Patent Application
20220412406
The present disclosure relates to formation of steel components. More specifically, the present disclosure relates to hammer bushings or other tubular components formed with a relatively hard inner region proximal to an inner surface.
Machines are in widespread use in construction, mining, forestry, and other similar industries. These machines often include a variety of tools thereon, such as a hydraulic hammer tool or hydraulic breaker. The hydraulic hammer tool is used to repeatedly impact objects, such as concrete, with a hammer to break-up or demolish the object. For example, a hydraulic hammer tool may be provided on an excavator and used to break through a portion of road (e.g., asphalt) or sidewalk (e.g., concrete). The hydraulic hammer tool includes a hammer with a head that impacts objects that are to be hammered. The hammer moves up and down within a housing of the hydraulic hammer tool and is generally kept in alignment by a bushing of the hydraulic hammer tool.
The hammer, therefore, is in contact with the bushing and, during use, imparts forces onto the bushing. As a result, the hammer imparts tribological wear on the inner surface of the bushing. Such hydraulic hammer tools can operate in extremely adverse environments in which hydraulic hammer tools, and the components therein, may be exposed to various abrasive mixtures of water, dirt, sand, rock or other mineral or chemical elements. Thus, hydraulic hammer tools, operating under harsh conditions, may grind the inner diameter of the bushing, resulting in reduced lifetime of the bushing components. Wear of the bushings results in having to replace the bushings that can involve costly in-the-field downtime and maintenance.
Due to the consequences of excessive wear on the inner surface of the bushings, it is desirable to have a relatively hard inner diameter of the bushings. This improves the wear resistance of the bushing and its operable lifetime. However, if the entirety of the bushing is hardened, the bushing may be relatively less tough and may crack during use. Thus, it is desirable to have a bushing with a relatively hard inner
region, proximal to the inner surface and a relatively soft outer region proximal to the outer surface.
An example of producing a bushing with a relatively high level of inner surface hardness is described in U.S. Pat. No. 10,493,610 (hereinafter referred to as the '610 reference), where a bushing with surface hardening by carburization is disclosed. For example, the bushing may be subject to a carburizing treatment, followed by a quench and tempering treatment. However, this process of the '610 reference includes additional steps, such as a carburizing process, which add processing time and cost in the manufacture of the bushings. Additionally, in this process of steel surface hardening, as described in the '610 reference, specialized equipment may be required to perform the carburization process.
Example embodiments of the present disclosure are directed toward overcoming the deficiencies described above.
In an example of the disclosure, a bushing includes an inner surface and an outer surface. The bushing further includes a bulk region disposed between the inner surface and the outer surface, the bulk region proximal to the outer surface, the bulk region having a bulk carbon concentration. The bushing still further includes an inner region disposed between the inner surface and bulk region, the inner region having an inner region carbon concentration, wherein the inner region has a hardness of at least about 60 Rockwell Hardness Scale C (HRC), the bulk region has a hardness in the range of about 35 HRC to about 45 HRC, and the bulk carbon concentration and the inner region carbon concentration are substantially the same.
In another example of the disclosure, a method of manufacturing a bushing includes forming a rough bushing with steel having a carbon content greater than about 0.58% by weight, the rough bushing having an inner surface and an outer surface opposing the inner surface. The method further includes heating the rough bushing to a temperature of at least about 760° C. and quenching the rough bushing directly from the temperature at which the heating is performed to form a hardened bushing. The method still further includes tempering the hardened bushing at a temperature in a range of about 450° C. to about 570° C. to form a softened bushing, induction heating the softened bushing along the inner surface, and quenching the softened bushing to form an inner region proximal to the inner surface, the inner region harder than the outer surface of the bushing.
In still another example of the disclosure, a machine includes a component The component includes an inner surface, an outer surface, and a bulk region disposed between the inner surface and the outer surface, the bulk region proximal to the outer surface, the bulk region having a bulk carbon concentration. The component further includes an inner region disposed between the inner surface and bulk region, the inner region having an inner region carbon concentration, wherein the inner region has a hardness of at least about 60 Rockwell Hardness Scale C (HRC), the bulk region has a hardness in the range of about 35 HRC to about 45 HRC, and the bulk carbon concentration and the inner region carbon concentration are substantially the same.
Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts.
The machine 100 includes a frame 102 on which other elements of the machine 100 are mounted. The machine 100 includes a propulsion system 104, such as a track chain assembly, as shown. Alternatively, the machine 100 may have any other suitable type of propulsion system 104, such as wheels and tires. The machine 100 further includes an engine 106, such as an internal combustion engine powered by hydrocarbon fuels. Alternatively, the machine 100 may be an electrically powered machine. The machine 100 includes an exhaust system 108 and/or one or more work systems 110 that may be movable by one or more hydraulic systems 112. The machine 100 may also include a transmission system (not shown) that mechanically couples the engine 106 to the propulsion system 104. According to examples of the disclosure, any component of the machine 100, including any variety of components of the propulsion system 104, the engine 106, the exhaust system 108, the work systems 110, the hydraulic systems 112, the transmission, etc., may be formed by the mechanisms disclosed herein. Additionally, any of the aforementioned components of the machine 100 may have the structure and the resultant material properties as disclosed herein, when formed by the mechanisms disclosed herein.
The machine 100 may further include a mount 114 that may be attached to the hydraulic system 112 to hold a hydraulic hammer tool 116, which may also be referred to as a hydraulic breaker tool. The hydraulic hammer tool 116 may be used to break material that needs to be removed, such as in a construction setting. Thus, the hydraulic hammer tool 116 may be used to break rocks, concrete, asphalt, boulders, walls, glass, ceramics, or the like. The hydraulic hammer tool 116 may be used to break materials in applications where it may be unsafe and/or impractical to use other mechanisms (e.g., explosives) for demolition and/or breaking. In other cases, the hydraulic hammer tool 116 may be used in other applications that rely on percussion hammering, such as pile driving. An operator (not shown) of the machine 100 may be able to use any variety of controls, such as a foot paddle, to control the hydraulic hammer tool 116.
The hydraulic hammer tool 116 may include a frame 118 within which a hammer 120 of the hydraulic hammer tool 116 is disposed. The hammer 120 may be aligned within a bushing 122 of a tubular shape and configured to hold and align the hammer 120 within the frame 118 of the hydraulic hammer tool 116. The hammer 120 may include a protruded region 124 that protrudes from the frame 118. In some cases, there may be a hammer head 126 at an end of the hammer 120. When in use, the hammer head 126 may make contact and provide percussive impact on the material that is to be broken by the hydraulic hammer tool 116. In some cases, the hydraulic hammer tool 116 may not have a hammer head 126 as depicted here. Instead, the end of the hammer 120 may be substantially the same or similar dimensions as the rest of the hammer 120. In other cases, the hammer head 126 may be a different shape than what is depicted in
The hydraulic hammer tool 116 may operate by modulating a pressurized fluid within the hydraulic hammer tool 116 to move the hammer 120 within the confines of the bushing 122. As a result, the proportion of the hammer 120 that is the protruded region 124, sticking out of the frame 118, varies when the hydraulic hammer tool 116 is in use. When the hammer 120 is fully extended and exerting force on the material to be broken, the protruded region 124 is maximum. Similarly, when the hammer 120 is fully retracted and may be pulling away from the material to be broken, the protruded region 124 is minimum. It is this cyclic movement (e.g., up and down) that provides the percussive force to break the objects that are to be broken during use of the hydraulic hammer tool 116.
As the hammer 120 cycles up and down during use of the hydraulic hammer tool 116, the hammer 120 may have a variety of forces imparted thereon, including lateral forces that may arise from impact with the material that is to be broken. Therefore, the bushing 122 provides a guide for holding the hammer 120 in alignment when in use. The bushing 122 has a tubular shape and the hammer 120 has a cylindrical shape and is configured to fit through the bushing 122. As the hammer 120 moves axially, or up and down along its length during use, lateral forces, such as in a radial and/or lateral direction may be imparted to the hammer 120. The bushing 122 contacts the outer surface of the hammer 120 and, therefore, provides counter forces to the lateral forces that are imparted to the hammer 120 during use of the hydraulic hammer tool 116.
Since the bushing 122 is in contact with the hammer 120 and often has relatively significant forces imparted along its inner surface by the hammer 120, the bushing 122 may be subject to various failures. In general, the movement of the hammer 120 may wear out the inner surface of the bushing 122 that is in contact with the outer surface of the hammer 120. In more extreme cases, the bushing 122 may experience galling defects due to the reciprocating movement of the hammer 120 while in contact with the bushing 122.
The bushing 122, due to the conditions under which it operates, may wear out on a regular basis. Therefore, the bushing 122 may be replaced on a regular basis and/or on a maintenance schedule, as it wears out during the use of the hydraulic hammer tool 116. For example, the bushing 122 may be designed to operate until a particular level of wear is experienced on its inner diameter, such as about 1 millimeter (mm) to about 5 mm radially on the inner diameter. Although the bushing 122, in some cases, may be a consumable part, regular maintenance and replacement of the bushing 122 results in downtime at a construction or mining site, as well as a cost (e.g., parts cost, labor cost, opportunity cost of downtime, etc.). Therefore, it is desirable to minimize the frequency of downtime resulting from replacement of the bushing 122 in the hydraulic hammer tool 116.
The bushing 122 may be more wear resistant and last longer between replacement if the portions (e.g., the inner diameter region) of the bushing 122 that are in contact with the hammer 120 are hard. However, hardening the entirety of the bushing 122 may result in reduced toughness of the bushing 122 and further may result in additional forces (e.g., repeated percussive forces) being imparted to the frame 118, which may degrade the frame 118 and/or other components of the hydraulic hammer tool 116. The disclosure herein provides a bushing 122 that is relatively wear resistant while maintaining a relatively high level of toughness.
The bushings 122, as disclosed herein, may have a hardness of greater than approximately 60 Rockwell Hardness Scale C (HRC) in regions proximal to its inner surface and may have a bulk hardness of about 35 HRC to about 45 HRC. This allows for a relatively hard, wear resistant region of the bushing 122 that contacts the outer portion of the hammer 120 and a relatively softer region the bushing 122 that is in contact with the frame 118 of the hydraulic hammer tool 116. It should be understood that the aforementioned hardness values are example values and that the disclosure herein contemplates other values outside of the ranges indicated.
Although a particular size and type of hydraulic hammer tool 116 is depicted herein, it should be understood that this disclosure applies to any suitable hydraulic hammer tool 116 of any suitable size. For example, the bushing 122 and the methods of making the bushing 122 apply to smaller hydraulic hammer tools 116, such as human-held jackhammer tools, as well as larger hydraulic hammer tools 116 that may be used for pile driving large rods. It should also be understood that the bushing and/or the methods of making the same may be applied to other components of the machine 100. For example, the hydraulic system 112 may include cylinders that may be fabricated as described herein. As another example, bushings in the propulsion system 104 may also be fabricated according to the disclosure herein.
According to examples, a region proximal to the inner surface 302 may have a hardness of greater than approximately 60 HRC and may have a hardness in the range of about 35 HRC to about 45 HRC in the bulk region 304 and the outer surface 300. In some cases, the inner surface 302 may have a hardness of about 63 HRC or greater. In yet other cases, the inner surface may have a hardness of about 66 HRC or greater. In some cases, the bulk region 304 and/or the outer surface 300 may have a hardness in the range of about 37 HRC to about 43 HRC. In yet other cases, the bulk region 304 and/or the outer surface 300 may have a hardness in the range of about 39 HRC to about 41 HRC.
The bushing 122 may be constructed of medium to high carbon steel. For example, the carbon content of the steel may be in the range of about 0.58% by weight to about 1.1% by weight. According to examples of the disclosure, the bushing 122 may be rough formed, such as by one or more machining processes, and then hardened by heating and quenching. This hardening process may form a bushing 122 that is hard throughout. Next, the bushing 122 may be tempered to form a stable softened bushing 122. After softening the bushing 122, an induction heating process may be performed in the inner surface 302 of the bushing. The induction heating process may heat a relatively small depth from the inner surface 302 of the bushing to temperatures that harden the steel. After induction heating, the bushing 122 may be quenched, such as by forced air quenching, to harden a region proximal to the inner surface 302 of the bushing 122, while the rest of the bushing 122 remains relatively soft. The depth of the hardening may about 2 mm to about 5 mm. Thus, the bushing 122 has a hardness profile such that the region proximal to the inner surface 302 is relatively hard and the rest of the bushing 122 is relatively soft. Additionally, the relatively hard portion of the bushing 122 and the rest of the bushing 122 have substantially the same carbon concentrations. In some examples, the hard portion of the bushing 122 proximal to the inner surface 302 may be under compressive stress, while the rest of the bushing 122 may be under tensile stress.
In some examples, the bushing 122 may have an inner diameter in a range of about 50 mm to about 200 mm. In some examples, the inner diameter of the bushing 122 may be in a range of about 100 mm to about 180 mm. The value of the inner diameter of the bushing 122 may depend in part on the size of the hydraulic hammer tool 116. For example, a large hydraulic hammer tool 116 mounted on an excavator may have a bushing 122 with an inner diameter in a range of about 125 mm to about 200 mm, while a bushing 122 for a smaller hydraulic hammer tool 116 mounted on a skid steer may have an inner diameter in a range of about 50 mm to about 125 mm. The wall thickness of the bushing 122 may be in the range of about 10 mm to about 50 mm. In some cases, the bushing 122 may have a wall thickness in the range of about 20 mm to about 35 mm. The bushing 122 may have an outer diameter in the range of about 70 mm to about 300 mm. The bushing 122 may have a length in a range of about 100 mm to about 300 mm. Although specific dimensional ranges are discussed herein, it should be understood that the disclosure herein applies to dimensional ranges outside of those discussed.
At block 502, the component may be formed from steel. The forming of the component may include rough forming the component, such as the bushing 122. Rough forming, as used herein, refers to forming the shape of a component, prior to subsequent thermal treatments, such as strengthening via thermal processing, such as annealing, quenching, etc. or tempering. The bushing 122 may be formed from medium-carbon and/or high-carbon steel. Any variety of suitable alloy steel, spring steel, bearing steel, medium carbon steel, and/or high carbon steel may be used to rough form the bushing 122. For example, American Iron and Steel and Institute (AISI) 5160 steel may be used to rough form the bushing 122. As another example, AISI 52100 steel may be used to rough form the bushing 122.
A rough formed component, such as the bushing 122, may be formed from medium carbon (C) steel and/or high carbon steel, with C content in the range of about 0.58% to about 1.1% by weight. The steel used to rough form the component may be any suitable crystal structure, such as ferrite, pearlite, cementite, bainite, spheroidal carbide, martensite, austenite, and/or the like. The steel may include a variety of other impurities and/or additives therein. For example, components of the machine 100 may be formed from steel that may further include other elements therein, such as manganese (Mn), phosphorus (P), sulfur (S), silicon (Si), chromium, (Cr), boron (B), cobalt (Co), molybdenum (Mo), nickel (Ni), titanium (Ti), tungsten (W), niobium (Nb), vanadium (V), combinations thereof, or the like. It should also be noted that in some examples, the composition of the steel may be relatively uniform throughout.
In some examples, the steel used to rough form the components, such as bushing 122, may include C in the range of about 0.56% to about 0.64% by weight, Mn in the range of about 0.7% to about 1% by weight, Si in the range of about 0% to about 0.3% by weight, P in the range of about 0% to about 0.05% by weight, S in the range of about 0% to about 0.05% by weight, and Cr in the range of about 0.65% to about 0.95% by weight. In other examples, the steel used to rough form the components, as discussed herein, may include C in the range of about 0.9% to about 1.1% by weight, Mn in the range of about 0.25% to about 0.7% by weight, Si in the range of about 0.1% to about 0.4% by weight, P in the range of about 0% to about 0.04% by weight, S in the range of about 0% to about 0.03% by weight, Ni in the range of about 0% to about 0.3% by weight, Cr in the range of about 1% to about 1.7% by weight, and Mo in the range of about 0% to about 0.15% by weight. It should be understood that the disclosure herein contemplates using steel with compositions outside of the aforementioned ranges.
The concentrations of additives and/or impurities in the steel, as discussed herein, may allow for the formation of the structures, as discussed in conjunction with
The initial medium or high carbon steel may be relatively soft and ductile, allowing for relatively easy rough formation of the component, such as the bushing 122. For example, the steel may have an initial hardness in the range of about 33 HRC to about 50 HRC. The component, during rough formation, may be any suitable crystal structure, such as ferrite, pearlite, bainite, cementite, spheroidal carbide, martensite, and/or austenite. In some cases, if the starting steel is not sufficiently soft, then a tempering process may be performed. In examples, the tempering process may be conducted at an under the carbon-steel eutectic temperature for a multi-hour anneal prior to forming the rough component. For example, the steel may be held at a range between about 300° C. to about 600° C. for about 30 minutes to about 5 hours to temper the steel prior to rough forming the component. The temperature and/or time ranges here, and throughout the disclosure, are examples, and temperatures and time periods shorter or longer may be used in accordance with examples of the disclosure.
The component, such as the bushing 122, may be formed by any suitable mechanism such as any suitable hot formation mechanism and/or machining technique. In some cases, the bushing may be rough formed by starting with bar stock steel, such as cylindrical bar stock steel and machining the bar stock steel. In these cases, the starting bar stock steel may be of a cylindrical shape, or any other suitable shape. The bar stock steel may be of any suitable type and/or composition. As discussed herein, in some cases, the bar stock steel may be AISI 5160, AISI 52100, or the like. The bar stock steel may be bored out and then milled on a lathe to form the bushing 122. Other types of machining, such as shaping, turning, milling, drilling, grinding, chiseling, lathing, and/or combinations thereof may also be performed on the bored out and milled steel to rough form bushing 122.
In some other cases, the bushing 122 may be rough formed by any variety of hot processes. For example, any type of casting, rolling, hot rolling, cold rolling, extrusion, combinations thereof, or the like may be used to form the rough component. Additionally or alternatively, the rough component may be formed by any variety of subsequent machining techniques suitable for forming the component, such as any type of shaping, turning, milling, drilling, grinding, chiseling, lathing, and/or other machining techniques.
At block 504, the component may be hardened. In some examples, this hardening process may include heating the component to a relatively high temperature and then quenching the component. The component, such as the bushing 122, may be heated to a range of about 760° C. to about 1100° C. In some cases, the bushing 122 may be heated to a range of about 800° C. to about 1000° C. In yet other cases, the bushing may be heated to a range of about 850° C. to about 950° C. The component may be held at temperature for about 30 minutes to about 3 hours. In some cases, the heating process may be a batch process, where more than one component of the machine 100 may be heated simultaneously. In some cases, the induction heating may be performed in a reducing and/or non-oxidizing ambient, such as in a nitrogen containing environment, a forming gas environment, an ammonia environment, an argon environment, combinations thereof, or the like.
After the heating process, the component, such as bushing 122, may be quenched. In some cases, the quenching may be performed as an oil quench. In other cases, other quenching mechanisms may be used, such as water quench, polymer quench, air quench, etc. In some examples, the component may be cooled at a rate of approximately between about 2° C./s (or 120° C./min) and about 6° C./s (or 360° C./min). After the quench, the rough component may have a substantially martensitic crystal structure. The rough component, after the quench may have a hardness greater than 60 HRC throughout the component. In some cases, the component may have a hardness greater than 63 HRC throughout, after the quench. In yet other cases, the component may have a hardness greater than 66 HRC throughout, after the quench. Because the component is substantially uniformly hard throughout, further processing may be performed to soften the bulk hardness of the component by way of the following processes of method 500.
At block 506, the component may be tempered. The tempering process may be conducted in a furnace with a non-oxidizing and/or reducing ambient (e.g., nitrogen ambient, argon ambient, etc.). In some cases, the tempering process may be performed in the same type of furnace that was used for hardening the component at block 504. In other cases, a different type of furnace may be used for tempering the component than the furnace used for hardening the component at block 504. In examples of the disclosure, the tempering process may be conducted at a particular temperature, such as within a range of about 400° C. to about 600° C., for a multi-hour anneal. In some cases, the steel may be held at a temperature range between about 450° C. and about 570° C. for about 1 to about 3 hours to temper the steel component, such as the bushing 122.
In some examples, the tempering conditions may be based at least in part on the composition of the steel. For example, if the rough component is formed with AISI 5160 steel, the component may be tempered at a temperature range between about 450° C. and about 550° C. for about 1 to 3 hours. As another example, if the rough component is formed with AISI 52100 steel, the component may be tempered at a temperature range between about 450° C. and about 570° C. for about 1 to 3 hours to temper the steel component.
The tempering process may lead to the component having a substantially tempered martensitic and/or spheroidal carbide crystal structure throughout. At this point the tempered component may have a hardness in the range of about 35 HRC to about 45 HRC throughout the component. Thus, at this point, the component, such as bushing 122, may have a stable and uniform structure throughout that will be maintained though the remaining processes of method 500 to maintain the relatively softer profile of the component proximal to its outer surface 300. However, method 500 includes further processing to harden the region proximal to the inner surface 302.
At block 508, the inner surface of the component may be induction heated. This heating may be performed in an induction furnace, where induction coils are used to heat a particular depth into the bushing 122 at the inner surface 302. In examples, the inner surface may be heated to a hardening temperature at a particular depth from the inner surface 302, such as a depth of about 1 mm to about 7 mm. In some cases, the hardening depth may be approximately in the range of about 2 mm to about 6 mm. In other cases, the hardening depth may be in the range of about 3 mm to about 5 mm. The induction heated temperature in the hardening depth may be about 760° C. or more. In some cases, the induction heated temperature in the hardening depth may be about 800° C. or more. In other cases, the induction heated temperature in the hardening depth may be about 850° C. or more.
The induction heating may be performed for any suitable length of time and at any suitable power and frequency of operation to provide the desired thickness of the hardened inner region proximal to the inner surface 302. For example, the induction heating may be performed for a time of about 5 seconds to about 10 minutes. The induction heating may be performed at any suitable frequency to achieve the desired depth of hardness of the inner region proximal to the inner surface 302, such as about 3 kilohertz (kHz) to about 10 kHz.
At block 510, the component may be quenched. In some cases, the component may be quenched at the inner surface 302 directly from the induction heating temperature. The quench may be performed in any suitable ambient condition and/or using any suitable quench mechanism. For example, the bushing 122 may be quenched using a forced air quench. In other examples, the bushing may be quenched using a polymer quench. Alternatively, the quenching process may be in any suitable medium, such as a salt bath, water, air, and/or oil. In some examples, the component may be cooled at a rate of approximately between about 1° C./second (° C./s) (or 60° C./minute (° C./min)) and about 6° C./s (or 360° C./min). In other examples, the component may be cooled at a rate of approximately between about 2° C./s (or 120° C./min) and about 4° C./s (or 240° C./min). During the quenching process, the component may be cooled from the induction heating temperature to less than 200° C. In other cases, during the quenching process, the component may be cooled from the induction heating temperature to near room temperature.
At block 512, the component may be tempered. This tempering process may be conducted as a furnace tempering process and/or an induction tempering process at a temperature in the range of about 100° C. to about 400° C. This tempering process may reduce the possibility of cracking, such as delayed cracking, in the hardened inner region of bushing 122 proximal to the inner surface 302.
It should be appreciated that after performing method 500, the inner region of the bushing 122, proximal to the inner surface 302, may be substantially martensitic and/or spheroidal carbide in crystal structure. In other words, the quenching process may result in a relatively high level of martensite crystal structure in the hardened region near the inner surface 302 of the bushing 122. This martensitic texture, combined with the relatively high carbon content of the steel results in a hardening of the region near the inner surface 302, while the remainder of the bushing 122 remains relatively soft. The bulk region 304 and the outer surface 300, on the other hand, may remain substantially tempered martensitic in crystal structure. Thus, the inner surface 320, as disclosed herein, may be harder than the bulk region 304 of the component. Additionally, the inner region proximal to the inner surface 302 may be in compressive stress, while the bulk region 304 may be in tensile stress. Thus, method 500, individually or in combination with the metallurgical compositions described herein, allows for the formation of the advantageous structure of the bushing 122, thereby enhancing the durability and lifetime of the bushing 122.
It should be noted that some of the operations of method 500 may be performed out of the order presented, with additional elements, and/or without some elements. Some of the operations of method 500 may further take place substantially concurrently and, therefore, may conclude in an order different from the order of operations shown above. Although certain processes are discussed with respect to method 500, it should be understood that there may be other processes implemented in addition to the processes listed here. In these cases, other processes, such as hard-facing, may be used to thicken inner region. Indeed, any suitable processes may be performed prior to or after the processes of method 500.
As discussed herein, the inner region 602 may also be referred to as a hard inner layer. Similarly, the bulk region 304 may also be referred to as a core region, core layer, and/or outer region. Although the inner region 602 and the bulk region 304 are depicted as having a sharp transition, it should be understood that in some cases the transition from the inner region 602 to the bulk region 304 may be graded and/or gradual. In other words, there may be a spatial transition region that embodies material properties intermediate between the inner region 602 and the bulk region 304. In some cases, the transition thickness between the inner region 602 and the bulk region 304 may range from about 200 micrometers (μm) to about 2 mm. In other cases, the transition thickness between the inner region 602 and the bulk region 304 may range from about 500 μm to about 1.5 mm.
According to examples of the disclosure, the inner region 602 may be substantially martensitic in crystal structure, while the bulk region 304 may also be martensitic in crystal structure. However, the bulk region 304 may be a tempered martensite crystal structure. Thus, the inner region 602 may be harder than the bulk region 304 of the bushing 122. The metallurgical concentrations, including carbon, may be substantially uniform throughout the bushing 122. In other words, the carbon content in the inner region 602 may be substantially the same as the carbon concentration in the bulk region 304.
As discussed herein, the inner region 602 may have a hardness of greater than approximately 60 HRC and the bulk region 304 and the outer surface 300 may have a hardness in the range of about 35 HRC to about 45 HRC. In some cases, the inner region 602 may have a hardness of about 63 HRC or greater. In yet other cases, the inner region 602 may have a hardness of about 66 HRC or greater. In some cases, the bulk region 304 and/or the outer surface 300 may have a hardness in the range of about 37 HRC to about 43 HRC. In yet other cases, the bulk region 304 and/or the outer surface 300 may have a hardness in the range of about 39 HRC to about 41 HRC.
It should also be understood that the properties of the inner region 602 may not be uniform throughout the thickness of the inner region 602. In some cases, the presence of the inner region 602 may be detected by measuring the hardness at a threshold depth into the inner region 602. For example, the hardness at a depth of approximately 500 μm into the inner region 602 may be in the range of approximately 60 HRC to about 65 HRC. In some cases, the hardness at a depth of approximately 500 μm into the inner region 602 may be in the range of approximately 62 HRC to about 66 HRC. For example, in some cases, the hardness at a depth of 500 μm into the inner region 602 may be approximately a minimum of 60 HRC.
The inner region 602 may be of any suitable thickness. For example, the inner region 602 may be a thickness in the range of about 1 mm to about 7 mm. In some other cases, the thickness of the inner region 602 may be in the range of approximately 3 mm to about 5 mm. Although the disclosure discusses certain thicknesses of the inner region 602 herein, it should be understood that the disclosure contemplates thicknesses outside of the ranges discussed herein. It should also be understood that the thickness of the inner region 602 may vary based at least in part on the component and/or the application of the component. For example, for a larger bushing 122, a thicker inner region 602 may be desired compared to that for a smaller bushing 122. The bulk region 304 may have a thickness in the range of about 10 mm to about 30 mm.
The inner region 602 is not just harder, but in some cases, the inner region 602 is also in compressive stress, while the bulk region 304 is in tensile stress. Thus, by engineering this component such that the maximum forces are imparted to a compressively stressed region, such as the inner region 602, a lower possibility of cracking can be achieved, leading to greater durability of the bushing 122. In addition to the advantageous stress profile described herein, the enhanced hardness of the inner region 602 improves its durability to impacts, such as impacts at elevated operating temperatures.
It should be understood that the structure of the bushing 122, as depicted in
The present disclosure describes systems, structures, and methods to increase wear tolerance, reduce crack initiation and/or crack propagation, and/or increase the toughness of components for machines 100 and/or any variety of hydraulic hammer tools 116, such as bushing 122. The bushing 122, as disclosed herein, may have a hard, wear-resistant inner region 602, as well as a soft bulk region 304. The soft bulk region 304 provides for a high level of toughness of the bushing 122, while the hard inner region 602 provides for a high level of wear resistance during operation of the hydraulic hammer tool 116. Additionally, the inner region 602 may be under compressive stress, thereby inhibiting crack formation and/or crack propagation, while the bulk region 304 may be under tensile stress.
As a result of the systems, apparatus, and methods described herein, parts of machines 100, such as bushing 122, may have a greater lifetime. For example, the bushing 122 described herein may have greater service lifetime than traditional bushings that are not formed by the mechanisms described herein. In some cases, components, such as the bushing 122, may allow for a significant improvement in the wear lifetime of parts of the machines 100. This reduces field downtime, reduces the frequency of servicing and maintenance, and overall reduces the cost of heavy equipment, such as machines 100. The improved reliability and reduced field-level downtime also improves the user experience such that the machine 100 can be devoted to its intended purpose (e.g., construction, mining, etc.) for longer times and for an overall greater percentage of its lifetime. Improved machine 100 uptime and reduced scheduled maintenance may allow for more efficient deployment of resources (e.g., fewer, but more reliable machines 100 at a construction site). Thus, the technologies disclosed herein improve the efficiency of project resources (e.g., construction resources, mining resources, etc.), provide greater uptime of project resources, and improves the financial performance of project resources.
While aspects of the present disclosure have been particularly shown and described with reference to the embodiments above, it will be understood by those skilled in the art that various additional embodiments may be contemplated by the modification of the disclosed machines, systems and methods without departing from the spirit and scope of what is disclosed. Such embodiments should be understood to fall within the scope of the present disclosure as determined based upon the claims and any equivalents thereof.
Recitation of ranges of values herein are merely intended to serve as a shorthand method of referring individually to each separate value falling within the range, unless otherwise indicated herein, and each separate value is incorporated into the specification as if it were individually recited herein. All methods described herein can be performed in any suitable order unless otherwise indicated herein.
The drawings are illustrative only and non-limiting. Items depicted therein are not necessarily to drawn to scale and the relative proportions of various components may not be uniform. The drawings may not reflect certain dimensions recited in this specification.
