Process of manufacturing of segments for carbon thrust bearing
11065672 · 2021-07-20
Inventors
Cpc classification
F16C17/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2223/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21K1/04
PERFORMING OPERATIONS; TRANSPORTING
C21D1/18
CHEMISTRY; METALLURGY
B21J1/06
PERFORMING OPERATIONS; TRANSPORTING
B21D53/10
PERFORMING OPERATIONS; TRANSPORTING
C21D1/25
CHEMISTRY; METALLURGY
F16C2220/70
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/108
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2220/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B24D11/001
PERFORMING OPERATIONS; TRANSPORTING
C21D1/00
CHEMISTRY; METALLURGY
F16C33/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B21D53/10
PERFORMING OPERATIONS; TRANSPORTING
F16C33/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C21D1/25
CHEMISTRY; METALLURGY
C21D1/18
CHEMISTRY; METALLURGY
C21D1/00
CHEMISTRY; METALLURGY
B21J5/02
PERFORMING OPERATIONS; TRANSPORTING
B21J1/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A process of manufacturing of segment for carbon thrust bearing uses stainless-steel (SS) round bars/sheets/logs of suitable grade as raw material. The SS round bars/sheets/logs undergo cutting operation to cut into SS billets. The billets successively undergo heating and hot forging processes to form segments of desired shapes. Thereafter, the segment is subjected to heat treatment process i.e. stress relieving, hardening and tempering process successively for obtaining consistent and uniform grain structure, mechanical properties and physical properties of segments which are cost-effective in terms of lower maintenance and lower handling efforts. After heat-treatment process, segment undergoes surface-finishing processes i.e. grinding, lapping and polishing successively for obtaining mirror like surface finishing that gives greater anti-friction property and lower co-efficient of friction. The manufacturing process according to present invention yields consistent grain structure, refine, dense and uniform microstructure of segments which imparts optimum strength, ductility, toughness and resistance to impact and fatigue.
Claims
1. A process of manufacturing of segments for carbon thrust bearing comprising the following steps: a) cutting of stainless steel round bars/strips/logs to form steel billets; b) heating of the steel billets obtained in step (a) at 900° C.-1000° C. in an induction furnace; c) carrying out a hot forging process on the steel billets obtained in step (b) using forging dies for forming segments of a desired shape; d) carrying out a stress relieving process on the segments obtained in step (c) at a temperature of 545° C.-555° C. to reduce internal residual stress and to prevent formation of excessive thermal stress; e) carrying out a hardening process after the stress relieving process on the segments obtained in step (d) at a temperature of 1040° C. to increase the hardness and toughness and to acquire uniform grain structure of the segments; f) carrying out a tempering process after the hardening process on segments obtained in step (e) at a temperature of 245° C.-255° C. to reduce brittleness and excess hardness; g) implementing a grinding process after the tempering process on the segments obtained in step (f) to acquire a finished surface of the segments; h) implementing a lapping process and a polishing process successively on the segments obtained in step (g) to obtain a mirror-like surface of the segments.
2. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein a steel grade of the stainless steel round bars/strips/logs is selected from the group consisting of AISI 420, AISI 420A, AISI 420B, AISI 420C, and AISI 410.
3. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein the hot forging process in step (c) is carried out in a mechanical press, a hydraulic press or a friction screw press.
4. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein the hot forging process in step (c) is carried out using an open die forging or closed die forging.
5. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein a trimming process and a grinding process are successively carried out on the segments obtained in step (c) if open die forging is used as a forging process.
6. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein the grinding process in step (g) is carried out in a bench grinder, a vertical rotary grinding machine or a horizontal surface grinding machine.
7. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein the hardening process in step (e) is induction hardening.
8. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 1 wherein the lapping process and polishing process in step (h) are successively carried out in a lapping machine and a polishing machine respectively.
9. The process of manufacturing of segments for carbon thrust bearing as claimed in claim 5 wherein the trimming process is carried out in a power press.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1)
(2)
(3)
(4)
SUMMARY OF INVENTION
(5) A process of manufacturing of segment for carbon thrust bearing of the present invention uses stainless-steel (SS) (round bars)/sheets/logs of suitable grade as raw material. The SS (round bars)/sheets/logs undergo cutting operation to cut into SS billets of predetermined sizes. The billets are heated in induction furnace at 900° C.-1000° C. Thereafter, billets undergo open-die hot forging or closed-die hot forging for acquiring the desired shape of segments. After open-die hot forging, the segment is subjected to trimming-grinding processes successively to remove the flashes formed on edges of the segment. For closed-die hot forging, trimming-grinding processes are not required. Thereafter, the segment is subjected to heat treatment process i.e. stress relieving, hardening and tempering process successively for obtaining predetermined mechanical properties and physical properties of segments which are cost-effective in terms of lower maintenance and lower handling efforts. After heat-treatment process, the segment undergoes surface-finishing processes i.e. surface grinding for obtaining final finished surface and thereafter lapping and polishing process are successively carried out for obtaining optimum degree of flatness and mirror like surface finishing of segment that gives greater anti-friction property and lower co-efficient of friction.
DETAILED DESCRIPTION OF INVENTION
(6) The nature of the invention and the manner in which it works is clearly described in the provisional specification. The invention has various embodiments and they are clearly described in the following pages of the provisional specification. Before explaining the present invention, it is to be understood that the phraseology and terminology employed herein is for the purpose of description and not of limitation.
(7) The present invention refers to a manufacturing process to eliminate the excess processing steps of the conventional process of manufacturing of the segments for carbon thrust bearings and to achieve exceptional strength, hardness, ductility, toughness and uniform grain structure of the segments for carbon thrust bearing.
(8) Before explaining the present invention, it is to be understood that the term “re-crystallization temperature” refers to the temperature at which the deformed grains of metal are replaced by a new set of defects-free (stress-free) grains for reduction in strength and hardness and simultaneous increase in ductility. The re-crystallization temperature for steels is typically ranges between 400° C.-700° C.
(9) In accordance with the present invention, the process of manufacturing of segments for carbon thrust bearing uses stainless steel (hereinafter referred as SS) round bars/sheets/logs as raw material or feed stock. This SS round bars/sheets/logs undergo cutting operation in cutting press to cut into SS billets of predetermined size. Thereafter, the steel billets are heated in induction furnace at 900° C.-1000° C. above its re-crystallization temperature to reduce the residual stress and for making it easy for machining. The induction heating provides quick, efficient and uniform heating of the steel billets. The heated SS billets undergo hot forging process preferably in mechanical press, hydraulic press or friction screw press having forging dies for forming the desired shape of the segments for carbon thrust bearing. In hot forging process, the SS steel billets are positioned between the forging-dies and subjected to a (single or) plurality of strokes through the ram/piston of the mechanical press, hydraulic press or friction screw for forming the desired shape of segments. In hydraulic press a (single or) plurality of strokes is applied on the ram/piston through the hydraulic fluid pressure. In mechanical press and friction screw press, a (single or) plurality of strokes is applied on the ram/piston through the motor. After hot forging process, the steel billets acquire the desired shape of the segments according to the shape of the dies.
(10) If the open dies are used in hot forging process, it is called open-die hot forging process and if closed dies are used in hot forging process, it is called closed-die hot forging process.
(11) During open die hot forging process, a thin layer of squeezed metal is formed on the edges of said segment and parting line of the mold, said a thin layer of squeezed metal is called as “flash”. Hence, after open-die hot forging process the segment is required to be subjected to trimming and grinding process successively preferably in power press and bench grinder respectively to remove the flashes formed on the edges of the segment during open-die hot forging and to get precision surface finishing of the segment. If the closed dies are used in hot forging process, the flashes formed on the edges of segment during closed-die hot forging process is negligible and hence the trimming and grinding processes are eliminated. The closed-die hot forging is also known as impression die forging process.
(12) Thereafter, for achieving desired mechanical and physical properties of the resultant segment, the heat treatment process i.e. stress relieving, hardening and tempering is successively carried out in order to obtain fine and uniform grain structure of the segment and to increase the strength, hardness, ductility and toughness of the segment for carbon thrust bearing. In stress relieving process, the segment is heated up to temperature of 545° C.-555° C. in an oven or furnace and holding at that temperature long time enough to achieve desired reduction in internal residual stresses and then the segment is cooled at a sufficiently slow rate to avoid formation of excessive thermal stress. The reduction in internal residual stresses of segment depends on the composition of steel, selection of temperature, time and rate of cooling.
(13) It is to be understood that the term “critical temperature” is the transformation temperature at which the steel goes into solid solution where atoms of the metals and atoms of the carbon in the steel mix freely and ultimately bond together. The temperature at which this process begins is called lower critical temperature of the steel. The critical temperature for steels is generally ranges from 1335° F.-1525° F. (724° C.-830° C.). The lower critical temperature for steels is usually ranges from 600° C.-724° C.
(14) After stress relieving process, the segment is subjected to hardening process for increasing the hardness and toughness of the segment and to acquire uniform grain structure of the segment. In hardening process, the segment is heated at 1040° C. above its critical temperature in furnace and holding the segment at this temperature for definite period of time about 80-120 minutes and then quenched in quenching medium of oil or air till it reaches to room temperature to achieve the desired hardness of the segment. The time generally depends upon the material characteristics, dimension and thickness of the segment and the hardness of segments achieved depends on rate of quenching. It is to be noted that sudden quenching greatly increases the hardness of the segments.
(15) After hardening, the tempering process is carried out to remove the quenching stress, to reduce brittleness and excess hardness, to increase toughness and to obtain predetermined mechanical and physical properties of the segments. In tempering process, the hardened segment is reheated at temperature 245° C.-255° C. below its lower critical temperature and gradually cooled at room temperature at required cooling rate to relive quenching stresses and to obtain required values of mechanical properties i.e. strength, hardness, ductility, toughness. The segment obtained after tempering is having better mechanical and physical properties. The mechanical properties of the segment also depend upon the tempering temperature, tempering time and cooling rate. The heat treatment process increases the mechanical properties i.e. wear resistance and corrosion resistance. After heat treatment process, the segment undergoes surface finishing processes i.e. surface grinding for obtaining final finished surface and thereafter lapping and polishing process are successively carried out for obtaining optimum degree of flatness and mirror like surface finishing of segment that gives greater anti-friction property and lower co-efficient of friction. Further, said surface finishing processes i.e. surface grinding, lapping and polishing are carried out on grinding machine, lapping machine and polishing machine respectively.
(16) Further, the present manufacturing process yields consistent grain structure of the segment which is shown in
(17) The present invention is illustrated more in details in the following example. The example describes and demonstrates embodiments within the scope of the present invention. This example is given solely for the purpose of illustration and is not to be construed as limitations of the present invention, as many variations thereof are possible without departing from spirit and scope.
EXAMPLE 1
(18) a) The stainless steel round bar of grade AISI 420B (SS 420B) was selected as feed stock or raw materials and was undergone cutting operation in cutting press to form billets;
(19) b) Said billets were undergone heating process at temperature of 900° C.-1000° C. in induction furnace;
(20) c) The steel billets obtained in step (b) were undergone hot forging process in mechanical press using closed forging dies for forming segments of desired shape;
(21) d) The segments obtained in step (c) were undergone stress relieving process at temperature of 545° C.-555° C. to reduce internal residual stress and to prevent the formation of excessive thermal stresses;
(22) e) The segments obtained in step (d) were undergone hardening process at temperature of 1040° C. to increase the hardness and toughness and to acquire uniform grain structure of the segment;
(23) f) The segments obtained in step (e) were subjected to tempering process at temperature of 245° C.-255° C. to reduce brittleness and excess hardness;
(24) (g) The segments obtained in step (f) were undergone grinding process in grinding machine to acquire finished surface of the segment;
(25) (h) The segments obtained in step (g) were successively undergone lapping process and polishing process in lapping machine and polishing machine respectively to obtain optimum degree of surface finishing and flatness for achieving mirror like surface of segment.
(26) Improved mechanical properties of segments obtained by said manufacturing process steps (a-g) are given in below table 1 in comparison with the mechanical properties of segments obtained by conventional investment casting process:
(27) TABLE-US-00001 TABLE 1 Mechanical Segments obtained by Segments obtained by Properties present process conventional process Hardness 51 HRC 46 HRC Compressive 89.55 KN 68.70 KN strength
(28) Further, the stainless steel strips/logs of grade SS 420B selected as feed stock or raw materials comprised of the composition given below in Table 2:
(29) TABLE-US-00002 TABLE 2 Element Obtain Specified value as per Sr. No. tested value in % grade SS 420 1 Carbon as C 0.308 0.15 Min. 2 Silicon as Si 0.344 1.00 Max. 3 Manganese 0.494 1.00 Max. as Mn 4 Sulphur as S 0.034 0.030 Max. 5 Phosphorous 0.016 0.040 Max. as P 6 Nickel as Ni 0.333 — 7 Chromium 12.171 12.00 to 14.00 as Cr 8 Molybdenum 0.158 — as Mo
Advantages:
(30) The novel process of manufacturing of segments for carbon thrust bearing according to present invention is an efficient, economic and timesaving which eliminates tedious and expensive processing steps of conventional manufacturing process of segments for carbon thrust bearing. Further, the present manufacturing process yields consistent grain structure of the segment (as shown in