Patent Application
20160265535
The present invention relates to a rotor (also called an impeller) for pumping molten metal, the rotor having hardened blade tips. The purpose of the hardened blade tips is to decrease wear, and help prevent breakage, on portions of the rotor that are struck by dross or other hard objects found in molten metal.
As used herein, the term “molten metal” means any metal or combination of metals in liquid form, such as aluminum, copper, iron, zinc and alloys thereof, in which devices according to the invention can function. The term “gas” means any gas or combination of gases, including argon, nitrogen, chlorine, fluorine, freon, and helium, that are released into molten metal.
Known molten-metal pumps include a pump base (also called a housing or casing), one or more inlets (an inlet being an opening in the housing to allow molten metal to enter a pump chamber), a pump chamber, which is an open area formed within the housing, and a discharge, which is a channel or conduit of any structure or type communicating with the pump chamber (in an axial pump the chamber and discharge may be the same structure or different areas of the same structure) leading from the pump chamber to an outlet, which is an opening formed in the exterior of the housing through which molten metal exits the casing. An impeller, also called a rotor, is mounted in the pump chamber and is connected to a drive system. The drive system is typically an impeller shaft connected to one end of a drive shaft, the other end of the drive shaft being connected to a motor. Often, the impeller shaft is comprised of graphite, the motor shaft is comprised of steel, and the two are connected by a coupling. As the motor turns the drive shaft, the drive shaft turns the impeller and the impeller pushes molten metal out of the pump chamber, through the discharge, out of the outlet and into the molten metal bath. Most molten metal pumps are gravity fed, wherein gravity forces molten metal through the inlet and into the pump chamber as the impeller pushes molten metal out of the pump chamber.
A number of submersible pumps used to pump molten metal (referred to herein as molten metal pumps) are known in the art. For example, U.S. Pat. No. 2,948,524 to Sweeney et al., U.S. Pat. No. 4,169,584 to Mangalick, U.S. Pat. No. 5,203,681 to Cooper, U.S. Pat. No. 6,093,000 to Cooper and U.S. Pat. No. 6,123,523 to Cooper, and U.S. Pat. No. 6,303,074 to Cooper, all disclose molten metal pumps. The disclosures of the patents to Cooper noted above are incorporated herein by reference, as are U.S. Pat. Nos. 7,402,276 and 7,507,367. The term submersible means that when the pump is in use, its base and rotor are at least partially submerged in a bath of molten metal, and preferably fully submerged.
Three basic types of pumps for pumping molten metal, such as molten aluminum, are utilized: circulation pumps, transfer pumps and gas-release pumps. Circulation pumps are used to circulate the molten metal within a bath, thereby generally equalizing the temperature of the molten metal. Circulation pumps may be used in a reverberatory furnace having an external well, or in any other suitable vessel that retains molten metal. The well is usually an extension of the charging well where scrap metal is charged (i.e., added).
Transfer pumps are generally used to transfer molten metal from the external well of a reverberatory furnace to a different location such as a ladle or another furnace.
Gas-release pumps, such as gas-injection pumps, circulate molten metal while releasing a gas into the molten metal. In the purification of molten metals, particularly aluminum, it is frequently desired to remove dissolved gases such as hydrogen, or dissolved metals, such as magnesium, from the molten metal. As is known by those skilled in the art, the removing of dissolved gas is known as “degassing” while the removal of magnesium is known as “demagging.” Gas-release pumps may be used for either of these purposes or for any other application for which it is desirable to introduce gas into molten metal. Gas-release pumps generally include a gas-transfer conduit having a first end that is connected to a gas source and a second submerged in the molten metal bath. Gas is introduced into the first end and is released from the second end into the molten metal. The gas may be released downstream of the pump chamber into either the pump discharge or a metal-transfer conduit extending from the discharge, or into a stream of molten metal exiting either the discharge or the metal-transfer conduit. Alternatively, gas may be released into the pump chamber or upstream of the pump chamber at a position where it enters the pump chamber. A system for releasing gas into a pump chamber is disclosed in U.S. Pat. No. 6,123,523 to Cooper. Furthermore, gas may be released into a stream of molten metal passing through a discharge or metal-transfer conduit wherein the position of a gas-release opening in the metal-transfer conduit enables pressure from the molten metal stream to assist in drawing gas into the molten metal stream. Such a structure and method is disclosed in a copending application entitled “System for Releasing Gas Into Molten Metal,” invented by Paul V. Cooper, and filed on Feb. 4, 2004, the disclosure of which is incorporated herein by reference.
There are also pumping systems that include a rotor inside of an essentially vertical conduit to drive molten metal upward into the conduit and out of an outlet in communication with the conduit. No pump base is used with such a system.
The materials forming the components that contact the molten metal bath should remain relatively stable in the bath. Structural refractory materials, such as graphite or ceramics, that are resistant to disintegration by corrosive attack from the molten metal may be used. As used herein “ceramics” or “ceramic” refers to any oxidized metal (including silicon) or carbon-based material, excluding graphite, capable of being used in the environment of a molten metal bath. A ceramic is harder and more durable to impact with a hard substance than graphite. “Graphite” means any type of graphite, whether or not chemically treated. Graphite is particularly suitable for being formed into pump components because it is (a) soft and relatively easy to machine, and (b) less expensive than ceramics.
When a molten metal pump, or pumping system, is operated, the rotor rotates, and the molten metal in which the rotor operates includes solid particles, such as dross and brick. As the rotor rotates the solid particles strike the moving rotor, potentially jamming or damaging the rotor and one or more of the other pump components, such as the rotor shaft.
Many attempts have been made to solve this problem, including the use of filters or disks to prevent solid particles from entering the inlet and the use of a non-volute pump chamber to increase the space between the inlet and rotor to allow solid pieces to pass into the pump chamber without jamming, where they can be pushed through the discharge by the action of the rotor.
The present invention relates to rotors used for pumping molten metal wherein the rotors have blades with hardened tips to alleviate damage to the rotor caused by dross or other hard particles striking the rotor as molten metal is pumped. The tips are at least twice as hard as the body portion of the rotor.
In one embodiment, the hardened tips are comprised of silicon carbide and the body portion is comprised of graphite. Aspects of the invention can be utilized on any molten metal rotor, whether used in a molten metal pump, a molten metal pumping system, a scrap melter, a degasser, or other device.
As used herein the relative hardness of materials is determined by the MOHS hardness scale. On the MOHS hardness scale, treated graphite (also referred to herein simply as graphite) is preferably used to form a rotor body according to the invention) generally has a hardness between 1.5 and 2.5 on the MOHS scale, whereas silicon carbide (preferably used to form a hardened tip according to the invention) generally has a hardness of 9-10 on the MOHS scale. By way of example, if a first material has a MOHS scale hardness of 1.0 and a second material has a MOHS scale hardness of 2.0, the second material is considered to be twice as hard as the first material for the purpose of this disclosure. Similarly, as an example, a third material with a MOHS scale hardness of 3.0 would be three times as hard as the first material and 50% harder than the second material for the purpose of this disclosure.
Turning now to the drawings, where the purpose is to describe preferred embodiments of the invention and not to limit same, systems and devices according to the invention will be described.
Rotor 10 may have a flow blocking and bearing plate 13. As shown, flow blocking and bearing plate 13 is cemented or otherwise attached to the bottom 14 of rotor 10. If rotor 10 is used on a bottom feed pump, the flow blocking and bearing plate 13 may be at the top of the rotor (in essence, the rotor would be turned upside down, with the blades 12 at the bottom, but the rotor shaft connective portion 18 would still be at the top of the rotor and formed through the flow blocking and bearing plate). The flow blocking and bearing plate 13 is preferably comprised of a hard, wear-resistant material, such as silicon carbide. Alternatively, a rotor according to the invention may not be attached to a flow blocking and bearing plate and any not have a bottom 14. For example, the rotor may be used in a system for moving molten metal upward into a conduit, or with scarp melter, or with a rotary degasser.
Rotor 10 further includes a connective portion 18, which is preferably a threaded bore, but can be any structure capable of drivingly engaging a rotor shaft (not shown) in order to rotate the rotor. It is most preferred that the outer surface of the end of a rotor shaft that is received in connective portion 18 has tapered threads and connective portion 18 be threaded to receive the tapered threads.
The preferred dimensions of rotor 10 will depend upon the size of the pump chamber or other structure in which the rotor is received and/or used. If rotor 10 is positioned in a pump chamber, top surface 16 is preferably flush with the pump chamber inlet.
Hardened tips 200 are preferably at least: twice as hard as the body portion 100, or 2-3 times harder than the body portion 100, or 2-4 times harder than the body portion 100, or 2-5 times harder than the body portion 100, or 2-6 times harder, 2-7 times harder, 2-8 times harder, 2-9 times harder, 2-10 times harder than the body portion 100. In one preferred embodiment, the body portion 100 is graphite and the tips 200 are silicon carbide.
Each hardened tip 200 preferably extends along at least part of top surface 16, and as shown each hardened tip extends along part of the leading surface 12A of each rotor blade 12. Preferably, each hardened tip 200 forms at least: 15%, or at least 20%, or at least 25%, or at least 30%, or at least 35%, or at least 40%, or at least 50%, or at least 75%, or at least 90%, or 100%, or 30%-100%, of the leading edge 17 of rotor 10.
The height of surface 12A is measured from edge 17 to the upper surface of bottom 14. Each hardened tip 200 also preferably extends downward along leading surface 12A by at least: 10% of the height of surface 12A, or at least 15% of the height of surface 12A, or at least 20% of the height of surface 12A, or at least 25% of the height of surface 12A, or at least 30% of the height of surface 12A, or at least 40% of the height of surface 12A, or at least 50% of the height of surface 12A, or at least 75% of the height of surface 12A, or 30%-100% of the height of surface 12A.
Each hardened tip 200 also preferably extends downward along the outermost edge of each vane 12 by at least: 15% of the height of surface 12A, at least 20% of the height of surface 12A, at least 25% of the height of surface 12A, at least 30% of the height of surface 12A. Each tip 200 also preferably extends along top surface 16 between leading edge 17 and trailing edge 19, by at least: 10%, at least 20%, at least 30%, at least 40%, or at least 50%, or 30%-100% of the distance between leading edge 17 and trailing edge 19.
Additionally, as shown each cut-out 70 has a back channel 21 that mates with corresponding sections 220 on each tip 200 to help secure tips 200 to rotor body 100. The tips are preferably cemented in place in cut-outs 70.
Surface 1012A is angled (as used herein the term angled refers to both a substantially planar surface, or a curved surface, or a multifaceted surface) such that, as rotor 1000 turns (as shown it turns in a clockwise direction) surface 1012A directs molten metal towards second portion 1012B. Any surface that functions to direct molten metal towards second portion 1012B can be used, but it is preferred that surface 1012A is substantially planar and formed at a 30°-60°, and most preferably, a 45° angle.
A recess or trailing surface 1012B as shown preferably extends from top surface 1016 to bottom 1014. Trailing surface 1012B is flat and preferably dimensioned relative the size of rotor blade 1012 to help reduce the area of top surface 1016 on the blade, thereby creating a larger opening for more molten metal to enter into the rotor 1000 thus enabling rotor 1000 to move more molten metal per rotor revolution.
Rotor 1000 may have a flow blocking and bearing plate 1013. As shown, flow blocking and bearing plate 1013 is cemented or otherwise attached to the bottom 1014 of rotor 1000. If rotor 1000 is used on a bottom feed pump, the flow blocking and bearing plate 1013 may be at the top of the rotor (in essence, the rotor would be turned upside down, with the blades 1012 at the bottom, but the rotor shaft connective portion 1018 would still be at the top of the rotor and be formed through the flow blocking and hearing plate). The flow blocking and bearing plate 1013 is preferably comprised of a hard, wear-resistant material, such as silicon carbide. Alternatively, a rotor according to the invention may not be attached to a flow blocking and bearing plate and may not have a bottom 1014. For example, the rotor may be used in a system for moving molten metal upward into a conduit, or with scarp melter, or with a rotary degasser.
Hardened tips 1200 are preferably at least: twice as hard as the body portion 1001, or 2-3 times harder than the body portion 1001, or 2-4 times harder than the body portion 1001, or 2-5 times harder, or 2-6 times harder, or 2-7 times harder, or 2-8 times harder, or 2-9 times harder, or 2-10 times harder, than the body portion 1001. In one preferred embodiment, the body portion 1001 is graphite and the tips 1200 are silicon carbide. As shown, each hardened tip 1200 extends along at least part of top surface 1016, along part of the leading surface 1012A of each rotor blade 1012, and along part of the trailing surface 1012B of each rotor blade 1012.
Each hardened tip 1200 extends along at least part of top surface 1016, and as shown each hardened tip extends along part of the leading surface 1012A of each rotor blade 1012. Preferably, each hardened tip 1200 forms at least: 15%, or at least 20%, or at least 25%, or at least 30%, or at least 35%, or at least 40%, or at least 50%, or at least 75%, or at least 90%, or 100%, or 30%-100%, of the leading edge 1017. Each hardened tip 1200 also preferably extends downward along leading surface 1012A by at least: 10% of the height of surface 1012A, at least 15% of the height of surface 1012A, at least 20% of the height of surface 12A, at least 25% of the height of surface 1012A, at least 30%, or at least 40% of the height of surface 1012A, or at least 50% of the height of surface 1012A, or at least 75% of the height of surface 1012A, or 30%-100% of the height of surface 1012A, or at least the entire height of surface 1012A. The height of surface 1012A is measured from surface 1016 on edge 1017 to the upper surface of bottom 1014.
Each hardened tip 1200 also extends downward along the outermost edge of each vane 1012 by at least: 15% of the height of surface 1012A, at least 20% of the height of surface 1012A, at least 25% of the height of surface 1012A, at least 30% of the height of surface 1012A, at least 40% of the height of surface 1012A, at least 50% of the height of surface, at least 75% of the height of surface 1012A, or 30%-100% of the height of surface 1012A. Each tip 1200 also preferably extends along top surface 1016 between leading edge 1017 and trailing edge 1019, by at least 10%, at least 20%, at least 30%, at least 40%, at least 50%, at least 75%, or 30%-100%, of the distance between leading edge 1017 and trailing edge 19.
Each hardened tip also preferably forms part of and extends along at least 10% of the height of back surface 1012B (as measured from top surface 1016 to the top of bottom 1014), at least 20% of the height of back surface 1012B, at least 30% of the height of back surface 1012B, at least 40% of the height of back surface 1012B, or at least 50% of the height of back surface 1012B, at least 75% of the height of surface 1012B, or 30%-100% of the height of back surface 1012B.
Rotor 1000 further includes a connective portion 1018, which is preferably a threaded bore, but can be any structure capable of drivingly engaging a rotor shaft (not shown). It is most preferred that the outer surface of the end of a rotor shaft that is received in connective portion 1018 has tapered threads and connective portion 1018 be threaded to receive the tapered threads.
The preferred dimensions of rotor 1000 will depend upon the size of the pump chamber or other structure in which it is received and/or used. If rotor 1000 is positioned in a pump chamber, top surface 1016 is preferably flush with the pump chamber inlet.
Additionally, as shown each gap has a channel 1015 and a back channel 1021 that mate with corresponding sections on each tip 1200 to help secure tips 1200 to rotor body 1001. The tips are preferably cemented in place.
Hardened tips may be utilized in any suitable rotor, such as the rotors described in U.S. Pat. Nos. 7,402,276, 8,178,037, 8,110,141, 8,409,495, and 8,075,837.
Having thus described some embodiments of the invention, other variations and embodiments that do not depart from the spirit of the invention will become apparent to those skilled in the art. The scope of the present invention is thus not limited to any particular embodiment, but is instead set forth in the appended claims and the legal equivalents thereof. Unless expressly stated in the written description or claims, the steps of any method recited in the claims may be performed in any order capable of yielding the desired result.
This application is a non-provisional of and claims priority to U.S. Provisional Application Ser. No. 62/110,899 entitled “Molten Metal Rotor With Hardened Blade Tips,” filed on Feb. 2, 2015, the contents of which are incorporated herein in its entirety for all purposes.
| Number | Date | Country | |
|---|---|---|---|
| 62110899 | Feb 2015 | US |
