US2578197A - Thermostatic device - Google Patents
Thermostatic device Download PDFInfo
- Publication number
- US2578197A US2578197A US661082A US66108246A US2578197A US 2578197 A US2578197 A US 2578197A US 661082 A US661082 A US 661082A US 66108246 A US66108246 A US 66108246A US 2578197 A US2578197 A US 2578197A
- Authority
- US
- United States
- Prior art keywords
- age
- nickel
- nitrided
- hardened
- iron
- 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
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 71
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 66
- 229910045601 alloy Inorganic materials 0.000 description 53
- 239000000956 alloy Substances 0.000 description 53
- 239000000203 mixture Substances 0.000 description 36
- 229910052759 nickel Inorganic materials 0.000 description 36
- 229910052742 iron Inorganic materials 0.000 description 32
- 239000011651 chromium Substances 0.000 description 20
- 239000010936 titanium Substances 0.000 description 20
- 229910052719 titanium Inorganic materials 0.000 description 20
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 19
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 19
- 229910052804 chromium Inorganic materials 0.000 description 19
- 229910052751 metal Inorganic materials 0.000 description 17
- 239000002184 metal Substances 0.000 description 16
- 229910052782 aluminium Inorganic materials 0.000 description 15
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 15
- 229910052710 silicon Inorganic materials 0.000 description 9
- 239000010703 silicon Substances 0.000 description 9
- 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 8
- 238000005121 nitriding Methods 0.000 description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 7
- 238000003483 aging Methods 0.000 description 7
- 229910052802 copper Inorganic materials 0.000 description 7
- 239000010949 copper Substances 0.000 description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 239000002131 composite material Substances 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- 229910000881 Cu alloy Inorganic materials 0.000 description 2
- 229910000570 Cupronickel Inorganic materials 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- YOCUPQPZWBBYIX-UHFFFAOYSA-N copper nickel Chemical compound [Ni].[Cu] YOCUPQPZWBBYIX-UHFFFAOYSA-N 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- -1 maganese Chemical compound 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 229910021652 non-ferrous alloy Inorganic materials 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 238000005480 shot peening Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 101100138673 Arabidopsis thaliana NPF3.1 gene Proteins 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910000914 Mn alloy Inorganic materials 0.000 description 1
- 229910000792 Monel Inorganic materials 0.000 description 1
- 241000208225 Rhus Species 0.000 description 1
- 235000014220 Rhus chinensis Nutrition 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- UTICYDQJEHVLJZ-UHFFFAOYSA-N copper manganese nickel Chemical compound [Mn].[Ni].[Cu] UTICYDQJEHVLJZ-UHFFFAOYSA-N 0.000 description 1
- 238000010494 dissociation reaction Methods 0.000 description 1
- 230000005593 dissociations Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- OTTJBKQXLHGKAI-UHFFFAOYSA-N iron nickel titanium Chemical compound [Ti][Fe][Ni][Ti] OTTJBKQXLHGKAI-UHFFFAOYSA-N 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K5/00—Measuring temperature based on the expansion or contraction of a material
- G01K5/48—Measuring temperature based on the expansion or contraction of a material the material being a solid
- G01K5/56—Measuring temperature based on the expansion or contraction of a material the material being a solid constrained so that expansion or contraction causes a deformation of the solid
- G01K5/62—Measuring temperature based on the expansion or contraction of a material the material being a solid constrained so that expansion or contraction causes a deformation of the solid the solid body being formed of compounded strips or plates, e.g. bimetallic strip
- G01K5/64—Details of the compounds system
- G01K5/66—Selection of composition of the components of the system
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H37/00—Thermally-actuated switches
- H01H37/02—Details
- H01H37/32—Thermally-sensitive members
- H01H37/52—Thermally-sensitive members actuated due to deflection of bimetallic element
- H01H2037/526—Materials for bimetals
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/936—Chemical deposition, e.g. electroless plating
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9335—Product by special process
- Y10S428/939—Molten or fused coating
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/125—Deflectable by temperature change [e.g., thermostat element]
- Y10T428/12521—Both components Fe-based with more than 10% Ni
Definitions
- the present invention relates to a composite metal temperature responsive device and more particularly to a thermostatic element to be used in a thermostat.
- the present invention provides a thermostatic element comprising a plurality of metallic members of dissimilar coeflicients of thermal expansion secured together in faceto-face relationship by rivets, spot welds, diffusion bonding, or other known manner, and adapted to act as a unitary element, at least one of said members being made of an agehardened alloy which is also nitrided throughout the cross section of the member.
- agehardened is meant that the member is in a hardened condition resulting from a solution treatment at high temperatures followed by a treatment at lower temperatures, the latter treatment producing the hardening eifect.
- agehardening is generally obtained by heating the alloy to a high temperature to place the precipitable phase in a solid solution, followed by rapid cooling to preserve the solid solution and treatment of the alloy at lower agin temperatures to precipitate the precipitable phase in a critical finely dispersed state to cause hardening.
- nitrided throughout the cross section is meant that the member contains nitrogen diffused throughout the cross section of the memher.
- the invention is not limited to the agehardening and nitriding of only one member 1946, Serial No. 661,082 Canada March 15, 1946 More than one member can be age-hardened and nitrided.
- thermostatic element consists of two members, both can be agehardened and nitrided throughout their cross sections.
- the thermostatic element consists of three or more members, more than one member can be age-hardened and nitrided throughout the cross section.
- thermostatic element made of at least one age-hardened and nitrided member has a high equivalent yield strength.
- the equivalent yield strengt is considered by many in the art to be a very important property which gives a good indication of the load-carrying capacity which will evaluate service life.
- the equivalent yield strength is the stress which will give a composite metal thermostatic element a permanent set when the stress is removed.
- the degree of permanent set is considered by many in the art to be the Proof Stress set, e. g. 0.01% permanent elongation.
- The. art has employed severe cold working or cold deformation to raise the equivalent yield strength.
- the age-hardened and nitrided members provided by the present invention have a higher equivalent yield strength than has been obtainable heretofore by cold working.
- the age-hardened and nitrided members also have greater strength, better flexing properties and longer life, by reason of improved fatigue resistance.
- the invention provides thinner thermostatic members, such as striplike members, than has been available heretofore.
- the smaller cross sectional dimension of the age-hardened and nitrided member not exceed about 0.03 inch.
- the sum total of the elements present which do not impart nitridability e. g.-nickel, copper, chromium, molybdenum, tungsten, should not exceed approximately of the whole composition.
- iron imparts nitridability to the member and is preferably present in the comthe case of copper-base alloys, manganese,
- the member to be age-hardened and nitrided is made of an alloy containing approximately 2% to 80% of one or more of those metallic elements which do not impart nltridability, e. g. nickel, copper, chromium, molybdenum, tungsten; approximately 20% to 97% of these ele- 'ments which are nitriding promoters, e. g.
- age-hardening element e. g.-titanium, aluminum, silicon, beryllium, and magnesium, and i: an amount sufilcient to impart age-hardenability and nitridability to the alloy.
- This invention particularly contemplates agehardened and nitrided members made of an ironnickel-titanium or an iron-nickel-chromiumtitani m alloy containing about 1% to 10% titaniup to about 25% chromium, about 2% to 80% nickel, the balance being substantially iron in an amount constituting at least 10% of the alloy, the sum of the nickel plus any chromium that may be present not exceeding approximately 80% of the whole composition, and the sum of the iron plus nickel contents being at least approximately 70% of the whole composition.
- An example of different types of alloys which also may be empolyed in accordance with this invention as an age-hardened and nitrided member of the thermostatic element are the copper-nickel-manganese alloys, e. g.-60% copper, 20% nickel, and 20% manganese, such as are disclosed in the Dean, United States patent, No. 2,234,552.
- Alloy compositions A, B, and C in the axehardened and nitrided condition are particularly suitable as the low-expansion member of the thermostatic element, for example,'members L4 and L-2 in the drawing.
- Alloy composition E when age-hardened and nitrided throughout the cross section can be used/ either as the low-expansion member or the high-expansion member.
- any of the latter is the low-expansion member
- the member of composition E is the high-expansion member.
- the composition E member is the low-expansion member.
- both the low-expansion and the high-expansion member can be in the ace-hard- .ened and nitrided condition, or only one member need be in such a condition.
- ber could be in an age-hardened and nitrided condition while the other is ina non-nitrided but age-hardened condition. It is preferred that both members be in an age-hardened and nitrided condition provided the expansion and other required properties will so permit.
- the other member when only one member is made of an agehardened and nitrided alloy, such as compositions A to E, the other member can be a non-nitridable material, such as non-ferrous alloys.
- suitable non-ferrous alloys include cupro-nickel, e. g., an alloy containing about 30% to 45% nickel and about 55% to 70% copp r, and nickel-copper alloys sold under the trade-mark of "Monel" and containing about two-thirds nickel and one-third 33% copper and about 63% to 73% nickel.
- the non-nitrided member can be made of such an age-hardenable alloy composition.
- that member is the high-expansion member when the other member is made of an age-hardened and nitrided alloy of compositions A, B, C, or E, and is the low-expansion member when the other member is made of an age-hardened nitrided alloy of composition D.
- compositions suitable for use in strip-like or ribbon-like form as the age-hardened 'and nitrided members in the thermostatic elements, and temperature responsive devices comprised thereof, contemplated by the invention include the following:
- compositions I to V are illustrative of alloys within the ranges of compositions A to E. respectively, and are all age-hardenable and nitridable.
- Age-hardening can be obtainodin all the compositions by treatment for at least twenty minutes, e. g., one-half to one and one-half hours. within the solution temperature range of about 1700" F. to 1850 F., followed by cooling the alloy to preserve the solid solution of the precipitable by a rapid cooling such as copper, e. g., about 26% to quenching, and thereafter treating the compositions within the aging temperature range of about 1100 F. to 1350 F. to impart age-hardness, e. g., treating within said range for about three to forty-eight hours.
- compositions can all be nitrided by treating them in an atmosphere of dissociated ammonia, e. g., about 24% to 40% dissociation, at nitriding temperatures between about 900 F. and 1200 F. for sufficient time to nitride the member throughout its cross section. Because the nitriding temperatures overlap the aging temperatures, it is possible to age-harden and nitride the member simultaneously, e. g., at temperatures of about 1100 F. to 1200 F. In other words, after treatment to simultaneously in an age-hardened and nitrided condition throughout its cross section.
- dissociated ammonia e. g., about 24% to 40% dissociation
- the age-hardened and nitrided member can advantageously be subjected to an additional shot-peening treatment to improve further the strength and performance of the thermostatic element.
- the shot-peening treatment can be accomplished by the usual methods, and its effect is superimposed on those derived from the agehardening and nitriding treatment whereby new and improved characteristics are obtained in thermostatic elements.
- a bimetallic thermostatic element comprising a low-expansion member made of an iron-nickel alloy containing about 40.5% to 53% nickel, about 2.2% to 2.8% titanium, about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese,a small amount up to about 6.5 chromium, a small amount up to about 0.1% carbon and the balance substantially iron, and a high expansion member made of an iron-nickel alloy containing about 28% to 30% nickel, about 2.2%
- titanium about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, about 8% to 9% chromium, up to about 0.1% carbon and the balance substantially iron, said low-expansion member and said highexpansion member both being in an age-hardened and nitrided condition throughout the cross sections of said members.
- a bimetallic thermostat the improvement which comprises making the low-expansion member of said thermostat of an alloy containing about 40.5% to 53% nickel, about 2.2% to 2.8% i a um. about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, a small amount up to about 6.5% chromium, a small amount up to about 0.1% carbon and the balance substantially iron; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- a bimetallic thermostat the improvement which comprises making the high-expansion member of said thermostat or an alloy containing about 28% to 30% nickel, about 2.2% to 2.8% titanium, about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, about 8% to 9% chromium, a small amount up to about 0.1% carbon and the balance substantially iron; said member having an agehardened and nitrided structure throughout the cross section thereof.
- thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 28% to 53% nickel,about 2.2% to 2.8% titanium, about 0.4% to 0.8% aluminum. about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, a small amount up to about 9% chromium, a small amount up to about 0.1% carbon, and the balance substantially iron; said member having an agehardened and nitrided structure throughout the cross section thereof.
- thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to nickel, about 1% to 10% titanium, and the balance substantially iron, the sum of the titanium plus iron contents being at least 20% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 1% to 10% titanium, a small amount up to about 25% chromium, and the balance substantially iron, the sum of the nickel plus chromium contents not exceeding approximately 80% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, about 1% to 10% titanium, the sum of the iron plus titanium contents being at least 20% of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said mem-- ber having an age-hardened and nitrided structure throughout the cross section thereof.
- thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, a small amount up to about 25% chromium, about 1% to 10% titanium, the sum of the nickel plus chromium contents not exceeding approximately 80% of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, and metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% suflicient to impart age-hardenability, the sum of the iron plus the metal from said group being at least 20% of the alloy composition, the sum or the iron plus nickel contents beingat least 70%.of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about to 97% iron, a small amount up to about 25% chromium, nd metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% suflicient to impart age-hardenability, the sum of the nickel plus chromium contents not exceeding 80% of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- thermoelectric element having a plurality of strip members
- improvement which comprises making at least one strip member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, and metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% sufllcient to impart age-hardenability, the sum of the iron plus the metal from said group being at least of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof; and joining said strip member in face-to-face relationship with another strip member of said thermostatic element.
- thermoelectric element having a plurality of strip members
- improvement which comprises making at least one strip member of said thermostatic element of an alloy contaning about 2% to 80% nickel, about 10% to 97% iron, a small amount up to about chromium, and metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% sumcient to impart age-hardenability, the sum of the nickel plus chromium contents not exceeding about 80% or the alloy composition,
- the sum of the iron plus nickel contents being at least 10% of the alloy composition; said member having an agehardened and nitrided structure throughout the cross section thereof: and joining this strip member in face-to-face relationship with another strip member of said thermostatic element.
- a temperature-responsive device having a plurality of members the improvement which comprises making at least one member of said device of an alloy containing a small but effective amout up to about of metal from the group consisting of nickel, chromium and copper, about 1 to about 10 2, of metal from the group consisting of titanium and aluminum and the balance consisting essentially of iron; said member having an age-hardened and nitrided structure throughout the cross section thereof.
- a temperature-responsive device having a plurality of members, the improvement which comprises making at least one member of said device of an alloy containing a, small but effective amount up to about 80% of metal from the group consisting of nickel, chromium and copper, and the balance essentially metal from the group consisting of titanium, aluminum, manganese, silicon and iron; said member having an age-hardened and nitrided structure throughout the cross section thereof.
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
Description
Dec. 11, 1951 H- ALLOY 0 AGE HARDENED NITR/DED sue/-74 c5 N/TRIDED INTER/012 mi N W. A. MUD GE THERMOSTATIC DEVICE Filed April 10, 1946 F IG.I.-
am/2W FIG. 2.
L-2 ALLOY C AGE-HARDENED N/TR/DED sumac: N/TR/DED INTER/0R INVENTOR. WILLIAM ALVIN MUDGE AM ATTORNEX Patented Dec. 11,1951
THERMOSTATIC DEVICE William Alvin Mudge, New York, N.
Y., assignor to The International Nickel Company, Inc., New York, N. Y., a corporation of Delaware Application April In 14 Claims.
The present invention relates to a composite metal temperature responsive device and more particularly to a thermostatic element to be used in a thermostat.
It is an object of the present invention to provide an improved composite metal thermo static element.
It is another object of the invention to provide a bimetallic thermostatic element having improved strength.
It is still another object of the invention to provide a bimetallic thermostatic element having longer life.
It is a further object to provide a composite metal thermostatic element having improved flexing properties 'by reason of better fatigue resistance.
It is also an object to provide an improved temperature responsive device, such as a thermostat, comprised of the composite metal thermostatic elements provided by the invention.
Other objects and advantages of the invention will be apparent to those skilled in the art from the following description taken in conjunction with the drawing which depicts two views in section of two bimetallic thermostatic elements each embodying the present invention.
Broadly stated, the present invention provides a thermostatic element comprising a plurality of metallic members of dissimilar coeflicients of thermal expansion secured together in faceto-face relationship by rivets, spot welds, diffusion bonding, or other known manner, and adapted to act as a unitary element, at least one of said members being made of an agehardened alloy which is also nitrided throughout the cross section of the member. By agehardened" is meant that the member is in a hardened condition resulting from a solution treatment at high temperatures followed by a treatment at lower temperatures, the latter treatment producing the hardening eifect. In the more common age-hardenable alloys, agehardening is generally obtained by heating the alloy to a high temperature to place the precipitable phase in a solid solution, followed by rapid cooling to preserve the solid solution and treatment of the alloy at lower agin temperatures to precipitate the precipitable phase in a critical finely dispersed state to cause hardening. By "nitrided throughout the cross section" is meant that the member contains nitrogen diffused throughout the cross section of the memher. The invention is not limited to the agehardening and nitriding of only one member 1946, Serial No. 661,082 Canada March 15, 1946 More than one member can be age-hardened and nitrided. Thus, if the thermostatic element consists of two members, both can be agehardened and nitrided throughout their cross sections. Likewise, if the thermostatic element consists of three or more members, more than one member can be age-hardened and nitrided throughout the cross section.
Despite the fact that age-hardening markedly increases the hardness and lowers ductility accordingly, and that nitriding renders metals and alloys extremely hard, up to 1000 Vickers hardness number, with a tendency to be brittle, I have discovered that when a member of a thermostatic element is age-hardened and nitrided throughout the cross section, better flexing properties are obtained. In addition, the thermostatic element made of at least one age-hardened and nitrided member has a high equivalent yield strength. The equivalent yield strengt is considered by many in the art to be a very important property which gives a good indication of the load-carrying capacity which will evaluate service life. The equivalent yield strength" is the stress which will give a composite metal thermostatic element a permanent set when the stress is removed. The degree of permanent set is considered by many in the art to be the Proof Stress set, e. g. 0.01% permanent elongation. The. art has employed severe cold working or cold deformation to raise the equivalent yield strength. The age-hardened and nitrided members provided by the present invention have a higher equivalent yield strength than has been obtainable heretofore by cold working. The age-hardened and nitrided members also have greater strength, better flexing properties and longer life, by reason of improved fatigue resistance. As a result of the improved properties, the invention provides thinner thermostatic members, such as striplike members, than has been available heretofore.
In carrying the invention into practice, it is preferred that the smaller cross sectional dimension of the age-hardened and nitrided member not exceed about 0.03 inch. In order that this member be nitridable, the sum total of the elements present which do not impart nitridability, e. g.-nickel, copper, chromium, molybdenum, tungsten, should not exceed approximately of the whole composition. On the other hand, iron imparts nitridability to the member and is preferably present in the comthe case of copper-base alloys, manganese,
' contain small amounts of ability. such as titanium, maganese, silicon, and aluminum act like iron in this respect. The greater the amount of those elements which are nitriding promoters, the more pronounced will be the effects of nitriding, with respect to both nitrogen concentration and rate of diffusion. The member to be age-hardened and nitrided is made of an alloy containing approximately 2% to 80% of one or more of those metallic elements which do not impart nltridability, e. g. nickel, copper, chromium, molybdenum, tungsten; approximately 20% to 97% of these ele- 'ments which are nitriding promoters, e. g.
titanium, maganese, silicon, aluminum, and particularly iron; and containing at least one age-hardening element, e. g.-titanium, aluminum, silicon, beryllium, and magnesium, and i: an amount sufilcient to impart age-hardenability and nitridability to the alloy.
This invention particularly contemplates agehardened and nitrided members made of an ironnickel-titanium or an iron-nickel-chromiumtitani m alloy containing about 1% to 10% titaniup to about 25% chromium, about 2% to 80% nickel, the balance being substantially iron in an amount constituting at least 10% of the alloy, the sum of the nickel plus any chromium that may be present not exceeding approximately 80% of the whole composition, and the sum of the iron plus nickel contents being at least approximately 70% of the whole composition. An example of different types of alloys which also may be empolyed in accordance with this invention as an age-hardened and nitrided member of the thermostatic element are the copper-nickel-manganese alloys, e. g.-60% copper, 20% nickel, and 20% manganese, such as are disclosed in the Dean, United States patent, No. 2,234,552.
Illustrative examples of ranges of compositions which are preferably employed in accordance with the invention as the nitrided and age-hardened member of the thermostatic element are as follows:
A B O I) E Percent Ni... 40.5425 44. 5-40.15 51.0-53.0 2s.0-a0.0 41.0-43.0 Percent'li... 2.2-2.8 2.2- 2.8 2.2-2.8 2.2-2.8 2.2-2.8 PereentAl... 0.4- 0.8 0.4-0.8 0.4-0.8 0.2-0.8 0.4-0.8 Per cent 8L.-. 0.1- 0.8 0.1- 0.8 0. l- 0.8 0.1- 0.8 0.1- 0.8 Per cent Mn... 0.3- 0.0 0.3- 0.0 0. 3- 0.6 0.3- 0.0 0.3- 0.0 Per cent Cr... 8.0- 9.0 4.5- 6.5 Per cent 0.... 0.1mm: 0.1max. lmax 0.1rnax. 0.1max. Per cent Fe. Balance Balance Balance Balance Balance When it is stated herein that the balance is iron or is substantially all iron, it is not intended to exclude small percentages of incidental elements and impurities such as cobalt, calcium, sulfur, phosphorus, etc. Thus, the compositions usually sulfur and/or phosphorus. but it is preferred that the amounts of each of these, when present, not exceed about 0.04%. Likewise, cobalt may be presen Commercial nickel usually contains some cobalt in amounts up to about 1% or more. The presence of cobalt in the amounts of the order of is often beneficial in low-expansion iron-nickel alloys such as set forth hereinabove. Small amounts of calcium of the order of about 0.05% are often desirable to impart forgeability.
Alloy compositions A, B, and C in the axehardened and nitrided condition are particularly suitable as the low-expansion member of the thermostatic element, for example,'members L4 and L-2 in the drawing. Alloy composition P in 1. constituent, e. g.,
the age-hardened and nitrided condition forms an excellent mghecxpansion member, for example, member 11-! in the drawing. Alloy composition E when age-hardened and nitrided throughout the cross section can be used/ either as the low-expansion member or the high-expansion member. Thus, when used in combination with an age-hardened and nitrided member of alloy composition A or B, any of the latter is the low-expansion member, and the member of composition E is the high-expansion member. when used in combination with a member made of alloy composition C or D, the latter is the high-expansion member, and the composition E member is the low-expansion member. In all the foregoing examples, both the low-expansion and the high-expansion member can be in the ace-hard- .ened and nitrided condition, or only one member need be in such a condition. ber could be in an age-hardened and nitrided condition while the other is ina non-nitrided but age-hardened condition. It is preferred that both members be in an age-hardened and nitrided condition provided the expansion and other required properties will so permit.
when only one member is made of an agehardened and nitrided alloy, such as compositions A to E, the other member can be a non-nitridable material, such as non-ferrous alloys. Illustrative examples of suitable non-ferrous alloys include cupro-nickel, e. g., an alloy containing about 30% to 45% nickel and about 55% to 70% copp r, and nickel-copper alloys sold under the trade-mark of "Monel" and containing about two-thirds nickel and one-third 33% copper and about 63% to 73% nickel. Small amounts of age-hardening elements, e. g., aluminum and/or titanium, may be present in the nickel-copper alloy, and such an alloy is sold under the trade-mark K Monel." The non-nitrided member can be made of such an age-hardenable alloy composition. When cupro-nickel or nickelcopper alloys are employed as the non-nitrided member, that member is the high-expansion member when the other member is made of an age-hardened and nitrided alloy of compositions A, B, C, or E, and is the low-expansion member when the other member is made of an age-hardened nitrided alloy of composition D.
Illustrative examples of compositions suitable for use in strip-like or ribbon-like form as the age-hardened 'and nitrided members in the thermostatic elements, and temperature responsive devices comprised thereof, contemplated by the invention include the following:
Thus, one mem- I 4 111 IV v 42.0 45.0 02.0 20.0 42.0 24 a4 24 2.4 2.4 0.4 0.4 0.4 0.4 0.4 0.3 as 0.0 0.5 0.5 0.4 0.4 0.4 0.4 0.4 as 5.4
0.00 0.00 0.00 0.00 0.00 max. max. max. max. max. Per cent Fe B81. an. m0. an. an.
Compositions I to V are illustrative of alloys within the ranges of compositions A to E. respectively, and are all age-hardenable and nitridable. Age-hardening can be obtainodin all the compositions by treatment for at least twenty minutes, e. g., one-half to one and one-half hours. within the solution temperature range of about 1700" F. to 1850 F., followed by cooling the alloy to preserve the solid solution of the precipitable by a rapid cooling such as copper, e. g., about 26% to quenching, and thereafter treating the compositions within the aging temperature range of about 1100 F. to 1350 F. to impart age-hardness, e. g., treating within said range for about three to forty-eight hours. The compositions can all be nitrided by treating them in an atmosphere of dissociated ammonia, e. g., about 24% to 40% dissociation, at nitriding temperatures between about 900 F. and 1200 F. for sufficient time to nitride the member throughout its cross section. Because the nitriding temperatures overlap the aging temperatures, it is possible to age-harden and nitride the member simultaneously, e. g., at temperatures of about 1100 F. to 1200 F. In other words, after treatment to simultaneously in an age-hardened and nitrided condition throughout its cross section.
The age-hardened and nitrided member can advantageously be subjected to an additional shot-peening treatment to improve further the strength and performance of the thermostatic element. The shot-peening treatment can be accomplished by the usual methods, and its effect is superimposed on those derived from the agehardening and nitriding treatment whereby new and improved characteristics are obtained in thermostatic elements.
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 variations and modifications are considered to be within the purview and scope of the invention and the appended claims.
I claim:
1. As a new article of manufacture, a bimetallic thermostatic element comprising a low-expansion member made of an iron-nickel alloy containing about 40.5% to 53% nickel, about 2.2% to 2.8% titanium, about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese,a small amount up to about 6.5 chromium, a small amount up to about 0.1% carbon and the balance substantially iron, and a high expansion member made of an iron-nickel alloy containing about 28% to 30% nickel, about 2.2%
to 2.8% titanium, about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, about 8% to 9% chromium, up to about 0.1% carbon and the balance substantially iron, said low-expansion member and said highexpansion member both being in an age-hardened and nitrided condition throughout the cross sections of said members.
2. In a bimetallic thermostat the improvement which comprises making the low-expansion member of said thermostat of an alloy containing about 40.5% to 53% nickel, about 2.2% to 2.8% i a um. about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, a small amount up to about 6.5% chromium, a small amount up to about 0.1% carbon and the balance substantially iron; said member having an age-hardened and nitrided structure throughout the cross section thereof.
3. In a bimetallic thermostat the improvement which comprises making the high-expansion member of said thermostat or an alloy containing about 28% to 30% nickel, about 2.2% to 2.8% titanium, about 0.4% to 0.8% aluminum, about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, about 8% to 9% chromium, a small amount up to about 0.1% carbon and the balance substantially iron; said member having an agehardened and nitrided structure throughout the cross section thereof.
4. In a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 28% to 53% nickel,about 2.2% to 2.8% titanium, about 0.4% to 0.8% aluminum. about 0.1% to 0.8% silicon, about 0.3% to 0.6% manganese, a small amount up to about 9% chromium, a small amount up to about 0.1% carbon, and the balance substantially iron; said member having an agehardened and nitrided structure throughout the cross section thereof.
5. In a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to nickel, about 1% to 10% titanium, and the balance substantially iron, the sum of the titanium plus iron contents being at least 20% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
6. In a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 1% to 10% titanium, a small amount up to about 25% chromium, and the balance substantially iron, the sum of the nickel plus chromium contents not exceeding approximately 80% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
7. In a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, about 1% to 10% titanium, the sum of the iron plus titanium contents being at least 20% of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said mem-- ber having an age-hardened and nitrided structure throughout the cross section thereof.
8. Ina thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, a small amount up to about 25% chromium, about 1% to 10% titanium, the sum of the nickel plus chromium contents not exceeding approximately 80% of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
9. In a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, and metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% suflicient to impart age-hardenability, the sum of the iron plus the metal from said group being at least 20% of the alloy composition, the sum or the iron plus nickel contents beingat least 70%.of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
10. In a thermostatic element having a plurality of members the improvement which comprises making at least one member of said thermostatic element of an alloy containing about 2% to 80% nickel, about to 97% iron, a small amount up to about 25% chromium, nd metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% suflicient to impart age-hardenability, the sum of the nickel plus chromium contents not exceeding 80% of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof.
11. In the method of producing a thermostatic element having a plurality of strip members the improvement which comprises making at least one strip member of said thermostatic element of an alloy containing about 2% to 80% nickel, about 10% to 97% iron, and metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% sufllcient to impart age-hardenability, the sum of the iron plus the metal from said group being at least of the alloy composition, the sum of the iron plus nickel contents being at least 70% of the alloy composition; said member having an age-hardened and nitrided structure throughout the cross section thereof; and joining said strip member in face-to-face relationship with another strip member of said thermostatic element.
12. In the method of producing a thermostatic element having a plurality of strip members the improvement which comprises making at least one strip member of said thermostatic element of an alloy contaning about 2% to 80% nickel, about 10% to 97% iron, a small amount up to about chromium, and metal from the group consisting of aluminum and titanium in an amount within the range of about 1% to 10% sumcient to impart age-hardenability, the sum of the nickel plus chromium contents not exceeding about 80% or the alloy composition,
the sum of the iron plus nickel contents being at least 10% of the alloy composition; said member having an agehardened and nitrided structure throughout the cross section thereof: and joining this strip member in face-to-face relationship with another strip member of said thermostatic element.
13. In a temperature-responsive device having a plurality of members the improvement which comprises making at least one member of said device of an alloy containing a small but effective amout up to about of metal from the group consisting of nickel, chromium and copper, about 1 to about 10 2, of metal from the group consisting of titanium and aluminum and the balance consisting essentially of iron; said member having an age-hardened and nitrided structure throughout the cross section thereof.
14. In a temperature-responsive device having a plurality of members, the improvement which comprises making at least one member of said device of an alloy containing a, small but effective amount up to about 80% of metal from the group consisting of nickel, chromium and copper, and the balance essentially metal from the group consisting of titanium, aluminum, manganese, silicon and iron; said member having an age-hardened and nitrided structure throughout the cross section thereof.
WILLIAM ALVIN MUDGE.
REFERENCES CITED The following references are of record in the file of this patent:
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2578197X | 1946-03-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2578197A true US2578197A (en) | 1951-12-11 |
Family
ID=4176450
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US661082A Expired - Lifetime US2578197A (en) | 1946-03-15 | 1946-04-10 | Thermostatic device |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2578197A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2346812A1 (en) * | 1976-04-01 | 1977-10-28 | Rau Fa G | HIGH-USE LIMIT BILAME AND PROCESS FOR MANUFACTURING IT |
| US4645120A (en) * | 1982-12-27 | 1987-02-24 | Gte Products Corporation | Thermostatic metal |
| US4680238A (en) * | 1982-12-27 | 1987-07-14 | Gte Products Corporation | Thermostatic metal |
| WO1994012679A1 (en) * | 1992-11-23 | 1994-06-09 | Albert Young | Nitrided nickel-base article and ion-nitriding method |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1805049A (en) * | 1928-11-16 | 1931-05-12 | Int Nickel Co | Iron-nickel-copper alloy |
| US1929252A (en) * | 1931-12-09 | 1933-10-03 | Moore Drop Forging Company | Nitrided ferrous article |
| US1939085A (en) * | 1930-04-23 | 1933-12-12 | Westinghouse Electric & Mfg Co | Bimetal thermostat |
| US2048163A (en) * | 1929-04-15 | 1936-07-21 | Int Nickel Co | Iron-nickel-titanium alloy |
| US2100411A (en) * | 1934-10-16 | 1937-11-30 | Ver Leichtmetallwerke Gmbh | Method of increasing the corrosion resistance of aluminum alloys and products resulting therefrom |
| USRE22357E (en) * | 1943-07-27 | Alloy | ||
| US2349577A (en) * | 1941-11-21 | 1944-05-23 | Chicago Dev Co | Control member |
-
1946
- 1946-04-10 US US661082A patent/US2578197A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USRE22357E (en) * | 1943-07-27 | Alloy | ||
| US1805049A (en) * | 1928-11-16 | 1931-05-12 | Int Nickel Co | Iron-nickel-copper alloy |
| US2048163A (en) * | 1929-04-15 | 1936-07-21 | Int Nickel Co | Iron-nickel-titanium alloy |
| US1939085A (en) * | 1930-04-23 | 1933-12-12 | Westinghouse Electric & Mfg Co | Bimetal thermostat |
| US1929252A (en) * | 1931-12-09 | 1933-10-03 | Moore Drop Forging Company | Nitrided ferrous article |
| US2100411A (en) * | 1934-10-16 | 1937-11-30 | Ver Leichtmetallwerke Gmbh | Method of increasing the corrosion resistance of aluminum alloys and products resulting therefrom |
| US2349577A (en) * | 1941-11-21 | 1944-05-23 | Chicago Dev Co | Control member |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2346812A1 (en) * | 1976-04-01 | 1977-10-28 | Rau Fa G | HIGH-USE LIMIT BILAME AND PROCESS FOR MANUFACTURING IT |
| US4131720A (en) * | 1976-04-01 | 1978-12-26 | G. Rau | Heavy-duty heat-responsive bimetallic material |
| US4645120A (en) * | 1982-12-27 | 1987-02-24 | Gte Products Corporation | Thermostatic metal |
| US4680238A (en) * | 1982-12-27 | 1987-07-14 | Gte Products Corporation | Thermostatic metal |
| WO1994012679A1 (en) * | 1992-11-23 | 1994-06-09 | Albert Young | Nitrided nickel-base article and ion-nitriding method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| AU627965B2 (en) | Oxidation resistant low expansion superalloys | |
| US3164465A (en) | Nickel-base alloys | |
| US5372662A (en) | Nickel-base alloy with superior stress rupture strength and grain size control | |
| US2920954A (en) | Stainless steel alloy of high hardness | |
| US3030206A (en) | High temperature chromiummolybdenum alloy | |
| US2542962A (en) | Nickel aluminum base alloys | |
| US2654946A (en) | Soldered joint for chromium alloy gas turbine structures | |
| US2578197A (en) | Thermostatic device | |
| US2274999A (en) | Glass-to-metal seal | |
| US2494736A (en) | Copper base alloy | |
| US3127265A (en) | Table ii | |
| US2306667A (en) | Alloy | |
| US2553609A (en) | Weldable and high-temperature resisting hard alloys of cobalt and iron base | |
| US3591371A (en) | Cobalt base oxidation resistant alloy | |
| US3005705A (en) | High temperature alloys | |
| US2332416A (en) | Bimetal | |
| US2109285A (en) | Alloy | |
| IE49710B1 (en) | Precipitation hardening copper alloys | |
| US2513469A (en) | Alloy articles for use at high temperatures | |
| US3303024A (en) | Nickel-base brazing alloys | |
| US1892316A (en) | Noncorrosive steel alloy | |
| US2575915A (en) | Nickel base high-temperature alloy | |
| US2177454A (en) | Alloy steel for internal combustion valves or valve elements | |
| US2978319A (en) | High strength, low alloy steels | |
| US3068096A (en) | Wear-resistant alloy |