US3475164A - Steels for hydrocracker vessels containing aluminum,columbium,molybdenum and nickel - Google Patents
Steels for hydrocracker vessels containing aluminum,columbium,molybdenum and nickel Download PDFInfo
- Publication number
- US3475164A US3475164A US587963A US3475164DA US3475164A US 3475164 A US3475164 A US 3475164A US 587963 A US587963 A US 587963A US 3475164D A US3475164D A US 3475164DA US 3475164 A US3475164 A US 3475164A
- Authority
- US
- United States
- Prior art keywords
- molybdenum
- nickel
- columbium
- steels
- steel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910000831 Steel Inorganic materials 0.000 title description 35
- 239000010959 steel Substances 0.000 title description 35
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title description 30
- 229910052750 molybdenum Inorganic materials 0.000 title description 16
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 title description 15
- 239000011733 molybdenum Substances 0.000 title description 15
- 229910052759 nickel Inorganic materials 0.000 title description 15
- 239000010955 niobium Substances 0.000 title description 14
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 title description 14
- 229910052782 aluminium Inorganic materials 0.000 title description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title description 11
- 229910045601 alloy Inorganic materials 0.000 description 17
- 239000000956 alloy Substances 0.000 description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 12
- 229910052799 carbon Inorganic materials 0.000 description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 11
- 238000010438 heat treatment Methods 0.000 description 9
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 7
- 229910052739 hydrogen Inorganic materials 0.000 description 7
- 239000001257 hydrogen Substances 0.000 description 7
- 229910052742 iron Inorganic materials 0.000 description 6
- 229910052710 silicon Inorganic materials 0.000 description 6
- 239000010703 silicon Substances 0.000 description 6
- 238000004517 catalytic hydrocracking Methods 0.000 description 5
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 125000004429 atom Chemical group 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000005253 cladding Methods 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000005984 hydrogenation reaction Methods 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910001339 C alloy Inorganic materials 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- YZCKVEUIGOORGS-UHFFFAOYSA-N Hydrogen atom Chemical compound [H] YZCKVEUIGOORGS-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 238000004523 catalytic cracking Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- -1 iron carbides Chemical class 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000003389 potentiating effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 239000004246 zinc acetate Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
Definitions
- hydrocracking involves a process of hydrogenation coupled with catalytic cracking wherein petroleum feed stock is treated with hydrogen gas under pressure (about 1000 to 2000 p.s.i.g.) at relatively high temperatures (600 F. to 850 F.) in the presence of a catalyst to produce gasoline or other high grade distillate. While the basic concept spans a period of nearly forty years, it has only been during the last decade that commercial exploitation of any consequence has been undertaken. But within this short period the impact industrially has been striking, a point perhaps best illustrated by a recent report which indicated that 38 gallons of gasoline were extracted from a 42-gallon barrel of crude using hydrocracking as opposed to but 21 gallons utilizing more conventional processing. This underscores the reasons for the expected expansion of hydrocracking.
- the problem is somewhat more complex than one of simply using a steel of high strength.
- the hydrocracking reaction is conducted at elevated temperature, thus requiring a steel which not only retains high strength at elevated temperature but which also exhibits high temperature stability, i.e., the steel must perform without degradation of mechanical properties over long periods.
- This focuses emphasis on the fact that the steel must be tough and ductile at ambient and operating temperatures and resistant to temper embrittlement.
- a steel irrespective of its structural constitution, must manifest the capability of resisting hot hydrogen attack. If a steel is unable to cope with hot hydrogen, it thus becomes subject to blistering or fissuring even though cladded with austenitic stainless.
- the interior surface of hydrocracker vessel walls are, for the most part, cladded with austenitic stainless. Because of the very substantial wall thickness of vessels now in use, this must be accomplished by the weld overlay procedure, a costly and undesirable technique since it must be performed after fabrication of the vessel. But with appropriate high strength steels and accompanying thinner walls, the advantages of standard roll cladding could be realized.
- alloys contemplated herein contain (in percent by weight) carbon in an amount up to less than 0.04%, about 5% to 10% nickel, about 0.7% to 1.2% aluminum, from 0.5% to 2% molybdenum, up to 1.5% chromium, up to 1% manganese, up to 1% silicon, up to 0.12% columbium, and most advantageously from 0.008% to 0.08% columbium, the balance being essentially iron.
- Constituents such as nitrogen, oxygen, sulfur and phosphorus should be maintained 'at low levels consistent with good commercial steelmaking practice.
- the carbon content of the steels should be less than 0.04% and it is beneficial that it not exceed 0.03%; otherwise, the risk is increased that nascent hydrogen evolved during the hydrocracking operation (and which permeates a stainless cladding) will combine or react with carbon present in the form of iron carbides.
- This reaction establishes the environment for methane gas to form at grain boundaries and other discontinuities.
- suflicient pressure may be built up from the trapped gas to cause fissuring or cracking.
- relatively low carbon per se is not necessarily a complete penacea since other low carbon steels have been tested with resulting failure.
- Nickel is required to confer adequate hardenability. Suitable nickel ranges are from 5% to 7% and, for optimum hardenability, 8% to 9.5%.
- Aluminum is a potent hardening and strengthening constituent, but excessive amounts thereof, e.g., 1.5%, should be avoided if the ability of the steels to absorb impact energy is not to be drastically impaired.
- Molybdenum confers strength and resistance to temper embrittlement and a particularly satisfactory range thereof is from 0.75% to 1.5%.
- Columbium it has been found, imparts strength without adversely affecting toughness, provided that amounts appreciably above 0.12% are avoided. Too, it is deemed that columbium is effective in resisting fissuring, i.e., it is capable of combining with carbon to form carbides which are less readily attacked by hydrogen.
- the Yield ,Strength (Y .S.) at 0.2% offset and Ultimate Tensile Strength (U.T.S.) are given in pounds per square inch (P.S.I.), the Elongation (EL) and Reduction in Area (R.A.) values in percent and the Charpy V-notch impact toughness (C.V.N.) determinations in foot-pounds (ft.-lbs.).
- Bal. ba1ance plus inpurities.
- the alloys within the invention manifested satisfactory room and elevated temperature mechanical properties, a tensile strength of nearly 200,000 p.s.i. and an impact strength of 30 ft.-lbs. (Alloy 5) at room temperautre and a strength of over 160,000 p.s.i. at 850 F. being deemed quite satisfactory.
- Alloys 1 and 2 Heating Treatment B
- Charpy V Notch impact strength was quite low, to wit, 6-7 ft.-lbs.
- a further compositional range suitable for hydrocracker applications is as follows: carbon up to 0.03%, 5% to 9.5% nickel, 0.75% to 1.2% aluminum, 0.75% to 1.5% molybdenum, 0.008% to 0.08% or 0.1% columbium, up to 1% chromium, up to 0.75% manganese, up to 0.5% silicon, and the balance essentially iron.
- a particularly satisfactory steel consists essentially of about 0.02% carbon, about 9% nickel, about 1% aluminum, about 0.9% molybdenum, about 0.06% to 0.1% columbium, about 0.5 manganese, about 0.2% silicon, with the balance being iron.
- the subject steels can otherwise be used in sundry environments, particularly applications where steels affording both relatively high strength and good toughness are required.
- the steels can be produced and used in the form of plate, bar, rod, forgings, etc.
- a novel alloy steel adapted for use in fabricating a hydrocracker vessel therefrom, said steel consisting essentially of less than 0.04% carbon, about 5% to 10% nickel, about 0.7% to 1.2% aluminum, from 0.5% to 2% molybdenum, columbium present up to 0.12%, up to 1.5 chromium, up to 1% manganese, up to 1% silicon, up to 5% cobalt, up to 2% copper, up to 2% tungsten, and the balance essentially iron.
- a steel in accordance with claim 1 containing at least 0.008% columbium.
- a steel in accordance with claim 7 consisting essentially of about 0.02% carbon, 9% nickel, about 1% aluminum, about 0.9% molybdenum, about 0.06% to 0.1% columbium, about 0.5% manganese and about 0.2% silicon.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Description
United States Patent 3,475,164 STEELS FOR HY DROCRACKER VESSELS CON- TAINING ALUMINUM, COLUMBIUM, M0- LYBDENUM AND NICKEL Peter Paul Hydrean, Mahwah, N.J., assignor to The International Nickel Company, Inc., New York, N.Y., a corporation of Delaware No Drawing. Filed Oct. 20, 1966, Ser. No. 587,963 Int. Cl. C22c 39/20, 37/10, 39/02 US. Cl. 75124 9 Claims ABSTRACT OF THE DISCLOSURE Steel which contains nickel, aluminum, molybdenum, columbium and low carbon offers a desirable combination of mechanical characteristics at elevated temperature and also resists temper embrittlement and hot hydrogen attack. Such properties in a steel are attractive in the fabrication of hydrocrackers.
As is generally known to those skilled in the art, hydrocracking involves a process of hydrogenation coupled with catalytic cracking wherein petroleum feed stock is treated with hydrogen gas under pressure (about 1000 to 2000 p.s.i.g.) at relatively high temperatures (600 F. to 850 F.) in the presence of a catalyst to produce gasoline or other high grade distillate. While the basic concept spans a period of nearly forty years, it has only been during the last decade that commercial exploitation of any consequence has been undertaken. But within this short period the impact industrially has been striking, a point perhaps best illustrated by a recent report which indicated that 38 gallons of gasoline were extracted from a 42-gallon barrel of crude using hydrocracking as opposed to but 21 gallons utilizing more conventional processing. This underscores the reasons for the expected expansion of hydrocracking.
In respect of the hydrocracker vessels per se, a common characteristic to all is their massiveness. Installed, a by no means unusual vessel is on the order of 100 feet in length, 10 feet in diameter (internal), and 7 inches thick, with a weight of one million pounds. As can be appreciated, the very magnitude of such dimensions, particularly wall thickness, not only gives rise to fabricating difficulties but renders transportion and erection (situs) particularly troublesome. Presently, these vessels are fabricated from a normalized and stress-relieved, low strength 2% chromium-1% molybdenum steel (ASTM, A387D). Now, it is the low strength thereof (60,000 to 80,000 p.s.i. ultimate) which is primarily responsible for the exceedingly thick walls necessary to resist the relatively high pressures encountered in operation. Accordingly, there is a more than definite commercial interest in utilizing higher strength steels whereby wall thickness, overall weight, etc., would be reduced, thereby minimizing the difiiculties now experienced.
But the problem is somewhat more complex than one of simply using a steel of high strength. By way of explanation, the hydrocracking reaction is conducted at elevated temperature, thus requiring a steel which not only retains high strength at elevated temperature but which also exhibits high temperature stability, i.e., the steel must perform without degradation of mechanical properties over long periods. This focuses emphasis on the fact that the steel must be tough and ductile at ambient and operating temperatures and resistant to temper embrittlement. It has been proposed to use the 2.%% chromium-1% molybdenum steel in the quenched and tempered (as opposed to the normalized and stress-relieved) condition, thereby increasing tensile strength; however, the steel would have a bainitic structure, a structure known to be particularly susceptible to temper embrittlement.
Further, as a consequence of hydrogenation, a steel, irrespective of its structural constitution, must manifest the capability of resisting hot hydrogen attack. If a steel is unable to cope with hot hydrogen, it thus becomes subject to blistering or fissuring even though cladded with austenitic stainless. In this regard the interior surface of hydrocracker vessel walls are, for the most part, cladded with austenitic stainless. Because of the very substantial wall thickness of vessels now in use, this must be accomplished by the weld overlay procedure, a costly and undesirable technique since it must be performed after fabrication of the vessel. But with appropriate high strength steels and accompanying thinner walls, the advantages of standard roll cladding could be realized.
It has now been discovered that a combination of desired mechanical characteristics, including high strength at ambient and elevated temperatures, toughness, ductility, resistance to both hot hydrogen attack and temper embrittlement, high temperature stability, etc., can be attained with steels of low carbon content and containing nickel, aluminum, molybdenum, and, advantageously, columbium, as described more fully herein.
It is an object of the invention to provide new and improved steels having characteristics which render the steels suitable for use in the fabrication of hydrocracker vessels.
Other objects and advantages will become apparent from the following description.
Generally speaking and in accordance with the present invention, alloys contemplated herein contain (in percent by weight) carbon in an amount up to less than 0.04%, about 5% to 10% nickel, about 0.7% to 1.2% aluminum, from 0.5% to 2% molybdenum, up to 1.5% chromium, up to 1% manganese, up to 1% silicon, up to 0.12% columbium, and most advantageously from 0.008% to 0.08% columbium, the balance being essentially iron. Constituents such as nitrogen, oxygen, sulfur and phosphorus should be maintained 'at low levels consistent with good commercial steelmaking practice. However, other elements may be present as follows: up to 5% cobalt, up to 1% or 2% copper, up to 0.01%, e.g., up to 0.005% boron, and up to 0.2% tantalum. Tungsten can be used in lieu of molybdenum on an atom for atom basis, two parts of tungsten for one part of molybdenum; however, molybdenum is appreciably more elfective than tungsten and is much preferred. Elements such as vanadium and titanium are quite unnecessary, although up to 0.2% of each can be tolerated. High amounts thereof detract from toughness.
In carrying the invention into practice, the carbon content of the steels should be less than 0.04% and it is beneficial that it not exceed 0.03%; otherwise, the risk is increased that nascent hydrogen evolved during the hydrocracking operation (and which permeates a stainless cladding) will combine or react with carbon present in the form of iron carbides. This reaction establishes the environment for methane gas to form at grain boundaries and other discontinuities. Eventually suflicient pressure may be built up from the trapped gas to cause fissuring or cracking. But as will be shown herein, relatively low carbon per se is not necessarily a complete penacea since other low carbon steels have been tested with resulting failure.
Nickel is required to confer adequate hardenability. Suitable nickel ranges are from 5% to 7% and, for optimum hardenability, 8% to 9.5%. Aluminum is a potent hardening and strengthening constituent, but excessive amounts thereof, e.g., 1.5%, should be avoided if the ability of the steels to absorb impact energy is not to be drastically impaired. Molybdenum confers strength and resistance to temper embrittlement and a particularly satisfactory range thereof is from 0.75% to 1.5%. Columbium, it has been found, imparts strength without adversely affecting toughness, provided that amounts appreciably above 0.12% are avoided. Too, it is deemed that columbium is effective in resisting fissuring, i.e., it is capable of combining with carbon to form carbides which are less readily attacked by hydrogen.
For the purpose of giving those skilled in the art a better understanding of the invention, the following description and illustrative data are given:
A series of alloys were prepared by either vacuum The compositions of the alloys are given in Table I, the age hardening Alloys 1. through 5 being within the invention whereas Alloys A, B and C are outside the scope thereof (Alloy A conforms to the aforementioned hydrocracker 2%% Cr1% Mo steel). In Table 11 room temperature (R.T.) and elevated temperature properties are reported. The Yield ,Strength (Y .S.) at 0.2% offset and Ultimate Tensile Strength (U.T.S.) are given in pounds per square inch (P.S.I.), the Elongation (EL) and Reduction in Area (R.A.) values in percent and the Charpy V-notch impact toughness (C.V.N.) determinations in foot-pounds (ft.-lbs.).
TABLE I Al, O Other, Fe percent percent percent percent percent percent 1. 02 11.9.. n.a. Bal. 0. 96 0. 008 n.a. Bel 1. 08 0. 008 11.9.. Bal. 1. 07 0. 06 0. 09 Bel. 1. 0. 08 0. 54 Bel. 0.54 Bal. 0. 03 0.38 Bal 0. 02 n.a. 0. 76 Bel.
n.a.=not added. =air melted. =added for deoxidation purposes. Bal.=ba1ance plus inpurities.
TABLE II Test Alloy Temp, Y.S U.T.S., EL, R. C.V.N. Number F. 11.5.! p.s.i. percent percent !t.-lbs.
R.T. 98, 800 111, 600 21 80 184 1 RT. 149, 900 154, 900 21 71 10. 800 105, 200 114, 300 22 75 R.T. 98, 100 113, 500 19 82. 5 181 2 R.T. 150, 500 155, 500 19. 5 70.8 17 800 107,800 115,000 23 75 A RT. 100, 000 124, 200 82. 5 224 3 R.T. 153, 400 167, 600 19 68. 5 47 B 800 114,700 129,700 20 75.0 C 800 125, 000 136, 700 20 71. 5 RIP. 140, 100 143, 500 21 76 116 4 B 650 113,100 118, 100 21 75 B 850 91, 200 101, 000 25 80. 8 RT. 160, 100 199, 200 16. 5 59. 5 5 D 650 145,900 179,000 18.5 65.0 D 850 132, 400 162, 200 17. 0 59. 8 Q & T RT. 108, 400 134, 000 18 63. 8 16 A Q & T 650 99, 600 149, 200 17 47. 2
Q, & T 850 88, 000 134, 600 19 49. 0 E RT. 82, 600 100, 100 27 72. 2 SO. 3 B E 650 67,200 ,200 23.5 59.5
E 850 54, 800 67, 500 23. 5 49. 0 F RT. 121, 950 136, 950 19. 5 68. 8 79. 0 C F 650 102, 000 116,200 17. 5 60. 0
Q & T=Quenched and Tempered.
induction or air melting processing. Ingots were forged and thereafter hot rolled to A-inch rounds or %-inch square bars (Alloy 5, Table I in form of Vz-inch plate), which, prior to testing were then given one or more of the following heat treatments:
Heat Treatment A:
(1) Heat treated at 1600 F. for 1 hour, air cooled. Heat Treatment B:
(1) Heat treated at 1600 F. for 1 hour, air cooled. (2) Heated to 1000 F. and held for 2 hours followed by air cooling. Heat Treatment C:
(1) Same as B except steels water quenched after heating to 1600 F. Heat Treatment D:
(1) Heat treated at 1600 F. for 1 hour, then fan cooled to simulate cooling rate of a water quenched 4-inch thick plate.
(2) Heated to 950 F., held for 3 hours, air cooled.
Heat Treatment E:
(1) Aged 1 hour at 1050 F. Heat Treatment F:
(1) Same as D except heated to 1050 F., held for 4 hours and air cooled.
With regard to the data in Table II, the alloys within the invention manifested satisfactory room and elevated temperature mechanical properties, a tensile strength of nearly 200,000 p.s.i. and an impact strength of 30 ft.-lbs. (Alloy 5) at room temperautre and a strength of over 160,000 p.s.i. at 850 F. being deemed quite satisfactory. It should be explained the reason for the low impact energy levels of Alloys 1 and 2 (Heat Treatment B) at 7 room temperautre stems from fact these alloys were low 000 p.s.i. could be obtained; however, the Charpy V Notch impact strength was quite low, to wit, 6-7 ft.-lbs.
Alloys 5, B and C were also tested to ascertain their behavior regarding long term stability, temper embrittlement and resistance to hydrogen under pressure. The results of this more discriminate and informative testing are set forth in Table III.
TABLE III Y.S., U.T.S., EL, C.V.N., Alloy Condition p.s.i. p.s.i. percent percent ft.-lo.
5 Before Exposure 160, 100 199, 200 16.5 59. 5 30 After 500 hrs. at 750 F. 15 54. 25 After 5,000 hrs. at 750 F 16. 59. 8 22 After 500 hrs. at 850 F 169, 200 200, 000 14 50. 0 24. 5 After 500 1118. at 750 F. and
1,000 p.s.i.g. H2 168, 800 198, 300 54. 0 25 After 500 hrs. at 850 F. and
1,000 p.s.i.g. H 169, 200 200,000 14. 5 50.0 24. 5
B Before Exposure 82, 600 100,100 27 72. 5 80. 3 After 5,000 hrs. at 650 F 81, 800 98, 000 24 72 48 After 5,000 hrs. at 850 F 85, 300 100, 000 25 69. 5 33 After 1,000 hrs. at 850 F. and
1,000 p.s.i.g. Hz 66, 300 76, 800 7 7 1 C Before Exposure 121, 950 136, 950 19. 5 68. 8 79. 0 After 5,000 hrs. at 750 F- 142, 750 155,750 18. 5 66. 0 22 After 5,000 hrs. at 850 F 131, 200 145, 000 16.5 57. 8 3
Whereas Alloy 5 behaved quite well, Table III, Alloys B and C performed poorly. Low carbon Alloy B manifested susceptibility to temper embrittlement and also was exceedingly prone to hydrogen attack. Examination revealed severe grain boundary attack. Similarly, Alloy C lost virtually all ability to absorb impact after prolonged exposure to 850 F.
A further compositional range suitable for hydrocracker applications is as follows: carbon up to 0.03%, 5% to 9.5% nickel, 0.75% to 1.2% aluminum, 0.75% to 1.5% molybdenum, 0.008% to 0.08% or 0.1% columbium, up to 1% chromium, up to 0.75% manganese, up to 0.5% silicon, and the balance essentially iron. A particularly satisfactory steel consists essentially of about 0.02% carbon, about 9% nickel, about 1% aluminum, about 0.9% molybdenum, about 0.06% to 0.1% columbium, about 0.5 manganese, about 0.2% silicon, with the balance being iron.
Although the present invention is specifically addressed to hydrocrackers, the subject steels can otherwise be used in sundry environments, particularly applications where steels affording both relatively high strength and good toughness are required. The steels can be produced and used in the form of plate, bar, rod, forgings, etc.
Although the present invention has been described in conjunction with preferred embodiments, it is to be understood that modifications and variations may be resorted to without departing from the spirit and scope of the invention, as those skilled in the art will readily understand. Such modifications and variations are considered to be within the purview and scope of the invention and appended claims.
I claim:
1. A novel alloy steel adapted for use in fabricating a hydrocracker vessel therefrom, said steel consisting essentially of less than 0.04% carbon, about 5% to 10% nickel, about 0.7% to 1.2% aluminum, from 0.5% to 2% molybdenum, columbium present up to 0.12%, up to 1.5 chromium, up to 1% manganese, up to 1% silicon, up to 5% cobalt, up to 2% copper, up to 2% tungsten, and the balance essentially iron.
2. A steel in accordance with claim 1 containing at least 0.008% columbium.
3. A hydrocracker vessel formed from the steel of claim 1.
4. A hydrocracker vessel formed from the steel of claim 2.
5. A steel in accordance with claim 1 in which the nickel content is from 5% to 7%.
6. A steel in accordance with claim 1 in which the nickel content is from 81% to 9.5
7. A steel in accordance With claim 1 and consisting essentially of carbon up to about 0.03%, 5% to 9.5% nickel, about 0.75 to 1.2% aluminum, about 0.75% to 1.5% molybdenum, from 0.008% to 0.08% columbium, up to 1% chromium, up to 0.75 manganese, up to 0.5% silicon, and the balance essentially iron.
8. A hydrocracker vessel formed from the steel of claim 7.
9. A steel in accordance with claim 7 consisting essentially of about 0.02% carbon, 9% nickel, about 1% aluminum, about 0.9% molybdenum, about 0.06% to 0.1% columbium, about 0.5% manganese and about 0.2% silicon.
References Cited UNITED STATES PATENTS 3,284,191 11/1966 Hydrean -124 3,262,823 7/1966 Sadowski.
3,303,023 2/ 1967 Dulis.
3,368,887 2/1968 Clark 75-124 X HYLAND BIZOT, Primary Examiner US. Cl. X.R.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US58796366A | 1966-10-20 | 1966-10-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3475164A true US3475164A (en) | 1969-10-28 |
Family
ID=24351903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US587963A Expired - Lifetime US3475164A (en) | 1966-10-20 | 1966-10-20 | Steels for hydrocracker vessels containing aluminum,columbium,molybdenum and nickel |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3475164A (en) |
| AT (1) | AT273195B (en) |
| BE (1) | BE705433A (en) |
| DE (1) | DE1608181A1 (en) |
| ES (1) | ES346215A1 (en) |
| GB (1) | GB1134978A (en) |
| NL (1) | NL6714193A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3655366A (en) * | 1969-10-13 | 1972-04-11 | Int Nickel Co | Low alloy structural steel |
| US3899368A (en) * | 1973-12-13 | 1975-08-12 | Republic Steel Corp | Low alloy, high strength, age hardenable steel |
| US4146409A (en) * | 1977-06-06 | 1979-03-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Process for making a high toughness-high strength iron alloy |
| US4214902A (en) * | 1979-01-25 | 1980-07-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | High toughness-high strength iron alloy |
| US5032922A (en) * | 1990-07-02 | 1991-07-16 | Xerox Corporation | Platen accessory for portable copier |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1986004097A1 (en) * | 1985-01-14 | 1986-07-17 | Nisshin Steel Co., Ltd. | Highly corrosion-resistant steel alloy for use in exhaust gas member |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3262823A (en) * | 1963-06-07 | 1966-07-26 | Int Nickel Co | Maraging steel |
| US3284191A (en) * | 1966-02-09 | 1966-11-08 | Int Nickel Co | Nickel-aluminum alloy steel for production of gears, steel plate and the like |
| US3303023A (en) * | 1963-08-26 | 1967-02-07 | Crucible Steel Co America | Use of cold-formable austenitic stainless steel for valves for internal-combustion engines |
| US3368887A (en) * | 1965-08-17 | 1968-02-13 | Union Carbide Corp | Consumable wire for improving mechanical properties of weld metal |
-
1966
- 1966-10-20 US US587963A patent/US3475164A/en not_active Expired - Lifetime
-
1967
- 1967-10-05 GB GB45574/67A patent/GB1134978A/en not_active Expired
- 1967-10-19 AT AT943467A patent/AT273195B/en active
- 1967-10-19 ES ES346215A patent/ES346215A1/en not_active Expired
- 1967-10-19 NL NL6714193A patent/NL6714193A/xx unknown
- 1967-10-20 DE DE19671608181 patent/DE1608181A1/en active Pending
- 1967-10-20 BE BE705433D patent/BE705433A/xx unknown
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3262823A (en) * | 1963-06-07 | 1966-07-26 | Int Nickel Co | Maraging steel |
| US3303023A (en) * | 1963-08-26 | 1967-02-07 | Crucible Steel Co America | Use of cold-formable austenitic stainless steel for valves for internal-combustion engines |
| US3368887A (en) * | 1965-08-17 | 1968-02-13 | Union Carbide Corp | Consumable wire for improving mechanical properties of weld metal |
| US3284191A (en) * | 1966-02-09 | 1966-11-08 | Int Nickel Co | Nickel-aluminum alloy steel for production of gears, steel plate and the like |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3655366A (en) * | 1969-10-13 | 1972-04-11 | Int Nickel Co | Low alloy structural steel |
| US3899368A (en) * | 1973-12-13 | 1975-08-12 | Republic Steel Corp | Low alloy, high strength, age hardenable steel |
| US4146409A (en) * | 1977-06-06 | 1979-03-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Process for making a high toughness-high strength iron alloy |
| US4214902A (en) * | 1979-01-25 | 1980-07-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | High toughness-high strength iron alloy |
| US5032922A (en) * | 1990-07-02 | 1991-07-16 | Xerox Corporation | Platen accessory for portable copier |
Also Published As
| Publication number | Publication date |
|---|---|
| GB1134978A (en) | 1968-11-27 |
| NL6714193A (en) | 1968-04-22 |
| ES346215A1 (en) | 1968-12-01 |
| DE1608181A1 (en) | 1970-11-12 |
| BE705433A (en) | 1968-04-22 |
| AT273195B (en) | 1969-08-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3093519A (en) | Age-hardenable, martensitic iron-base alloys | |
| US5069870A (en) | High-strength high-cr steel with excellent toughness and oxidation resistance | |
| JP3514182B2 (en) | Low Cr ferritic heat resistant steel excellent in high temperature strength and toughness and method for producing the same | |
| JP3422561B2 (en) | Heat and creep resistant steel with martensitic structure obtained by heat treatment | |
| JP4369612B2 (en) | Steel plate for low quenching or normalizing type low alloy boiler steel pipe excellent in toughness, and method of manufacturing steel pipe using the same | |
| US3154412A (en) | Heat-resistant high-strength stainless steel | |
| AU2002252427B2 (en) | Duplex stainless steel | |
| US20090081068A1 (en) | Ultra-High Strength Stainless Steels | |
| EP0171868B1 (en) | Austenitic stainless steel for low temperature service | |
| US3658513A (en) | Precipitation-hardenable stainless steel | |
| EP0199046B1 (en) | High-strength heat-resisting ferritic steel pipe and tube | |
| US3355280A (en) | High strength, martensitic stainless steel | |
| US3262777A (en) | Ultra tough maraging steel | |
| US3453102A (en) | High strength,ductile maraging steel | |
| US3475164A (en) | Steels for hydrocracker vessels containing aluminum,columbium,molybdenum and nickel | |
| US3514284A (en) | Age hardenable nickel-iron alloy for cryogenic service | |
| US3266876A (en) | Ferrous weld deposit and structure | |
| US2225440A (en) | Austenitic alloy steel | |
| JP2000204434A (en) | Ferritic heat-resistant steel excellent in high-temperature strength and its manufacturing method | |
| US3132938A (en) | Aged steel | |
| US3336168A (en) | Weldable tough steel essentially composed of chromium and manganese and method of manufacturing the same | |
| JP3757462B2 (en) | High strength Cr-Mo-W steel | |
| JP3237137B2 (en) | High chromium ferritic heat-resistant steel with small decrease in strength of weld heat affected zone | |
| US5814274A (en) | Low-Cr ferritic steels and low-Cr ferritic cast steels having excellent high teperature strength and weldability | |
| US3396013A (en) | Beryllium-containing maraging steel |