Rotary degassers and components therefor
10570745 ยท 2020-02-25
Assignee
Inventors
Cpc classification
F27D27/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27B3/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D3/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D5/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/108
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D2027/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04B17/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27B3/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F27D27/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C21C1/06
CHEMISTRY; METALLURGY
F27D3/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/108
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Disclosed are degassers, couplings, impeller shafts and impellers for use in molten metal. One such coupling transfers gas into an impeller shaft, the coupling having a smooth, tapered internal surface to align with a corresponding surface on the impeller shaft and help prevent gas leakage and to assist in preventing damage to the impeller shaft. Improved impellers for shearing and mixing gas are also disclosed, as is a degasser including one or more of these components.
Claims
1. A rotor shaft configured for use in a molten metal environment, the rotor shaft comprising one or more of graphite and ceramic, and the rotor shaft being configured so that it cannot be threadingly connected to a corresponding coupling, and is configured to be received and retained in the corresponding coupling, which has no internal threads, the rotor shaft comprising: (a) a first end that is tapered and not threaded; (b) a non-tapered center portion that that includes at least one helical groove that is not threads, and that is configured to receive an end of a retainer, wherein the non-tapered center portion has a first side connected to the first end, and a second side; (c) an outer surface connected to the second end side of the center portion, wherein the outer surface has no threads or grooves; and (d) a second end that is threaded and configured to connect to a rotor; wherein the first end of the shaft is configured to be received in the corresponding coupling so that the first end of the shaft mates with an inner tapered portion of the corresponding coupling, and one or more retainers are received in openings in the corresponding coupling such that each of the one or more retainers is positioned to be pressed against the at least one helical groove, in order to apply driving force from the corresponding coupling to the shaft.
2. The rotor shaft of claim 1, wherein the second end is connected to a rotor.
3. The rotor shaft of claim 1 wherein the taper is at an angle between 20 and 45.
4. The rotor shaft of claim 1 that has a single helical groove.
5. The rotor shaft of claim 2, wherein the taper is at an angle between 20 and 45.
6. The rotor shaft of claim 2 that has a single helical groove.
7. The rotor shaft of claim 1 that is a unitary structure.
8. The rotor shaft of claim 1 that further comprises an inner passage for transferring gas.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
(11) Reference will now be made in detail to the present exemplary embodiments of the invention, examples of which are illustrated in the accompanying drawings.
(12) The exemplary rotary degasser 10 includes an impeller shaft 100 (also shown are shafts 100 and 100), an impeller 200 and a coupling 20 for coupling the impeller shaft to the motor shaft of a drive source (not shown). Impeller shaft 100, impeller 200, and each of the impellers used in the practice of the invention, are preferably made of graphite impregnated with oxidation-resistant solution, although any material capable of being used in a molten metal bath, such as ceramic, or non-impregnated graphite could be used. Oxidation and erosion treatments for graphite parts are practiced commercially, and graphite so treated can be obtained from sources known to those skilled in the art.
(13) The drive source can be any structure, system, or device capable of rotating shaft 100 and impeller 200 and is preferably a pneumatic motor or electric motor, the respective structures of which are known to those skilled in the art. The drive source can be connected to impeller shaft 100 in any suitable manner, but is preferably indirectly connected by a motor shaft that is connected to one end of coupling 20, whereas the other end (or collar) of coupling 20 is connected to a first end 102 of the impeller shaft 100. The motor shaft is preferably comprised of steel, comprises an inner passage for the transfer of gas, and is preferably in communication with a rotary union, which releases gas from a gas source into the motor shaft, as is known by those skilled in the art. A typical rotary union is a rotary union of the type described in U.S. Pat. No. 6,123,523 to Cooper, filed Sep. 11, 1998, the disclosure of which from page 9, line 21 to page 10, line 23, and FIGS. 4 and 4D, are incorporated herein by reference.
(14) As is illustrated in
(15) A preferred embodiment of the shaft 100 at end 102 is shown in
(16) The tapered portion 102A of end 102 of the impeller shaft 100 aligns with an internal, tapered portion 422 of coupling 200, as seen in
(17) An embodiment of a coupling according to the present invention is shown in
(18) Second coupling member 404 (best seen in
(19) In one embodiment, referring now to
(20) When end 102 (as shown in
(21) Turning now to
(22) By operating impeller 200 at a lower speed less stress is transmitted to the moving components, which leads to longer component life, less maintenance and less downtime. Another advantage that may be realized by operating the impeller at slower speeds is the elimination of a vortex. Some known devices must be operated at high speeds to achieve a desired efficiency. This can create a vortex that draws air into the molten metal from the surface of bath B. The air can lead to metal ingots and finished parts that have air pockets, which is undesirable and/or to the formation of dross. As shown by the arrows in
(23) In one embodiment, impeller 200 comprises a top surface 202, sides 204, 206, 208 (not shown) and 210 (not shown) corners 212, 214, 216 and 218, and a lower surface 220. Impeller 200 is preferably imperforate, rectangular and most preferably square in plan view, with sides 204, 206, 208 and 210 being preferably equal in length. It also is possible that impeller 200 could be triangular, pentagonal, or otherwise polygonal in plan view. A connector (not shown) is formed in top surface 202. The connector is preferably a threaded bore that extends from top surface 202 to lower surface 220 and terminates in gas-release opening 223, though the impeller 200 can be connected to the shaft 100 in any suitable manner.
(24) This exemplary impeller 200 includes one or more cavities 224 defined in part by each of curved sides 204, 206, 208 and 210, which are beneath upper surface 230. Each cavity 224 is preferably symmetrical about the center of its respective side (204, 206, 208, or 210), although one or more of the cavities could be formed off center from its respective side. The cavities need not be identical to each other as long as gas escaping through the gas-release opening enters each cavity where it is ultimately mixed with the molten metal entering the cavity. The invention could function with fewer than or more than four cavities 224. Additionally, the cavities may be formed in any portion of impeller 200, rather than being formed at 90-degree intervals by the sides (204, 206, 208, or 210) as shown in
(25) In the present exemplary embodiment, each cavity preferably comprises an identical structure, therefore only one cavity 224 shall be described. Cavity 224 is partially defined by concave side surface 204, wherein the distance from the center of the curved surface 204 is closer to a center of the impeller 200 than the distance from ends (212, 214) of the curved surface 204 to the center of the impeller 200. Cavity 224 is further defined by upper surface 230. In the present exemplary embodiment, surface 230 of the impeller 200 is substantially flat and circular as viewed from the bottom of the impeller 200.
(26) The impeller 200 may comprise one or more channels 225 in the bottom surface 220 of the impeller 200. The channels 225 may be any size, shape, and configuration. In the present exemplary embodiment, the device comprises four channels 225, one that extends to in each of the four side cavities.
(27) The edges, such as edges 212, 214, 216 and 218, act as sheering surfaces to break apart gas bubbles into smaller bubbles as the rotor 200 rotates. The impeller 200 is threadingly received onto the impeller shaft. A lip 234 is formed between top wall 230 and top surface 202; lip 234 preferably comprises a minimum width of one quarter of an inch. Lower surface 220 comprises edges 240 juxtaposed each of the recesses 224. The impeller 200 is comprised of a heat resistant material such as graphite or ceramic.
(28) In one embodiment, the second end 104 of shaft 100 is preferably connected to impeller 200 by threading end 104 into a connector (not shown) on the impeller. If desired, shaft 100 could be connected to impeller 200 by techniques other than a threaded connection, such as by being cemented, pinned or in any other suitable manner. The use of coarse threads (4 pitch, UNC) facilitates manufacture and assembly. The threads may be tapered.
(29) Upon placing impeller 200 in molten metal bath B and releasing gas through passage 108, the gas will be released through gas-release opening 223 and at least some will flow outwardly through the channels 225 in lower surface 220, and into each cavity.
(30) As impeller 200 turns, the gas in each of cavities 224 mixes with the molten metal entering the cavity and this mixture is pushed outward from impeller 200. The released gas will also be sheared into smaller bubbles as they are struck by a shearing surface when rotor 200 rotates.
(31) By using impeller 200, high volumes of gas can be mixed with the molten metal at relatively low impeller speeds. Unlike some conventional devices that do not have cavities, the gas cannot simply rise past the side of the impeller 200. Instead at least some of the gas enters the cavities 224 and is mixed with the molten metal.
(32) An alternate, impeller 300 is shown in
(33) Impeller 300 includes two sets of cavities, wherein each set is at a different vertical position, that can capture gas and mix it with molten metal. Thus, impeller 300 is a two-stage impeller with respect to mixing gas and molten metal. Impeller 300 comprises a top surface 302, a bottom surface 320, a first stage 360 and a second stage 370. First stage 360 includes a plurality of cavities 362 wherein each cavity is juxtaposed by at least one edge, or other shearing structure, 362A.
(34) Impeller 300 also has a second stage 370 that includes four sides 304, 306, 308 and 310 four corners 312, 314, 316 and 318, and cavities 372. Impeller 300 is preferably imperforate, and rectangular (and most preferably square in plan view, with sides 304, 306, 308 and 310 being preferably equal in length). It also is possible that impeller 300 could be triangular, pentagonal, or otherwise polygonal in plan view. A connector 322 is formed in top surface 302. The connector is preferably a threaded bore that extends from top surface 302 to lower surface 320 and terminates in gas-release opening 323, though any other suitable connector may be used.
(35) One or more cavities 372 are formed in part by sides 304, 306, 308 and 310. Each cavity 372 is preferably symmetric about the center of its respective side, although one or more of the cavities could be formed off center. Further, the invention could function with fewer than or more than the cavities shown. Additionally, the cavities may be formed in any suitable portion of impeller 300 and may be of any suitable size, shape, or configuration.
(36) An impeller 300 rotates, gas is released through opening 323 and at least some of the gas enters the one or more cavities 362 and the one or more cavities 372. The respective edges, or other shearing structures 362A and 372A break the gas into smaller bubbles as rotor 300 rotates thereby helping to disperse the gas into the molten metal.
(37) Referring now to
(38) As shown in
(39) 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.