Molten metal rotor with hardened top
09903383 ยท 2018-02-27
Assignee
Inventors
Cpc classification
F27D27/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D7/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D7/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/242
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2300/226
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D3/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/2261
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D2003/0054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22B7/003
CHEMISTRY; METALLURGY
B22D17/30
PERFORMING OPERATIONS; TRANSPORTING
F04D29/2216
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22D39/00
PERFORMING OPERATIONS; TRANSPORTING
F04D29/2222
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02W30/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F05D2240/303
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D7/065
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/026
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10S266/901
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
C22B21/0092
CHEMISTRY; METALLURGY
International classification
F04D29/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D7/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22D17/30
PERFORMING OPERATIONS; TRANSPORTING
B22D39/00
PERFORMING OPERATIONS; TRANSPORTING
F04D29/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D3/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22B7/00
CHEMISTRY; METALLURGY
F04D29/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D27/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D7/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Embodiments of the invention are directed to a rotor for a molten metal pump and a molten metal pump including the rotor. The rotor has a main body and a top comprised of a material that is at least twice as hard as the main body. The top, among other things, may form a first portion of each rotor blade wherein the first portion directs molten metal into a pump chamber or other structure in which the rotor is mounted.
Claims
1. A rotor for use in a molten metal pump, the rotor comprising (a) a graphite body; (b) a plurality of blades, wherein each blade has a first portion and a second portion, wherein the first portion is above the second portion and is configured to push molten metal downwards towards the second portion, and the second portion is configured to push the molten metal outward; (c) a hardened top portion comprising material at least twice as hard as the graphite body; (d) wherein the hardened top portion forms at least part of the first portion and at least part of the second portion.
2. The rotor of claim 1 wherein the hardened top portion is comprised of material between 2-3 times as hard as the graphite body.
3. The rotor of claim 1 wherein the hardened top portion is comprised of material between 2-4 times as hard as the graphite body.
4. The rotor of claim 1 wherein the hardened top portion is comprised of material between 2-5 times as hard as the graphite body.
5. The rotor of claim 1 wherein the hardened top portion is cemented to the graphite body.
6. The rotor of claim 1 wherein the hardened top portion comprises silicon carbide.
7. The rotor of claim 1 wherein the at least part of the second portion formed by the hardened top portion is immediately beneath the first portion.
8. The rotor of claim 1 that includes a flow blocking and bearing plate having a circumference and each blade extends no more than 1 beyond the circumference.
9. The rotor of claim 1 that has a top surface having an area, and each rotor blade includes a recess on the side opposite the first portion, each recess for decreasing the area of the top surface so as to create a larger opening through which more molten metal can pass.
10. The rotor of claim 9 wherein the hardened top portion forms at least part of the recess.
11. The rotor of claim 10 wherein the recess extends from the top surface at a position forward of the trailing surface and terminates at the trailing surface.
12. The rotor of claim 1 that includes a body portion having gaps at the corner of each blade and the hardened top portion has sections that are received by and mate with the gaps.
13. The rotor of claim 12 wherein the gaps include openings that each receive a pin positioned in each respective section of the hardened top portion.
14. The rotor of claim 12 wherein the gap and the hardened top portion include mating openings wherein each two mating openings receive a dowel pin.
15. The rotor of claim 1 wherein the first portion has an angled bottom with an angle of between 30 and 60.
16. A molten metal pump including the rotor of claim 1.
17. The molten metal pump of claim 16 that includes a superstructure on which a motor is supported, a pump base including a pump chamber in which the rotor is received, and a plurality of support posts connecting the superstructure to the pump base.
18. The rotor of claim 1 that further includes a flow blocking and bearing plate having a circumference and the first portion of each blade extends past the circumference.
19. The rotor of claim 18, wherein the first portion of each blade has a leading edge, and each blade includes a recess and a connecting portion that connects the leading edge and the recess.
20. The rotor of claim 1, wherein the first portion includes a leading edge and the entire leading edge is part of the hardened top portion.
21. The rotor of claim 1, wherein each blade includes a recess and the entire recess is part of the hardened top portion.
22. The rotor of claim 1, wherein the entire first portion is part of the hardened top portion.
23. The rotor of claim 1, wherein part of the leading surface is part of the hardened top portion.
24. The rotor of claim 1, wherein part of the trailing surface is part of the hardened top portion.
25. A rotor that includes a top surface and a bottom; a plurality of imperforate rotor blades for displacing molten metal, wherein each of the plurality of rotor blades includes a horizontally-oriented first portion with a surface angled at 30 degrees to 60 degrees that is configured to push molten metal downward, and a second portion beneath the first portion that is configured to push molten metal outward, a trailing face, and a recess that reduces the area of the top surface to help permit molten metal to pass therethrough and into pump chamber; wherein the plurality of imperforate rotor blades are comprised of graphite; and the top surface is comprised of ceramic.
26. The rotor of claim 25 that further includes a flow blocking and bearing plate.
27. The rotor of claim 26 wherein the flow blocking and bearing plate is comprised of ceramic.
28. The rotor of claim 25 wherein there are three imperforate rotor blades.
29. The rotor of claim 25 that includes a body portion and the top surface is cemented to the body portion.
30. The rotor of claim 25 that further includes a threaded connective portion at the top for connecting to a rotor shaft.
31. The rotor of claim 25 wherein the first portion of each rotor blade has a horizontally-extending projection with a top surface and a bottom surface, wherein the bottom surface is angled to move molten metal downward.
32. The rotor of claim 31 wherein the second portion of each rotor blade is vertical.
33. The rotor of claim 31 wherein the bottom surface of each horizontally-extending projection is formed at a 10-60 downward angle relative a horizontal axis.
34. The rotor of claim 31 wherein the top surface of the first portion of each rotor blade is horizontal.
35. The rotor of claim 31 wherein the horizontally-extending projection has a leading edge that is at least thick.
36. The rotor of claim 25 wherein each recess extends at an angle from the top surface downward to the trailing surface.
37. A molten metal pump including the rotor of claim 25.
38. The pump of claim 37 that includes a superstructure on which a motor is supported, a pump base including a pump chamber in which the rotor is received, and a plurality of support posts connecting the superstructure to the pump base.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
(5) As used herein the relative hardness of materials is determined by the MOHS hardness scale. On the MOHS hardness scale, treated graphite may have a hardness between 1.5 and 2.5, whereas silicon carbide generally has a hardness of 9-10.
(6) Turning now to the drawings, where the purpose is to describe a preferred embodiment of the invention and not to limit same, systems and devices according to the invention will be described.
(7)
(8) A rotor according to aspects of the invention has a body (or body portion) 101 with a hardened top surface 106. Rotor 100 may have a flow blocking and bearing plate 110. As shown, flow blocking and bearing plate 110 is cemented to the bottom 120 of rotor 100. If rotor 100 is used on a bottom feed pump, the flow blocking and bearing plate 110 may be at the top of the rotor (in essence, the rotor would be turned upside down, with the blades at the bottom, but the rotor shaft attachment mechanism would still be at the top). The flow blocking and bearing plate 110 is preferably comprised of a hard, wear-resistant material, such as silicon carbide. Alternatively, a rotor according to the invention may not have a flow blocking and bearing plate.
(9) Rotor 100 further includes a connective portion 112, 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 the rotor shaft that is received in portion 112 has tapered threads and connective portion 112 be threaded to receive the tapered threads.
(10) The preferred dimensions of rotor 100 will depend upon the size of the pump chamber or other structure in which it is received.
(11) Preferably each vane 102 has the same configuration so only one vane 102 shall be described. Each vane 102 preferably includes a horizontally-oriented first portion 102A and a vertically-oriented second portion 102B. The respective vertical and horizontal orientation of the portions described herein is in reference to a rotor positioned in a standard pump having an input port in its top surface. The invention, however, covers any rotor for use in a molten-metal pumping application, whether the flow of molten metal is first contacting the rotor at the top or bottom or both. It will be therefore understood that the terms horizontal and vertical refer to the rotor as shown in the orientation in
(12) Top surface 106 is preferably flush with a pump chamber inlet, if used with a pump chamber.
(13) Section 102A preferably has a leading edge 116 and an angled surface (or first surface) 118. Surface 118 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 100 turns (as shown it turns in a clockwise direction) surface 118 directs molten metal towards second portion 102B. Any surface that functions to direct molten metal towards second portion 102B can be used, but it is preferred that surface 118 is substantially planar and formed at a 30-60, and most preferably, a 45 angle.
(14) Portion 102B, which is preferably vertical (but can be angled or curved), extends from the bottom of section 102A to the top of base (or bottom) 120. Portion 102B has a leading face (or second surface) 122. Leading face 122 is preferably planar and vertical, although it can be of any configuration that directs molten metal outward, such as towards the wall of a pump chamber or other structure in which the rotor 100 is housed.
(15) A recess 130 is formed in top portion 104 and preferably extends from top surface 106 to at least as far as the trailing face 132 of second portion 102B. As shown, recess 130 begins at a position on surface 106 slightly forward of face 132 and terminates at a position even with trailing face 132. The purpose of recess 130 is to reduce the area of top surface 106, thereby creating a larger opening for more molten metal to enter into the rotor 100 thus enabling rotor 100 to move more molten metal per rotor revolution.
(16) The hardened top 104 is shown in
(17)
(18) Additionally, gaps 150 may have openings 151 that mate with pins (not shown) in sections 152, or gaps 150 and sections 152 may have openings that receive dowel pins (not shown) to help secure top 104 to the body portion. The center opening 112 in the body portion may also include a locating ring 112A formed therein, which mates with an extending portion (not shown) in the top 104 to properly center the two.
(19) A similar hardened top may be utilized in a rotor device such as the one described in U.S. Pat. No. 7,402,276.
(20) The flow blocking and bearing plate 110 has a circumference and the first portion 102A of each blade 102 preferably extends beyond the circumference, as best seen in
(21) 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.