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US3375105A - Method for the production of fine grained steel - Google Patents

Method for the production of fine grained steel Download PDF

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Publication number
US3375105A
US3375105A US502476A US50247665A US3375105A US 3375105 A US3375105 A US 3375105A US 502476 A US502476 A US 502476A US 50247665 A US50247665 A US 50247665A US 3375105 A US3375105 A US 3375105A
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steel
vanadium
aluminum
fine grained
alloy
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US502476A
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Dunstan W P Lynch
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Vanadium Corp of America
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    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21CPROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C7/00Treating molten ferrous alloys, e.g. steel, not covered by groups C21C1/00 - C21C5/00
    • C21C7/0006Adding metallic additives

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  • ABSTRACT OF THE DISCLOSURE Method of producing fine grained steel by adding to said steel prior to teeming analloy containing aluminum and silicon and another alloy containing vanadium and silicon.
  • This invention relates toa novel method for treating molten steel to produce fine grain size. in the fimshed;
  • austenite When carbon or alloy steel is heated above its transformation temperature, it enters into asolid solu'tionphase known as austenite. Austenite is a crystalline structure and the size of the austenite crystals or grains is a tune tion of the degree to which the steel is heated beyond the transformation temperature. As the temperature increases beyond the transformation temperature, the austenite grain esses, sucha hardening, normalizing andannealing; require that the steel be heated to temperatures in excess of the transformation temperature, it is necessary to inhibit austenitic grain growth where a fine grain size is desired' For example, carburizing steel for case hardening is most commonly performed atabout 1700 F. which is well above the transformation temperatureof the austenitic phase. Such steels must remain fine grained after treatment. i
  • McQuaid-Ehn test is commonly used for determining the austenitic grain size, and the ASTM grain size numbers 1 are normally used for rating the steels.
  • An ASTM rating of l to 5 is considered coarse, while an ASTM rating of 5 to 8 is considered fine. Grain size ratings finer than 8 ice
  • Another detrimentalef-. fectgof aluminum is that it createsa poor. surfaceon the: ingotor'wrought product and this-results in costly conditioning, poor formability or even rejection.
  • Fine grained heat treated steels are normally preferred.
  • melting practices are used which will produce a fine grained steel.
  • the practices include additions prior to and during tapping which tend to inhibit austenitic grain growth in the final product.
  • Aluminum is most commonly used to produce fine grained steels because it is both effective and inexpensive. Normal aluminum additions for producing a fine grained plain carbon steel range from 1 lb./ ton of steel to 5 lb./ ton of steel depending upon the grade of steel and the steelmaking practice. A residual aluminum content of .02 to .O5% is desired to produce a fine grain structure. With alloy steels the residual aluminum may be as low as .015% to produce a fine grain structure.
  • V-Fe-Si vanadium-.iron-silicon alloy including some of the elements specifiedfabove is termedcomplex V-Fe-Si and is disclosed in my copending application Ser. No. 502,3 80. if
  • my method consists in treating molten steel Prior to teeming by ad i g all a minum-ir nsilicon alloy and a vanadium-iron-silicon alloy to the molten metal.
  • ad i g all a minum-ir nsilicon alloy and a vanadium-iron-silicon alloy to the molten metal.
  • the addition of aluminum and vanadium in the form of silicon. alloys as distinguished from aluminum metal and ferrovanadium produces a fine grained steel which may be treated at temperatures well within the austenitic range while maintaining a fine grain size.
  • the treatment in the ladle in each instance was to de- Calcium-ferrosilicon alloy 16.0% Ca, 57.8% Si, 'bal.
  • V-FeSi Ht. 28
  • EPQAMPLE 2 Additional ingots were made and processed in the manner described in Example 1. The ladle additions and the grain size results for the individual heats are listed below.
  • EXAMPLE 3 Additional ingots were made and processed in the manner described in Example 1. The ladle additions and the grain size results for the individual heats are listed below.
  • V-Fe-Si Ht. 15
  • EXAMPLE 4 Additional ingots were made and processed in the manner described in Example 1. The ladle additions and the trally Fe. grain size results for the individual heats are listed below.
  • Example 4 also demonstrates that when the molten steel is treated according to my novel method using the complex vanadium alloy disclosed in my copending application, the amount of vanadium necessary to assure fine grain size is far less than the amount required when other vanadium alloys are used.
  • the method of producing fine grained steel comprising adding to molten steel prior to teeming aluminum as an alloy containing aluminum and silicon and adding vanadium as another alloy containing vanadium and silicon and teeming said molten steel.
  • said alloy containing vanadium and silicon includes small amounts of columbium, titanium, zirconium and boron.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Treatment Of Steel In Its Molten State (AREA)

Description

United States Patent O 3,375,105 METHOD FOR THE PRODUCTION" on FINE GR AlNED STEEL Dunstan W. P. Lynch, Cambridge, Ohio, assignon t0. Vanadium Corporation of America,.New York, N.Y.,.
a corporation of Delaware N Drawing. Filed Oct. 22, 1965, Ser. No. 502,476 6 Claims. (Cl. 75-129) ABSTRACT OF THE DISCLOSURE" Method of producing fine grained steel by adding to said steel prior to teeming analloy containing aluminum and silicon and another alloy containing vanadium and silicon.
This invention relates toa novel method for treating molten steel to produce fine grain size. in the fimshed;
product.
When carbon or alloy steel is heated above its transformation temperature, it enters into asolid solu'tionphase known as austenite. Austenite is a crystalline structure and the size of the austenite crystals or grains is a tune tion of the degree to which the steel is heated beyond the transformation temperature. As the temperature increases beyond the transformation temperature, the austenite grain esses, sucha hardening, normalizing andannealing; require that the steel be heated to temperatures in excess of the transformation temperature, it is necessary to inhibit austenitic grain growth where a fine grain size is desired' For example, carburizing steel for case hardening is most commonly performed atabout 1700 F. which is well above the transformation temperatureof the austenitic phase. Such steels must remain fine grained after treatment. i
' Steels with large grains are termed coarse grained, while steels with small grains are termed fine grained. The
McQuaid-Ehn test is commonly used for determining the austenitic grain size, and the ASTM grain size numbers 1 are normally used for rating the steels. An ASTM rating of l to 5 is considered coarse, while an ASTM rating of 5 to 8 is considered fine. Grain size ratings finer than 8 ice However, there are many'cases'where the: additionof'. aluminum to the. steel is detrimental. For instance: trans verse'mechanical properties. ofplate products from such; steels are lower than longitudinal? mechanical properties, particularly in impact resistance. Another detrimentalef-. fectgof aluminum is that it createsa poor. surfaceon the: ingotor'wrought product and this-results in costly conditioning, poor formability or even rejection. Furthermore, aluminum cannot be added to some grades of steel be-- cause it causes poor hot-workability. Still another detrim n l if ctof. aluminum has. recentlycome to.light with. the advent of continuous. casting, in. thatv the additionof. sufiicient aluminum to. the steel in. the. ladle to. produce a fine. grained steel causes. the molten. metal to solidify. in. the relatively small tundish nozzles.
It is known that the additionof. other elements, Such as vanadium, columbium, titanium, and zirconium, either singly or in combination, will produce fine grained steels. Apart from aluminum the element most commonly used for this purpose is vanadium. The amount of vanadium normally added, as ferrovanadium, is .Q 8% to .l5 While the use of vanadium is eifective, it is relatively expensive, costing approximately ten times more. per pound than aluminum.
My novel method is directed to the treatment of molten carbon and alloy steels to produce a high quality, fine grained steel; in thecast or Wrought condition. The steel treated in accordance with my method may becontinuously cast and retains its fine grain. structure at high temperatures such as are encountered in high temperature carburizing. Additionally-, my method is. inexpensive since it, requires a very small amount of vanadium.
I have discovered that the addition of a small amount of aluminum, insutficient by itself to produce fine grained steel, plus the addition of a much smaller amount of vanadium than that required to produce, fine grained steel when used alone inaccordance with previous practices, will produce a fine grained steel.j In my novel method it is: essential that the, aluminum be added as an alloy containing both aluminum; and silicon rather than as aluminum metal. Additionally, it is essential in my method that the vanadium be added as an alloy containing vanadium may also occur. It is to be understood that the term fine grained steel, when used hereinafter, refers to steel having an ASTM number of 5 to 8 and finer as determined by the McQuaid-Ehn grain size test, unless otherwise specified.
Fine grained heat treated steels are normally preferred.
over coarse grained steels because, for a given hardness, the fine grained steel is tougher, residual stresses are lower, there is less distortion, quenching cracks are less prevalent and the steel has less retained austenite. For this reason,-
melting practices are used which will produce a fine grained steel. The practices include additions prior to and during tapping which tend to inhibit austenitic grain growth in the final product.
Aluminum is most commonly used to produce fine grained steels because it is both effective and inexpensive. Normal aluminum additions for producing a fine grained plain carbon steel range from 1 lb./ ton of steel to 5 lb./ ton of steel depending upon the grade of steel and the steelmaking practice. A residual aluminum content of .02 to .O5% is desired to produce a fine grain structure. With alloy steels the residual aluminum may be as low as .015% to produce a fine grain structure.
and silicon rather than as ferrovanadium. The alloys disclosed in my copending application Ser. No. 502,380, filed on even date herewith are especially adapted for this purpose.
I have, alsddiscovered that if the alloy of vanadium and silicon contains small amounts of one or more carbide and nitride forming elements, for example, columbium, titanium, zirconium and boron, even smaller additions of vanadium produce a fine grained steel. When an alloy including carbide and nitride forming elements is used, the steel remains fine grained after heating to temperatures in excess of 1700 F. A vanadium-.iron-silicon alloy including some of the elements specifiedfabove is termedcomplex V-Fe-Si and is disclosed in my copending application Ser. No. 502,3 80. if
Basically my method consists in treating molten steel Prior to teeming by ad i g all a minum-ir nsilicon alloy and a vanadium-iron-silicon alloy to the molten metal. The addition of aluminum and vanadium in the form of silicon. alloys as distinguished from aluminum metal and ferrovanadium produces a fine grained steel which may be treated at temperatures well within the austenitic range while maintaining a fine grain size.
In order to determine the grain size of; steel produced by my process, A181 1040 steel heats were melted in a 300 pound induction furnace and various additions were made to the molten metal after it was tapped into a ladle. The ladles of steel were then teemed into 4" x 4" x 24" molds. The resulting ingots were identified and forged to 1% square bars. Sections were cut from these bars for the McQuaid-Ehn grain size tests and the ASTM grain size was determined after heat treatment.
In melting the steel heats, Armco scrap was melted in the induction furnace, the slag removed and suflicient silicon added as 50% FeSi to lower the FeO content and leave a residual of 0.10% silicon in the bath. Sufiicient pig iron was added to give .40% carbon and when in solution, electrolytic manganese and ferrosilicon were added to produce the required composition. The heats were then tapped at 2900 F. into the ladle and treated.
The analysis of the steels after treatment met the AISI 1040 specification and had the following composition ranges:
Percent C .4l-.43 Mn .82.88 P .0.012 S .017.019 Si .24-.32
The treatment in the ladle in each instance was to de- Calcium-ferrosilicon alloy 16.0% Ca, 57.8% Si, 'bal.
, essentially Fe. Aluminum-silicon-iron alloy 19.0% A1, 38.9% Si, bal.
essentially Fe. Aluminum 99.5% Al. Ferrovanadium 75.15% V, bal. essentially Fe. V-Fe-Si (Ht. 28.00% V, 51.48% Si, bal.
essentially Fe. V-FeSi (Ht. 28) 51.34% V, 24.82% Si, bal.
' essentially Fe. Complex VFe-Si (Ht. 16) 29.55% V, 46.12% 2.31% Cb, 2.04%
1.98% Zr, 0.11% B, 1.75% Al, 1.59% Ba, 2.34% Mn, bal. essen- Si, Ti,
4 It will be observed that the addition of .02% aluminum to AISI 1040 steel, either as aluminum or as an alloy containing aluminum and silicon produced a coarse grained steel.
EPQAMPLE 2 Additional ingots were made and processed in the manner described in Example 1. The ladle additions and the grain size results for the individual heats are listed below.
Heat No. Ladle Additions McQuaid-l'ghn Grain Size, 1,100" F 148 .OZFVgVAI as alumlnum+.06% V as 7, 8 plus 5, (Ya. 21C .02% Al as Alumlnum-\-.04% V as Duplex 5% plus l-4. 21B .0%9Z,V.:Al as Al-Fe-Sl+.04% V as Duplex 5-8 plus 1-4.
EXAMPLE 3 Additional ingots were made and processed in the manner described in Example 1. The ladle additions and the grain size results for the individual heats are listed below.
Heat No. Ladle Additions McQuaid-Ehn Gr Size, 1,700 F.
240 .02% Alas Aluminum-+01% V as Duplex 5-8 plus 1-4.
V-Fe-Si (Ht. 15). 24B. .02% Al as AlFeSi+.04% V as 7, 8 and finer.
V-Fe-Sl (Ht. 15).
When the vanadium was added to the steel as the V- Fe-Si alloy, a fine grained steel was P oduced at the lower vanadium level but, as shown by a comparison of heats 24B and 24C, only when the aluminum was added as an alloy containing silicon. It is pointed out that the grain size for Heat 246 is the same as for Heats 21B and 21C in Example 2.
EXAMPLE 4 Additional ingots were made and processed in the manner described in Example 1. The ladle additions and the trally Fe. grain size results for the individual heats are listed below.
McQuald-Ehn Grain Size Heat N0. Ladle Additions 3011 .02% Al as A1-Fe Si+.005% V as 7, 8 and finer, few 6's Duplex 7, 8 and finer plus V-Fe-Si (Ht. l5 "s.
D .02% Al as Al-Fe-Si+.0025% V as do 7, 8 and finer, few 6s.
Complex V-Fe-Si (Ht. l6).
29D .02% Al as Al-Fe-Si+.04% V as V-Fe- 7, 8 and finer Duplex 7, 8 and finer plus Sl (Ht. 28). l-3S.
31C .02% Al as Al-Fe-Si+.04% V as do 7,8 and finer, iew fis.
Complex V-Fe-Si (Ht. 16).
The following examples will serve to illustrate the eifect of various ladle additions on the McQuaid-Ehn. grain size of AISI 1040 steel.
EXAMPLE 1 The ladle additions exclusive of the 2 lbs. of calcium-fer-' rosilicon alloy per ton of steel which was added to each ladle and the resulting grain size for the individual heats are listed below:
Heat No. Ladle Additions l\lcQ,uaid-Ehn Graln Size, 1,700" F..
5A .02% Alas Aluminum With an addition of .02% aluminum as an alloy contk'aun'ing silicon, extremely low additions of vanadium as the V-Fe-Si alloy or as the complex V-Fe-Si alloy containing small amounts of other elements produced fine grained steel. The steels treated with the complex V-Fe-Si alloy were also fine grained at higher temperatures. To show that the fine grain at 1800 F. is a characteristic of the complex V-Fe-Si alloy used and not the level of the vanadium addition, the higher vanadium additions of .04% as each of the two vanadium alloys containing silicon are included in the example. In all of the above tests the core of the carburized specimens had the same grain size as the grain size recorded for the case.
The addition of the calcium-ferrosilicon deoxidizer prior to the alurninum-iron-silicon alloy addition is not essental but assures more uniform aluminum recoveries. Other deoxidizers could be used if desired.
The above examples demonstrate that the aluminum must be added as an alloy of aluminum containing silicon, and that the vanadium must be added as an alloy of vanadium containing silicon. Example 4 also demonstrates that when the molten steel is treated according to my novel method using the complex vanadium alloy disclosed in my copending application, the amount of vanadium necessary to assure fine grain size is far less than the amount required when other vanadium alloys are used.
In addition it has been demonstrated that minute amounts of vanadium, when added as the novel complex vanadium silicon alloy containing small amounts of elements such as columbium, titanium, zirconium, boron, etc., and in accordance with my novel method, will produce a fine grained steel which steel will be fine grained at higher temperatures such as used for high temperature carburizing. The amounts of the effective elements other than vanadium in the .0025% vanadium addition (Ht. 30D) were extremely minute and, except for vanadium, are too low to be determined quantitatively in the finished steel. Based on the knowledge of grain size control of steel, such levels of addition, either singlyor in combination, would not have any effect on the grain size of the steel.
My invention may be embodied Within the scope of the appended claims.
I claim:
1. The method of producing fine grained steel comprising adding to molten steel prior to teeming aluminum as an alloy containing aluminum and silicon and adding vanadium as another alloy containing vanadium and silicon and teeming said molten steel.
2. The method set forth in claim 1 wherein said aluminum addition is less than about 02%.
3. The method set forth in claim 1 wherein said vanadium addition is about .-O05%.
4. The method set forth in claim 1 wherein said aluminum addition is less than about .02% and said vanadium addition is about .005
5. The method set forth in claim 1 wherein said alloy containing vanadium and silicon includes small amounts of columbium, titanium, zirconium and boron.
6. The method set forth in claim 1 wherein said alloy containing vanadium and silicon includes small amounts of columbium, titanium, zirconium and boron, and said vanadium addition is .0025%.
References Cited UNITED STATES PATENTS 2,221,783 11/1940 Critchett et a1. 5 8 2,280,283 4/1942 Crafts 755 8 X 2,291,842 8/ 1942 Strauss 75-5 8 2,296,938 9/ 1942 Lytle 755 8 BENJAMIN HENKIN, Primary Examiner.
DAVID L. RECK, Examiner.
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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE28790E (en) * 1969-07-16 1976-04-27 Jones & Laughlin Steel Corporation High-strength low-alloy steels having improved formability
US4374667A (en) * 1981-10-14 1983-02-22 Reading Alloys, Inc. Ferrovanadium carbide addition agents and process for their production
US4484946A (en) * 1981-06-02 1984-11-27 Metal Research Corporation Method of producing iron-, nickle-, or cobalt-base alloy with low contents of oxygen, sulphur, and nitrogen
US5556485A (en) * 1994-11-07 1996-09-17 Bethlehem Steel Corporation Bake hardenable vanadium containing steel and method of making thereof
US5656102A (en) * 1996-02-27 1997-08-12 Bethlehem Steel Corporation Bake hardenable vanadium containing steel and method thereof
US6685882B2 (en) 2001-01-11 2004-02-03 Chrysalis Technologies Incorporated Iron-cobalt-vanadium alloy
US20120255398A1 (en) * 2011-04-06 2012-10-11 Hoeganaes Corporation Vanadium-Containing Powder Metallurgical Powders And Methods of Their Use
US9351889B2 (en) 2013-12-16 2016-05-31 Pride Mobility Products Corporation Elevated height wheelchair
US11191685B2 (en) 2016-02-27 2021-12-07 Pride Mobility Products Corporation Adjustable height wheelchair

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US2221783A (en) * 1938-04-14 1940-11-19 Electro Metallurg Co Addition agent and its use
US2280283A (en) * 1940-01-05 1942-04-21 Electro Metallurg Co Deep-hardening boron steels
US2291842A (en) * 1940-07-18 1942-08-04 Vanadium Corp Production of steel
US2296938A (en) * 1940-11-20 1942-09-29 Electro Metallurg Co Welding rod and method of manufacturing welding rods

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2221783A (en) * 1938-04-14 1940-11-19 Electro Metallurg Co Addition agent and its use
US2280283A (en) * 1940-01-05 1942-04-21 Electro Metallurg Co Deep-hardening boron steels
US2291842A (en) * 1940-07-18 1942-08-04 Vanadium Corp Production of steel
US2296938A (en) * 1940-11-20 1942-09-29 Electro Metallurg Co Welding rod and method of manufacturing welding rods

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE28790E (en) * 1969-07-16 1976-04-27 Jones & Laughlin Steel Corporation High-strength low-alloy steels having improved formability
US4484946A (en) * 1981-06-02 1984-11-27 Metal Research Corporation Method of producing iron-, nickle-, or cobalt-base alloy with low contents of oxygen, sulphur, and nitrogen
US4374667A (en) * 1981-10-14 1983-02-22 Reading Alloys, Inc. Ferrovanadium carbide addition agents and process for their production
US5556485A (en) * 1994-11-07 1996-09-17 Bethlehem Steel Corporation Bake hardenable vanadium containing steel and method of making thereof
US5656102A (en) * 1996-02-27 1997-08-12 Bethlehem Steel Corporation Bake hardenable vanadium containing steel and method thereof
US6685882B2 (en) 2001-01-11 2004-02-03 Chrysalis Technologies Incorporated Iron-cobalt-vanadium alloy
US20040089377A1 (en) * 2001-01-11 2004-05-13 Deevi Seetharama C. High-strength high-temperature creep-resistant iron-cobalt alloys for soft magnetic applications
US6946097B2 (en) 2001-01-11 2005-09-20 Philip Morris Usa Inc. High-strength high-temperature creep-resistant iron-cobalt alloys for soft magnetic applications
US20070289676A1 (en) * 2001-01-11 2007-12-20 Philip Morris Usa Inc. High-strength high-temperature creep-resistant iron-cobalt alloys for soft magnetic applications
US7776259B2 (en) 2001-01-11 2010-08-17 Philip Morris Usa Inc. High-strength high-temperature creep-resistant iron-cobalt alloys for soft magnetic applications
US9340855B2 (en) * 2011-04-06 2016-05-17 Hoeganaes Corporation Vanadium-containing powder metallurgical powders and methods of their use
CN103459632A (en) * 2011-04-06 2013-12-18 赫格纳斯公司 Vanadium-containing pulverulent metallurgical powder and method of use thereof
US20120255398A1 (en) * 2011-04-06 2012-10-11 Hoeganaes Corporation Vanadium-Containing Powder Metallurgical Powders And Methods of Their Use
US10351938B2 (en) 2011-04-06 2019-07-16 Hoeganaes Corporation Vanadium-containing powder metallurgical powders and methods of their use
US9566200B2 (en) 2013-12-16 2017-02-14 Pride Mobility Products Corporation Elevated height wheelchair
US9808383B2 (en) 2013-12-16 2017-11-07 Pride Mobility Products Corporation Elevated height wheelchair
US10130532B2 (en) 2013-12-16 2018-11-20 Pride Mobility Products Corporation Elevated height wheelchair
US9351889B2 (en) 2013-12-16 2016-05-31 Pride Mobility Products Corporation Elevated height wheelchair
US10561548B1 (en) 2013-12-16 2020-02-18 Pride Mobility Products Corporation Elevated height wheelchair
US10588797B2 (en) 2013-12-16 2020-03-17 Pride Mobility Products Corporation Elevated height wheelchair
US10687997B2 (en) 2013-12-16 2020-06-23 Pride Mobility Products Corporation Elevated height wheelchair
US10828212B2 (en) 2013-12-16 2020-11-10 Pride Mobility Products Corporation Elevated height wheelchair
US11141330B2 (en) 2013-12-16 2021-10-12 Pride Mobility Products Corporation Elevated height wheelchair
US11571345B2 (en) 2013-12-16 2023-02-07 Pride Mobility Products Corporation Elevated height wheelchair
US11998495B2 (en) 2013-12-16 2024-06-04 P{ride Mobility Products Corporation Elevated height wheelchair
US11191685B2 (en) 2016-02-27 2021-12-07 Pride Mobility Products Corporation Adjustable height wheelchair

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