GB1075887A - Creación de Inventos y Patentes con Inteligencia Artificial

GB1075887A – Improvements in and relating to titanium and titanium base alloys
– Google Patents

GB1075887A – Improvements in and relating to titanium and titanium base alloys
– Google Patents
Improvements in and relating to titanium and titanium base alloys

Info

Publication number
GB1075887A

GB1075887A
GB17753/65A
GB1775365A
GB1075887A
GB 1075887 A
GB1075887 A
GB 1075887A
GB 17753/65 A
GB17753/65 A
GB 17753/65A
GB 1775365 A
GB1775365 A
GB 1775365A
GB 1075887 A
GB1075887 A
GB 1075887A
Authority
GB
United Kingdom
Prior art keywords
coating
parts
sodium silicate
weight
titanium
Prior art date
1964-04-27
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
GB17753/65A
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.)

CONTINENTAL TITANIUM METALS CO

Original Assignee
CONTINENTAL TITANIUM METALS CO
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.)
1964-04-27
Filing date
1965-04-27
Publication date
1967-07-12

1965-04-27
Application filed by CONTINENTAL TITANIUM METALS CO
filed
Critical
CONTINENTAL TITANIUM METALS CO

1967-05-24
Priority claimed from GB2423067A
external-priority
patent/GB1127566A/en

1967-07-12
Publication of GB1075887A
publication
Critical
patent/GB1075887A/en

Status
Expired
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

Classifications

C—CHEMISTRY; METALLURGY

C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL

C23D—ENAMELLING OF, OR APPLYING A VITREOUS LAYER TO, METALS

C23D5/00—Coating with enamels or vitreous layers

C23D5/10—Coating with enamels or vitreous layers with refractory materials

C—CHEMISTRY; METALLURGY

C03—GLASS; MINERAL OR SLAG WOOL

C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS

C03C4/00—Compositions for glass with special properties

C—CHEMISTRY; METALLURGY

C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES

C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE

C04B28/00—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements

C04B28/24—Compositions of mortars, concrete or artificial stone, containing inorganic binders or the reaction product of an inorganic and an organic binder, e.g. polycarboxylate cements containing alkyl, ammonium or metal silicates; containing silica sols

C04B28/26—Silicates of the alkali metals

C—CHEMISTRY; METALLURGY

C21—METALLURGY OF IRON

C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING

C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering

C21D1/68—Temporary coatings or embedding materials applied before or during heat treatment

C—CHEMISTRY; METALLURGY

C21—METALLURGY OF IRON

C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING

C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering

C21D1/68—Temporary coatings or embedding materials applied before or during heat treatment

C21D1/70—Temporary coatings or embedding materials applied before or during heat treatment while heating or quenching

C—CHEMISTRY; METALLURGY

C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS

C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS

C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working

C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon

C22F1/18—High-melting or refractory metals or alloys based thereon

C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

C—CHEMISTRY; METALLURGY

C23D—ENAMELLING OF, OR APPLYING A VITREOUS LAYER TO, METALS

C23D5/00—Coating with enamels or vitreous layers

Abstract

A titanium or titanium base alloy body has a surface coating which essentially consists of sodium silicate and/or silica and finely distributed aluminium and is such as to form an effective protective glaze when working the body at temperatures of the order of 1800 DEG to 2400 DEG F. A titanium body has a surface coating to protect the surface from atmospheric oxidation at temperatures up to 2400 DEG F. which comprises a layer of 1/64 to 1/4 inch thickness of an intimate mixture consisting essentially of (a) 3 to 6 parts by weight of a sticky aqueous solution of sodium silicate and/or colloidal silica, (b) 3 to 8 parts by weight of aluminium powder, minus 40 mesh, and (c) up to 2 parts of sand, sandblast grade, minus 120 mesh. The aqueous solution of sodium silicate may be of a Na2O to SiO2 ratio from 1 to 1.7 to 1 to 3.9 and water content not more than 65%. The layer may comprise sodium silicate solution of 40 DEG Be, 1.0 to 3.25 Na2O to SiO2 ratio. The layer may comprise about 5 parts of the aqueous solution of sodium silicate and/or colloidal silica, may contain about 5 parts by weight of the aluminium powder, e.g. of minus 200 mesh, and may comprise about 1 part by weight of the sand. The coating may be dried at a temperature not exceeding about 200 DEG F. The drying may be at such rate as to prevent blistering of the coating and after drying the coating, the body is heated to a temperature between 1800 DEG and 2400 DEG F. The body may be rolled after it has been so heated. The coating may be applied by trowelling, spraying or brushing.ALSO:A titanium or titanium base alloy body has a surface coating which essentially consists of sodium silicate and/or silica and finely distributed aluminium and is such as to form an effective protective glaze when working the body at temperatures of the order of 1800 DEG F to 2400 DEG F. A titanium body has a surface coating to protect the surface from atmospheric oxidation at temperatures up to 2400 DEG F which comprises a layer of 1/64 to 1/4 inch thickness of an intimate mixture consisting essentially of (a) 3 to 6 parts by weight of a sticky aqueous solution of sodium silicate and/or colloidal silica, (b) 3 to 8 parts by weight of aluminium powder, minus 40 mesh, and (c) up to 2 parts of sand, sandblast grade, minus 120 mesh. The aqueous solution of sodium silicate may be of a Na2O to SiO2 ratio from 1 to 1.7 to 1 to 3.9 and water content not more than 65%. The layer may comprise sodium silicate solution of 40 DEG Be, 1.0 to 3.25 Na2O to SiO2 ratio. The layer may comprise about 5 parts of the aqueous solution of sodium silicate and/or colloidal silica, may contain about 5 parts by weight of the aluminium powder, e.g. of minus 200 mesh, and may comprise about 1 part by weight of the sand. The coating may be dried at a temperature not exceeding about 200 DEG F. The drying may be at such rate as to prevent blistering of the coating and after drying the coating, the body is heated to a temperature between 1800 and 2400 DEG F. The body may be rolled after it has been so heated. The coating may be applied by trowelling, spraying or brushing.

GB17753/65A
1964-04-27
1965-04-27
Improvements in and relating to titanium and titanium base alloys

Expired

GB1075887A
(en)

Applications Claiming Priority (2)

Application Number
Priority Date
Filing Date
Title

US36293064A

1964-04-27
1964-04-27

GB2423067A

GB1127566A
(en)

1967-05-24
1967-05-24
Improved coatings for titanium bodies

Publications (1)

Publication Number
Publication Date

GB1075887A
true

GB1075887A
(en)

1967-07-12

Family
ID=26256999
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB17753/65A
Expired

GB1075887A
(en)

1964-04-27
1965-04-27
Improvements in and relating to titanium and titanium base alloys

Country Status (2)

Country
Link

FR
(1)

FR1455097A
(en)

GB
(1)

GB1075887A
(en)

Cited By (1)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

WO2018095048A1
(en)

2016-11-23
2018-05-31
叶卫斌
Application of water-soluble silicon glaze

Families Citing this family (1)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

JP3557868B2
(en)

1997-01-14
2004-08-25
セイコーエプソン株式会社

Surface treatment method for decorative articles, decorative articles and electronic equipment

1965

1965-04-27
FR
FR14771A
patent/FR1455097A/en
not_active
Expired

1965-04-27
GB
GB17753/65A
patent/GB1075887A/en
not_active
Expired

Cited By (1)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

WO2018095048A1
(en)

2016-11-23
2018-05-31
叶卫斌
Application of water-soluble silicon glaze

Also Published As

Publication number
Publication date

FR1455097A
(en)

1966-04-01

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