GB1124044A - Improvements in and relating to heat treatment of nickel-base alloys - Google Patents

Improvements in and relating to heat treatment of nickel-base alloys

Info

Publication number
GB1124044A
GB1124044A GB38102/65A GB3810265A GB1124044A GB 1124044 A GB1124044 A GB 1124044A GB 38102/65 A GB38102/65 A GB 38102/65A GB 3810265 A GB3810265 A GB 3810265A GB 1124044 A GB1124044 A GB 1124044A
Authority
GB
United Kingdom
Prior art keywords
heating
nickel
relating
heat treatment
base alloys
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
GB38102/65A
Other languages
English (en)
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1124044A publication Critical patent/GB1124044A/en
Expired legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C16/00Alloys based on zirconium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/32Selection of soldering or welding materials proper with the principal constituent melting at more than 1550 degrees C
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/10Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
GB38102/65A 1964-10-21 1965-09-07 Improvements in and relating to heat treatment of nickel-base alloys Expired GB1124044A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US405410A US3310440A (en) 1964-10-21 1964-10-21 Heat treatment of nickel base alloys

Publications (1)

Publication Number Publication Date
GB1124044A true GB1124044A (en) 1968-08-21

Family

ID=23603591

Family Applications (1)

Application Number Title Priority Date Filing Date
GB38102/65A Expired GB1124044A (en) 1964-10-21 1965-09-07 Improvements in and relating to heat treatment of nickel-base alloys

Country Status (8)

Country Link
US (1) US3310440A (xx)
JP (1) JPS5136206B1 (xx)
BE (1) BE671189A (xx)
CH (1) CH466931A (xx)
DE (1) DE1483315B1 (xx)
GB (1) GB1124044A (xx)
NL (1) NL148945B (xx)
SE (1) SE312921B (xx)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0330858A1 (de) * 1988-03-02 1989-09-06 Asea Brown Boveri Ag Ausscheidungshärtbare Nickelbasis-Superlegierung mit verbesserten mechanischen Eigenschaften im Temperaturbereich von 600 bis 750oC

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3753790A (en) * 1972-08-02 1973-08-21 Gen Electric Heat treatment to dissolve low melting phases in superalloys
DE2620197C3 (de) * 1976-05-07 1980-08-07 Maschinenfabrik Augsburg-Nuernberg Ag, 8000 Muenchen Verfahren zur Wärmebehandlung von Bauteilen aus hochwarmfesten Werkstoffen
JPS52154903U (xx) * 1976-05-20 1977-11-24
US4221610A (en) * 1978-02-24 1980-09-09 The United States Of America As Represented By The United States Department Of Energy Method for homogenizing alloys susceptible to the formation of carbide stringers and alloys prepared thereby
US4492672A (en) * 1982-04-19 1985-01-08 The United States Of America As Represented By The Secretary Of The Navy Enhanced microstructural stability of nickel alloys
FR2572738B1 (fr) * 1984-11-08 1987-02-20 Snecma Methode de regeneration de pieces en superalliage base nickel en fin de potentiel de fonctionnement
AT383762B (de) * 1985-12-23 1987-08-25 Plansee Metallwerk Verfahren zur herstellung mehrkomponentiger, kongruent erschmelzender lotmaterialien
US4717432A (en) * 1986-04-09 1988-01-05 United Technologies Corporation Varied heating rate solution heat treatment for superalloy castings
US6531005B1 (en) * 2000-11-17 2003-03-11 General Electric Co. Heat treatment of weld repaired gas turbine engine components
ITMI20042481A1 (it) * 2004-12-23 2005-03-23 Nuovo Pignone Spa Turbina a vapore
ITMI20042483A1 (it) * 2004-12-23 2005-03-23 Nuovo Pignone Spa Turbina a vapore
ITMI20042488A1 (it) * 2004-12-23 2005-03-23 Nuovo Pignone Spa Turbina a vapore

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE533026C (de) * 1928-12-30 1931-09-10 Georg Brunhuebner Lot
US2887420A (en) * 1956-04-06 1959-05-19 Bristol Aero Engines Ltd Surface treatments for articles made from heat resisting alloys
DE1153226B (de) * 1957-10-23 1963-08-22 Philips Nv Verfahren zum Verbinden einer aus einem hochschmelzenden Metall bestehenden Folie mit einem Gegenstand aus einem hoch-schmelzenden Metall mit Hilfe eines pulver-foermigen, ein Monokarbid dieses Metalls enthaltenden Loetmaterials
DE1146728B (de) * 1959-11-23 1963-04-04 Atomic Energy Commission Verfahren zum Zusammenloeten von Teilen aus Niob
US3212886A (en) * 1961-10-03 1965-10-19 Armco Steel Corp High temperature alloy
US3166412A (en) * 1962-08-31 1965-01-19 Int Nickel Co Cast nickel-base alloy for gas turbine rotors
US3254994A (en) * 1963-06-24 1966-06-07 Trw Inc Alloys having improved stress rupture properties
US3272666A (en) * 1963-12-09 1966-09-13 Du Pont Method of heat treating nickel base alloy articles up to 20 mils in thickness

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0330858A1 (de) * 1988-03-02 1989-09-06 Asea Brown Boveri Ag Ausscheidungshärtbare Nickelbasis-Superlegierung mit verbesserten mechanischen Eigenschaften im Temperaturbereich von 600 bis 750oC
CH675256A5 (xx) * 1988-03-02 1990-09-14 Asea Brown Boveri
US4957703A (en) * 1988-03-02 1990-09-18 Asea Brown Boveri Ltd. Precipitation-hardenable nickel-base superalloy with improved mechanical properties in the temperature range from 600 to 750 degrees celsius

Also Published As

Publication number Publication date
JPS5136206B1 (xx) 1976-10-07
NL148945B (nl) 1976-03-15
CH466931A (fr) 1968-12-31
BE671189A (xx) 1966-02-14
SE312921B (xx) 1969-07-28
NL6512668A (xx) 1966-04-22
DE1483315B1 (de) 1971-06-09
US3310440A (en) 1967-03-21

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