GB1109494A - Composite thermally-responsive materials - Google Patents

Composite thermally-responsive materials

Info

Publication number
GB1109494A
GB1109494A GB2771065A GB2771065A GB1109494A GB 1109494 A GB1109494 A GB 1109494A GB 2771065 A GB2771065 A GB 2771065A GB 2771065 A GB2771065 A GB 2771065A GB 1109494 A GB1109494 A GB 1109494A
Authority
GB
United Kingdom
Prior art keywords
weight
balance
range
copper
responsive materials
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
Application number
GB2771065A
Inventor
Raymond Milton Sears
Unto Uljas Savolainen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Texas Instruments Inc
Original Assignee
Texas Instruments Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Texas Instruments Inc filed Critical Texas Instruments Inc
Priority to GB2771065A priority Critical patent/GB1109494A/en
Publication of GB1109494A publication Critical patent/GB1109494A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
    • B32B15/015—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium the said other metal being copper or nickel or an alloy thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
    • 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
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Contacts (AREA)
  • Conductive Materials (AREA)

Abstract

Alloys suitable for use in bi-metallic temperature responsive elements may comprise nickel within the range 98.5% to 99.9% by weight and the balance manganese; copper within the range 95% to 99.75% and the balance silver; copper within the range 97% to 99.75% by weight and the balance cadmium, or nickel within the range 18% to 25% by weight together with 2% to 12% chromium by weight and the balance iron. Also disclosed is an alloy containing not less than 65% by weight of manganese with the balance copper and/or nickel.
GB2771065A 1965-06-30 1965-06-30 Composite thermally-responsive materials Expired GB1109494A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2771065A GB1109494A (en) 1965-06-30 1965-06-30 Composite thermally-responsive materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2771065A GB1109494A (en) 1965-06-30 1965-06-30 Composite thermally-responsive materials

Publications (1)

Publication Number Publication Date
GB1109494A true GB1109494A (en) 1968-04-10

Family

ID=10264043

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2771065A Expired GB1109494A (en) 1965-06-30 1965-06-30 Composite thermally-responsive materials

Country Status (1)

Country Link
GB (1) GB1109494A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4041432A (en) * 1975-09-16 1977-08-09 Texas Instruments Incorporated Motor protector for high temperature applications and thermostat material for use therein
EP2231394A4 (en) * 2008-01-02 2015-08-19 Ems Engineered Materials Solutions Llc Metallic laminate composite

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4041432A (en) * 1975-09-16 1977-08-09 Texas Instruments Incorporated Motor protector for high temperature applications and thermostat material for use therein
EP2231394A4 (en) * 2008-01-02 2015-08-19 Ems Engineered Materials Solutions Llc Metallic laminate composite

Similar Documents

Publication Publication Date Title
GB925044A (en) Improvements in columbium base alloys
GB1109494A (en) Composite thermally-responsive materials
GB912002A (en) Porous sintered metal friction element
GB1022806A (en) Titanium base alloys
GB1046603A (en) High temperature alloys
ALEXANDER et al. CORROSION OF METALS IN TROPICAL ENVIRONMENTS--NICKEL AND NICKEL-COPPER ALLOYS
GB838949A (en) Improvements relating to brazing and to alloys for use therein
GB885544A (en) Improvements in or relating to temperature measuring devices
Tsumuraya et al. Mechanism of Reversion in Pb-Sb Alloys Containing Traces of As
Frantsevich et al. Use of tagged atoms to determine the relative and total mass transfer in metals and their alloys under the effect of direct current
GRIGOROVICH Investigation of heat resistance properties of zirconium-niobium alloys such as hardness, short-time strength and creep
GB766999A (en) Improvements in lead-base electrical conductor elements
Bouillon et al. INFLUENCE OF SMALL QUANTITIES OF NICKEL ON THE OXIDATION OF COPPER
GB1095807A (en) Hafnium alloys
JPS5369051A (en) Frame for spectacles
GE et al. Heat resistance of alloys of the ti-al-mo-v quaternary system(Heat resistance of titanium-aluminum-molybdenum- vanadium quaternary alloy as function of composition and structure)
Motomura et al. Relating the Resistance to Deformation of Commercial Purity Al and Al Alloys to Strain, Strain Rate and Temperature
Johnson et al. Mechanical and physical properties of five copper-base casting alloys
ES275095A1 (en) Improvements in the alloys of metals very resistant chemically in front of acids and lyps (Machine-translation by Google Translate, not legally binding)
Takezawa et al. Temperature Dependence of the Electrical Resistivity of Pd-Fe Alloy
Bolshakov et al. The mg sub 3 sb sub 2-mg sub 2 si system(Thermal, x-ray and metallographic analysis of as- cast or annealed alloy compositions in solid solution of magnesium antimonide- magnesium silicide)
GB954288A (en) Improvements in and relating to copper-beryllium alloys
GB912175A (en) Improvements in and relating to thermoelement positive electrodes
BUKHANOVA et al. Certain general patterns in the occurence of hydrogen brittleness in the alloys VT 3-1 and VT 15(Development of hydrogen brittleness in titanium alloy at low temperature and low strain rates)
YOUNG PROGRESS IN THE FUSION WELDING OF NON-FERROUS ALLOYS