US2883283A - Oxidation resistant molybdenum base alloy - Google Patents
Oxidation resistant molybdenum base alloy Download PDFInfo
- Publication number
- US2883283A US2883283A US669433A US66943357A US2883283A US 2883283 A US2883283 A US 2883283A US 669433 A US669433 A US 669433A US 66943357 A US66943357 A US 66943357A US 2883283 A US2883283 A US 2883283A
- Authority
- US
- United States
- Prior art keywords
- molybdenum
- oxidation
- base
- base alloy
- oxidation resistant
- 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
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 title claims description 38
- 229910052750 molybdenum Inorganic materials 0.000 title claims description 38
- 239000011733 molybdenum Substances 0.000 title claims description 38
- 230000003647 oxidation Effects 0.000 title claims description 25
- 238000007254 oxidation reaction Methods 0.000 title claims description 25
- 229910045601 alloy Inorganic materials 0.000 title claims description 19
- 239000000956 alloy Substances 0.000 title claims description 19
- 239000003381 stabilizer Substances 0.000 claims description 10
- 229910000476 molybdenum oxide Inorganic materials 0.000 claims description 6
- PQQKPALAQIIWST-UHFFFAOYSA-N oxomolybdenum Chemical compound [Mo]=O PQQKPALAQIIWST-UHFFFAOYSA-N 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 4
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 4
- 229910052790 beryllium Inorganic materials 0.000 claims description 4
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052791 calcium Inorganic materials 0.000 claims description 4
- 239000011575 calcium Substances 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 239000011651 chromium Substances 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 239000010703 silicon Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052720 vanadium Inorganic materials 0.000 claims description 4
- 229910052726 zirconium Inorganic materials 0.000 claims description 4
- 229910052684 Cerium Inorganic materials 0.000 claims description 3
- 229910052691 Erbium Inorganic materials 0.000 claims description 3
- 229910052779 Neodymium Inorganic materials 0.000 claims description 3
- -1 PRAESODYMIUM Substances 0.000 claims description 3
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 claims description 3
- 229910052746 lanthanum Inorganic materials 0.000 claims description 3
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 3
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims description 3
- 230000000979 retarding effect Effects 0.000 claims description 2
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims 1
- 239000000654 additive Substances 0.000 description 12
- 230000000996 additive effect Effects 0.000 description 8
- 230000015572 biosynthetic process Effects 0.000 description 7
- 238000009792 diffusion process Methods 0.000 description 7
- 230000004888 barrier function Effects 0.000 description 6
- 239000010953 base metal Substances 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 230000001590 oxidative effect Effects 0.000 description 4
- 238000000576 coating method Methods 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 230000001066 destructive effect Effects 0.000 description 3
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 2
- 238000005253 cladding Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000008188 pellet Substances 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910001182 Mo alloy Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000004320 controlled atmosphere Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000005382 thermal cycling Methods 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten 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
- C22C27/00—Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
- C22C27/04—Alloys based on tungsten or molybdenum
Definitions
- This invention relates to molybdenum base alloys having a. high resistance to. oxidation at temperatures up. to 2500 F. even after prolonged or intermittent. exposure to oxidizing atmospheres at such temperatures and to a method wherebymolybdenum is protected from destructive oxidation.
- alloys of molybdenum with at least one element from the group of elements which function as oxidation retarders or stabilizers and which consists of beryllium, titanium, aluminum, zirconium, chromium, silicon and vanadium in amounts up to about 6% by weight and at least one of a second group of elements which functions as a diffusion barrier and which may be present in amounts from an effective percentage up to about 1.0% and selected from the group consisting of calcium, cerium, erbium, lanthanum, neodymium, praesodymium, lead, or tin.
- Molybdenum and molybdenum base alloys possess high temperature strength properties which make these metals desirable for many end uses. Unfortunately it has been found that these desirable properties are accompanied by poor oxidation resistance. When pure molybdenum or many molybdenum base alloys are exposed to oxidation at high temperatures, coatings form on the surface ranging from possibly MoO to and including M00 At about 1200 F., M00 volatilizes and continually exposes fresh metal to the oxidative conditions so that the destruction of the base metal as the result of oxidation tends to become catastrophic.
- One object of this invention is to provide a means for protecting molybdenum and molybdenum base alloys against oxidation at elevated temperatures and particularly against oxidation in environments in which the protective member is subject to repeated heating and cooling and to bending stresses.
- Another object of the present invention is to provide a technique for selecting alloy compositions which will result in members possessing a combination of inherent properties which prevent the destructive oxidation of the molybdenum base material.
- the first additive characterized by me as a stabilizer or retarder must be selected from elements having atomic volumes or radii less than the atomic volume or radius of molybdenum, so that ions or atoms of the additive will diffuse as fast as the base metal. Furthermore, the heats of formation of the oxides of the additives should be preferably greater than the heat of formation of the molybdenum oxide which forms when the base metal is exposed to oxidation.
- the second additive characterized by me as a' diffusion barrier, must be selected from elements whose atomic volumes are greater than the molecular volume of the oxide which first appears on the surface of the molybdenum base article when it is exposed to oxidation. Furthermore, this additive should be selected from elements whose oxides have high heats of formation'relative tothe heat of formation of molybdenum oxide and whose oxides are refractory in nature and are capable of forming compounds with the first oxide which appears on the surface to be protected. The resulting compounds must themselves be refractory in nature for the proper protection to be achieved.
- the additive atoms which are present in the molybdenum oxide lattice maintain the structure and composition of the molybdenum suboxide and thus avoid the continued destructive oxidation characteristic of untreated base material.
- the higher heat of formation of these oxides relative to the heat of formation of the molybdenum oxide is additionally responsible for maintaining the stability of the molybdenum suboxide film.
- Suitable stabilizers may consist of one or more of the following: beryllium, titanium, aluminum, zirconium, chromium, silicon and vanadium.
- Each of the recited elements is capable of reducing higher oxides of molybdenum not only to the monoxide but also to the metal and each of the stabilizers listed may be added from effective amounts up to about 6% by weight of a total of the listed elements.
- the second additive is selected from those elements having atomic volumes greater than the molecular volume of molybdenum suboxide, and as a result it blocks any composition may be prepared by melting the molybdenum or molybdenum base alloy in a suitable furnace under a controlled atmosphere to avoid oxidation or contamination of the melt and adding thereto a desired retarder or stabilizer in effective amounts up to 6% by weight and the desired amount of diffusion barrier element in amounts up to 1.0% by weight.
- a second method of applying this technique is to coat the molybdenum or molybdenum base article after it has been formed with a mixture of powder in a suitable vehicle compounded so as to contain the proper proportions of retarder and difiusion barrier additives.
- the desired alloys may be prepared as follows:
- the coarsely granular metals (approximately 20 to 40 mesh) are mixed in suitable proportions and compressed into pellets. These pellets are then fused twice in an arc furnace operating in an argon atmosphere at approximately half atmospheric pressure.
- the arc furnace consists of a water-cooled copper hearth and a water-cooled tungsten tip. The double melting is utilized to insure uniformity.
- the buttons obtained are rolled into sheet and the edges of the sheet cropped.
- the analyses given in the table below are those obtained on the finished alloy.
- the oxidation resistance is determined qualitatively by examination of specimens after a 3-hour exposure in air at 2000 F. and 2500 F.
- Suitable alloys for the purpose and an indication of their oxidation resistance are given m the following table.
- An oxidation resistant molybdenum base alloy consisting of between about 0.5% and 6% by weight of at least one element retarding the oxidation of molybdenum and selected from the group consisting of beryllium, titanium, aluminum, zirconium, chromium, silicon, and vanadium, and between about 0.1% and 1.0% by weight of at least one molybdenum oxide stabilizer from the group consisting of calcium, cerium, erbium, lanthanum, neodymium, praesodymium, lead and tin, balance essentially all molybdenum.
- An oxidation resistant molybdenum base alloy consisting of between about 0.5% and 6% by weight of aluminum, between about 0.1% and 1.0% of calcium, balance essentially all molybdenum.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Description
United States Patent Eugene Waiuer, Cleveland; Heights, Ohio, assignor to Horizons Incorporated, a corporation of N ew Jersey No Drawing. Application July 2, 1957 Serial No. 669,433
2. Claims. (Cl. 75-176).
This invention relates to molybdenum base alloys having a. high resistance to. oxidation at temperatures up. to 2500 F. even after prolonged or intermittent. exposure to oxidizing atmospheres at such temperatures and to a method wherebymolybdenum is protected from destructive oxidation.
More particularly, it relates to alloys of molybdenum with at least one element. from the group of elements which function as oxidation retarders or stabilizers and which consists of beryllium, titanium, aluminum, zirconium, chromium, silicon and vanadium in amounts up to about 6% by weight and at least one of a second group of elements which functions as a diffusion barrier and which may be present in amounts from an effective percentage up to about 1.0% and selected from the group consisting of calcium, cerium, erbium, lanthanum, neodymium, praesodymium, lead, or tin.
Molybdenum and molybdenum base alloys possess high temperature strength properties which make these metals desirable for many end uses. Unfortunately it has been found that these desirable properties are accompanied by poor oxidation resistance. When pure molybdenum or many molybdenum base alloys are exposed to oxidation at high temperatures, coatings form on the surface ranging from possibly MoO to and including M00 At about 1200 F., M00 volatilizes and continually exposes fresh metal to the oxidative conditions so that the destruction of the base metal as the result of oxidation tends to become catastrophic.
One previously proposed means for overcoming this poor oxidation resistance has been to clad the molybdenum or molybdenumv base alloy article with a suitable oxidation resistant alloy. This approach has not been entirely successful because diffusion between the cladding material and the molybdenum base has often produced brittle interfaces which did not withstand repeated thermal cycling and which in many instances ultimately failed by actual physical separation of the clad from the base.
Still another disadvantage in the prior efforts to clad molybdenum and molybdenum base materials has been inherent in the brittleness of the cladding materials themselves. This has seriously limited the use of such coatings in applications where the article to be protected is subject to bending stresses.
One object of this invention is to provide a means for protecting molybdenum and molybdenum base alloys against oxidation at elevated temperatures and particularly against oxidation in environments in which the protective member is subject to repeated heating and cooling and to bending stresses.
Another object of the present invention is to provide a technique for selecting alloy compositions which will result in members possessing a combination of inherent properties which prevent the destructive oxidation of the molybdenum base material.
In order to develop a system applicable to the protection of molybdenum and molybdenum base alloys, it has been found that a double barrier must be provided to accomplish the required properties; Two distinct functions must be performed by the alloying elements added to the base whether applied as coating material or incorporated into the base as an alloying addition.- The first of these functions is to retard'or stabilize the oxidatron and the second is to bar diffusion. The two additives may be described in terms of their chemical andphysical properties relative to molybdenum and its compounds.
The first additive characterized by me as a stabilizer or retarder must be selected from elements having atomic volumes or radii less than the atomic volume or radius of molybdenum, so that ions or atoms of the additive will diffuse as fast as the base metal. Furthermore, the heats of formation of the oxides of the additives should be preferably greater than the heat of formation of the molybdenum oxide which forms when the base metal is exposed to oxidation.
The second additive, characterized by me as a' diffusion barrier, must be selected from elements whose atomic volumes are greater than the molecular volume of the oxide which first appears on the surface of the molybdenum base article when it is exposed to oxidation. Furthermore, this additive should be selected from elements whose oxides have high heats of formation'relative tothe heat of formation of molybdenum oxide and whose oxides are refractory in nature and are capable of forming compounds with the first oxide which appears on the surface to be protected. The resulting compounds must themselves be refractory in nature for the proper protection to be achieved.
When an alloy has been prepared with suitable content of an element or elementsfrom the'firstabove described group and the second above described group, the following process takes place as soon as the resulting alloy is heated in an oxidizing atmosphere. First, an oxide will appear on the surface of the article and, in molybdenumrich systems such as those presently contemplated in which the molybdenum content comprises substantially at least by weight of the alloy, this oxide is apparently a suboxide of molybdenum. On continued heating the atoms of the stabilizer or retarder additive or additives diifuse rapidly through the superficial film of molybdenum suboxide to the outside and thereupon form an oxide as a result of contact with the oxygen or oxidizing environment. In addition to protecting the base metal from further oxidation by the formation of this oxide, the additive atoms which are present in the molybdenum oxide lattice maintain the structure and composition of the molybdenum suboxide and thus avoid the continued destructive oxidation characteristic of untreated base material. In this connection the higher heat of formation of these oxides relative to the heat of formation of the molybdenum oxide is additionally responsible for maintaining the stability of the molybdenum suboxide film.
Suitable stabilizers, as has been previously indicated, may consist of one or more of the following: beryllium, titanium, aluminum, zirconium, chromium, silicon and vanadium.
Each of the recited elements is capable of reducing higher oxides of molybdenum not only to the monoxide but also to the metal and each of the stabilizers listed may be added from effective amounts up to about 6% by weight of a total of the listed elements.
As a result of diffusion of both molybdenum and stabilizer atoms from the surface of the base metal into the oxide layer, a substantial increase of concentration of atoms of the second additive, above described by me as the diffusion barrier, is available just at the surface on the base metal under the oxide layer.
The second additive is selected from those elements having atomic volumes greater than the molecular volume of molybdenum suboxide, and as a result it blocks any composition may be prepared by melting the molybdenum or molybdenum base alloy in a suitable furnace under a controlled atmosphere to avoid oxidation or contamination of the melt and adding thereto a desired retarder or stabilizer in effective amounts up to 6% by weight and the desired amount of diffusion barrier element in amounts up to 1.0% by weight.
A second method of applying this technique is to coat the molybdenum or molybdenum base article after it has been formed with a mixture of powder in a suitable vehicle compounded so as to contain the proper proportions of retarder and difiusion barrier additives.
When the first method is employed, the desired alloys may be prepared as follows:
The coarsely granular metals (approximately 20 to 40 mesh) are mixed in suitable proportions and compressed into pellets. These pellets are then fused twice in an arc furnace operating in an argon atmosphere at approximately half atmospheric pressure. The arc furnace consists of a water-cooled copper hearth and a water-cooled tungsten tip. The double melting is utilized to insure uniformity. The buttons obtained are rolled into sheet and the edges of the sheet cropped. The analyses given in the table below are those obtained on the finished alloy. The oxidation resistance is determined qualitatively by examination of specimens after a 3-hour exposure in air at 2000 F. and 2500 F.
Suitable alloys for the purpose and an indication of their oxidation resistance are given m the following table.
Wt. Wt. Wt. Oxidation Resistance Percent Percent Percent Retarder Stabilizer Mo 0 0 100.0 Nil Nil.
. 6.0 Si 0 95. 0 Fair Poor.
4.70 Si.--" 0.77 La 94. 5 Excellent- Good. 5.01 AL-" 0.66 Ce- 94.3 ..do..... Do. 5.21 Cr". 0.95 08.... 93.0 do Do. 3.98 AL... 0.96 Ga... 95. 0 ..do Excellent. 4.52Z 0.86 SIL... 94.6 .do Fair.
Having now described my invention in accordance with the patent statutes, I claim:
1. An oxidation resistant molybdenum base alloy consisting of between about 0.5% and 6% by weight of at least one element retarding the oxidation of molybdenum and selected from the group consisting of beryllium, titanium, aluminum, zirconium, chromium, silicon, and vanadium, and between about 0.1% and 1.0% by weight of at least one molybdenum oxide stabilizer from the group consisting of calcium, cerium, erbium, lanthanum, neodymium, praesodymium, lead and tin, balance essentially all molybdenum.
2. An oxidation resistant molybdenum base alloy consisting of between about 0.5% and 6% by weight of aluminum, between about 0.1% and 1.0% of calcium, balance essentially all molybdenum.
References Cited in the file of this patent UNITED STATES PATENTS 2,678,268 Ham May 11, 1954 2,678,269 Ham May 11, 1954 2,678,270 Ham May 11, 1954 2,678,271 Ham May 11, 1954 2,678,272 Ham May 11, 1954
Claims (1)
1. AN OXIDATION RESISTANT MOLYBDENUM BASE ALLOY CONSISTING OF BETWEEN ABOUT 0.5% AND 6% BY WEIGHT OF AT LEAST ONE ELEMENT RETARDING THE OXIDATION OF MOLYBDENUM AND SELECTED FROM THE GROUP CONSISTING OF BERYLLIUM, TITANIUM, ALUMINUM, ZIRCONIUM, CHROMIUM, SILICON, AND VANADIUM, AND BETWEEN ABOUT 0.1% AND 1.0% BY WEIGHT OF AT LEAST ONE MOLYBDENUM OXIDE STABILIZER FROM THE GROUP CONSISTING OF CALCIUM, CERIUM, ERBIUM, LANTHANUM, NEODYMIUM, PRAESODYMIUM, LEAD AND TIN, BALANCE ESSENTIALLY ALL MOLYBDENUM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US669433A US2883283A (en) | 1957-07-02 | 1957-07-02 | Oxidation resistant molybdenum base alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US669433A US2883283A (en) | 1957-07-02 | 1957-07-02 | Oxidation resistant molybdenum base alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2883283A true US2883283A (en) | 1959-04-21 |
Family
ID=24686308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US669433A Expired - Lifetime US2883283A (en) | 1957-07-02 | 1957-07-02 | Oxidation resistant molybdenum base alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2883283A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3030206A (en) * | 1959-02-17 | 1962-04-17 | Gen Motors Corp | High temperature chromiummolybdenum alloy |
| US3061482A (en) * | 1959-09-16 | 1962-10-30 | Nicholas J Grant | Ceramic coated metal bodies |
| US3174852A (en) * | 1959-04-14 | 1965-03-23 | Gen Motors Corp | High temperature chromium-tungstenmolybdenum alloy |
| US4370299A (en) * | 1980-07-08 | 1983-01-25 | Tokyo Shibaura Denki Kabushiki Kaisha | Molybdenum-based alloy |
| US11306375B2 (en) * | 2019-02-26 | 2022-04-19 | Deutschland Gmbh & Co. Kg | Molded article made of a molybdenum-aluminum-titanium alloy |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2678272A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-columbium alloys |
| US2678268A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-vanadium alloys |
| US2678269A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-titanium alloys |
| US2678270A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-tantalum alloys |
| US2678271A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-zirconium alloys |
-
1957
- 1957-07-02 US US669433A patent/US2883283A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2678272A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-columbium alloys |
| US2678268A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-vanadium alloys |
| US2678269A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-titanium alloys |
| US2678270A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-tantalum alloys |
| US2678271A (en) * | 1951-10-06 | 1954-05-11 | Climax Molybdenum Co | Molybdenum-zirconium alloys |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3030206A (en) * | 1959-02-17 | 1962-04-17 | Gen Motors Corp | High temperature chromiummolybdenum alloy |
| US3174852A (en) * | 1959-04-14 | 1965-03-23 | Gen Motors Corp | High temperature chromium-tungstenmolybdenum alloy |
| US3061482A (en) * | 1959-09-16 | 1962-10-30 | Nicholas J Grant | Ceramic coated metal bodies |
| US4370299A (en) * | 1980-07-08 | 1983-01-25 | Tokyo Shibaura Denki Kabushiki Kaisha | Molybdenum-based alloy |
| US11306375B2 (en) * | 2019-02-26 | 2022-04-19 | Deutschland Gmbh & Co. Kg | Molded article made of a molybdenum-aluminum-titanium alloy |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2883282A (en) | Protection of niobium from oxidation | |
| US3479161A (en) | Oxidation resistant tungsten and molybdenum alloy bodies | |
| US2883283A (en) | Oxidation resistant molybdenum base alloy | |
| EP0227471B1 (en) | Sintered silicon nitride ceramic article | |
| US3028236A (en) | Columbium base alloy | |
| US3383235A (en) | Silicide-coated composites and method of making them | |
| US4762557A (en) | Refractory metal alloys having inherent high temperature oxidation protection | |
| US3156560A (en) | Ductile niobium and tantalum alloys | |
| US3295346A (en) | Methods for the elevated temperature protection of metallic surface, and coatings therefor | |
| KR100683548B1 (en) | Electrical heat-resistant components | |
| US2885313A (en) | Process of treating magnesium-bearing aluminum base alloys with fluoroborate | |
| US3055088A (en) | Composite metal body for high temperature use | |
| US3166414A (en) | Tantalum base alloys | |
| US5683524A (en) | High temperature melting molybdenum-chromium-silicon alloys | |
| JPS62142736A (en) | Zn alloy for hot dipping having high corrosion resistance, high workability, and high heat resistance | |
| US3595644A (en) | Hafnium base alloy (cr-ai) | |
| US3622308A (en) | Hafnium base alloy (iridium) | |
| US3037858A (en) | Columbium base alloy | |
| US3104972A (en) | Zirconium-base brazing alloys | |
| US3188206A (en) | Columbium alloy | |
| US3168380A (en) | Columbium base alloys | |
| US3574572A (en) | Coatings for high-temperature alloys | |
| US3622309A (en) | Hafnium base alloy (boron) | |
| US3175279A (en) | Ductile chromium composition | |
| US3236638A (en) | Columbium-base alloy of improved fabricability |