less, and according to some preferred embodiments, the thickness of the keyslot walls 515,516 is about 1 inch. According to a preferred embodiment, the wall thicknesses of the key slot walls 515,516, the straps 520,521 and top and bottom walls 531,532 may be from about 1 inch to 1.25 inches, wherein each wall or strap pair may have a thickness within this range, which may be a different thickness than the other wall pair or strap pair. According to a preferred embodiment, each strap 520,521 preferably may have a uniform thickness along its length between joining locations (which is shown joining with the butt end 512 at one end thereof, where a radiused fillet may be provided (
According to a preferred embodiment, as illustrated, the yoke 510 has a butt end portion 512 disposed opposite the head portion 511. The butt end portion 512 is shown having radiused or curved edges 512b,512c, and a pair of pockets 550a,550b (see
Referring to
The yoke 610 is shown according to a preferred embodiment, with strap openings 635,636 provided in the respective straps 620,621. The strap openings 635,636 preferably oppose each other. According to a preferred embodiment, the strap openings 635,636 are elongated to span across the straps 620,621. The strap openings 635,636 are shown having radiused ends and a straight elongated portion. The straps 620,621 may be constructed in accordance with an AAR standard, which in some preferred embodiments is 5¾ inches in height (as viewed in
According to a preferred embodiment, the thickness of the walls of the yoke 610 preferably may be constructed to have thicknesses between about 1.25 inches to about 0.25 inch. For example, the thickness of the walls forming the straps 620,621 may be from about 1 inch to 1.25 inches, with a preferred thickness of about 1.125 inches. According to some embodiments, the top and bottom walls 617,618 of the head portion 611 may have a wall thickness that is similar to the walls of the straps 620,621. The top and bottom walls 617,618 may comprise extensions of the respective straps 620,621 and have similar thicknesses or, alternatively, have different thicknesses than the respective straps 620,621. Accordingly, the pin bores 615,616 preferably have a depth corresponding with the thickness of the respective top and bottom wall 615,616, or respective top or bottom strap 620,621. According to a preferred embodiment a positioning feature is provided at the yoke head portion 611. Referring to
According to a preferred embodiment, as illustrated, the yoke 610 has a butt end portion 612 disposed opposite the head portion 611. The butt portion 612 is shown having radiused or curved edges 612b,612c, and pockets 650a,650b provided in the butt end portion 612. According to preferred embodiments, the pocket arrangement includes a first pocket 650a and second pocket 650b. Referring to
According to a preferred embodiment, the front portion of the straps 620,621 may be constructed to slightly taper inwardly at the head portion 611. According to a preferred embodiment, the inwardly taper of the straps 620,621 preferably is after the front of the openings 635,636, and the straps 620,621 and head walls 617,618 that join with straps 620,621, respectively, also may have an inward taper. According to a preferred embodiment, a further inward taper of the front portions of the walls 617,618 may be provided, and the inward taper may include a portion of converging wall thickness in the front of each wall 617,618, preferably at each front flange 617b,618b.
According to some embodiments, the yoke 610 may be configured with standard yoke contour dimensions for F-Type yokes. According to preferred configurations, a yoke configured with the S-149 yoke dimension preferably has a draft gear pocket length of 24⅝ inches and a length of 37½ inches. The spacing between the straps 620,621, as depicted in
According to a preferred embodiment, the yokes 210,310,410,510,610 are constructed from an austempered metal, and more preferably, from austempered ductile iron (ADI). Although other austempered metals may be used, and other grades of ADI, according to a preferred embodiment, yokes may be constructed from Grade 3 ADI. According to a preferred embodiment, the ADI may be Grade 3 ADI in accordance with ASTM A897/A897M for ADI castings. According to some preferred embodiments, yokes 10,110 may have properties that meet or exceed the specifications for Grade 3 ADI.
The yoke preferably joins with a coupler that carries a pivotally connected knuckle movable between open and closed positions. According to alternate embodiments, the yokes 210, 310,410,510,610 may be made from austempered steel, which may be an austempered alloy steel. Other austempered metals, such as, for example, austempered ductile iron, and austempered metal alloys, may be used to construct the yokes 210,310,410,510,610. As discussed herein, the coupler, as well as the knuckle used in conjunction with the yoke 210,310,410,510,610 also may be constructed from austempered metal. As discussed above in connection with the couplers, preferred compositions, such as steel, as well as alloy steel compositions, e.g., alloyed preferably with magnesium, manganese, molybdenum, copper or mixtures thereof, or more preferably, with chromium, nickel or mixtures thereof, (or mixtures of the preferred and more preferred metals), may be used to form the yokes 210,310,410,510,610. The steel or preferred/more preferred alloy steel composition is austempered to obtain tensile strength, yield, and elongation properties for the inventive yokes which are suitable to meet or exceed the AAR standards for yokes utilized in coupling systems, including the current standard set forth by the American Association of Railroads (AAR) in AAR Manual of Standards and Recommended Practices, such as current standard M-211, M-205, M-220 NDT and Rule 88 of the AAR Office Manual, the complete contents of which are herein incorporated by reference. Like the couplers discussed herein, the yokes 210,310,410,510,610, according to preferred embodiments, may be constructed from ductile iron that is austempered. The ductile iron also may be used in alloy form, preferably, with nickel, molybdenum, manganese, copper, or mixtures thereof, to form the yokes 210, 310,410. The yokes 210.310.410.510,610 may be produced using any suitable production method. According to one method, the yoke 210,310,410,510,610 may be formed from a casting. For example, where the casting of the yoke is made from ductile iron, the ductile iron casting may be subjected to an austempering process to produce an austempered ductile iron yoke.
According to some embodiments, the yokes may be provided with one or more zones of reduced material, which, for example, where a casting process is used to form the yoke, may be accomplished by coring, and preferably, with specialized coring in designated zones of the yoke. Embodiments of the yoke may be provided with ribs for strengthening areas or zones of the yoke, and, according to some preferred embodiments, ribs may be provided in conjunction with coring. The ribs may be provided in configurations alternate to those preferred configurations shown and described herein. Although some embodiments of the present lightweight yoke may be constructed to resemble prior yoke geometries, including prior exterior yoke geometries, lightweight yokes according to the invention may be constructed to have geometries that are different than prior yokes but which also are compatible with coupling and usage of the prior yokes for connection with and use with prior and existing standard AAR couplers and other components of the coupling assembly. The lightweight yokes of the invention provide a lightweight alternative that may be used in place of prior yokes, wherever the prior yokes have been used or are called for.
According to preferred embodiments, the yokes may be made from a casting, although any suitable process for forming the yokes may be employed, including, for example, investment casting.
These and other advantages may be realized with the present invention. While the invention has been described with reference to specific embodiments, the description is illustrative and is not to be construed as limiting the scope of the invention. Moreover, while specific advantages have been enumerated above, various embodiments may include all, some or none of the enumerated advantages. The yokes may be formed by any suitable process, including, for example, molding, casting, and forging. The dimensions and thicknesses of the yokes, according to some preferred embodiments, are such that the yokes according to the invention, such as the yokes, 210,310,410,510,610 shown and described herein, may be used in standard coupling assemblies with other standard coupling assembly components, such as, for example, couplers, knuckles, locks and lock lifts. The improved yokes preferably may be interchangeable with prior yokes, and yokes according to the invention may meet or exceed AAR standards for yokes. Various modifications and changes may occur to those skilled in the art without departing from the spirit and scope of the invention described herein and as defined by the appended claims. It is intended that the foregoing detailed description be regarded as illustrative rather than limiting, and that it be understood that it is the following claims, including all equivalents, that are intended to define the spirit and scope of this invention.
It is intended that the foregoing detailed description be regarded as illustrative rather than limiting, and that it be understood that it is the following claims, including all equivalents, that are intended to define the spirit and scope of this invention. Numerous other changes, substitutions, variations, alterations and modifications may be ascertained by those skilled in the art and it is intended that the present invention encompass all such changes, substitutions, variations, alterations and modifications as falling within the spirit and scope of the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
2088135 | Johnson et al. | Jul 1937 | A |
4024958 | Kaufhold | May 1977 | A |
4081082 | Scherrer | Mar 1978 | A |
4206849 | Kaim | Jun 1980 | A |
4537304 | Kaim et al. | Aug 1985 | A |
4605133 | Altherr | Aug 1986 | A |
5096076 | Elliott et al. | Mar 1992 | A |
5320229 | Mautino et al. | Jun 1994 | A |
5511676 | Holmes | Apr 1996 | A |
5582307 | Hawthorne et al. | Dec 1996 | A |
5878897 | Lazzaro | Mar 1999 | A |
5900082 | Hewitt | May 1999 | A |
6796448 | Wilt et al. | Sep 2004 | B1 |
7926672 | Ely | Apr 2011 | B2 |
8607998 | McMillen et al. | Dec 2013 | B2 |
Entry |
---|
Brandenberg, Kristin; “Successfully Machining Austempered Ductile Iron (ADI)”; Applied Process Inc. Technologies Div.—Livonia, Michigan, USA; Oct. 2001. |
A. Kahn and B . K. Chen, “Evaluation of Grade 1 Austempered Ductile Iron for Application to Rail Cast Components”, Proceedings of the Fifth Asia Pacific Industrial Engineering and Management Systems Conference 2004. |
Luís Magalhães, Jorge Seabra, “Teeth Surface Failures in Austempered Ductile Iron (ADI) Gears”, Gears and Transmission Workshop, Paper No. XIII, p. 269-286, Faculdade de Engenharia da Universidade do Porto, Portugal, Jun. 5, 2003. |
SY40AE Yoke Publication. |
Y45AE Yoke Publication. |
Stokes, B. et al.; “Effects of Carbides on Fatigue Characteristics of Austempered Ductile Iron”, Metallurgical and Materials Transactions A, 36 (2005) 977-988. |
Bubenko et al.; “Fatigue Crack Propagation through Austempered Ductile Iron Microstructure”; Materials Engineering, vol. 17, 2010, No. 3, p. 15-20. |
Bubenko et al.; “Fatigue Crack Propagation Within the Austempered Ductile Iron Microstructure”; Acta Metallurgica Slovaca, vol. 17, 2011, No. 1, p. 18-25. |
Dundar, Sacit; “Application of Austempered Ductile Iron to Rail Wheel Sets”; Journal of Engineering Sciences 2003, 9 (3), p. 283-287. |
International ADI and Simulation Conference; May 28-30, 1997. |
SAIFoundry; “Austempered ductile iron production properties”; http://www.slideshare.net/SAIFoundry/austempered-ductile-iron-production-properties-applications#; Mar. 19, 2012. |
Keough, J. R. et al; Continuing Developments in the Science and Application of Austempered Ductile Iron (ADI). |
Number | Date | Country | |
---|---|---|---|
20140360965 A1 | Dec 2014 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 13678021 | Nov 2012 | US |
Child | 14329593 | US | |
Parent | 13678203 | Nov 2012 | US |
Child | 13678021 | US |