FR2099818A5 - - Google Patents

Info

Publication number
FR2099818A5
FR2099818A5 FR7122753A FR7122753A FR2099818A5 FR 2099818 A5 FR2099818 A5 FR 2099818A5 FR 7122753 A FR7122753 A FR 7122753A FR 7122753 A FR7122753 A FR 7122753A FR 2099818 A5 FR2099818 A5 FR 2099818A5
Authority
FR
France
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
FR7122753A
Other languages
French (fr)
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
Application granted granted Critical
Publication of FR2099818A5 publication Critical patent/FR2099818A5/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • C22F1/10—Changing 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7122753A 1970-06-25 1971-06-14 Expired FR2099818A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US4995770A 1970-06-25 1970-06-25

Publications (1)

Publication Number Publication Date
FR2099818A5 true FR2099818A5 (en) 1972-03-17

Family

ID=21962666

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7122753A Expired FR2099818A5 (en) 1970-06-25 1971-06-14

Country Status (6)

Country Link
US (1) US3676225A (en)
CA (1) CA940806A (en)
DE (1) DE2130518A1 (en)
FR (1) FR2099818A5 (en)
GB (1) GB1342831A (en)
SE (1) SE379212B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2557148A1 (en) * 1983-12-27 1985-06-28 United Technologies Corp PROCESS FOR INCREASING THE FORGEABILITY OF A NICKEL-BASED SUPERALLIAGE ARTICLE
FR2557147A1 (en) * 1983-12-27 1985-06-28 United Technologies Corp PROCESS FOR FORGING HIGH-RESISTANCE NICKEL-BASED SUPERALLIER MATERIALS, ESPECIALLY IN MOLDED FORM
FR2557145A1 (en) * 1983-12-21 1985-06-28 Snecma THERMOMECHANICAL TREATMENT PROCESS FOR SUPERALLOYS TO OBTAIN STRUCTURES WITH HIGH MECHANICAL CHARACTERISTICS
US5417782A (en) * 1992-06-03 1995-05-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Heat treatment process for a NI-based superalloy

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4514360A (en) * 1982-12-06 1985-04-30 United Technologies Corporation Wrought single crystal nickel base superalloy
US4769087A (en) * 1986-06-02 1988-09-06 United Technologies Corporation Nickel base superalloy articles and method for making
US5074925A (en) * 1990-06-25 1991-12-24 The United States Of America As Represented By The Secretary Of The Air Force Thermomechanical fabrication of net shape single crystal airfoils
FR2722510B1 (en) * 1994-07-13 1996-08-14 Snecma PROCESS FOR THE PREPARATION OF 718 ALLOY SHEETS AND FOR THE SUPERPLASTIC FORMING OF SAME
US20040221929A1 (en) 2003-05-09 2004-11-11 Hebda John J. Processing of titanium-aluminum-vanadium alloys and products made thereby
US7837812B2 (en) 2004-05-21 2010-11-23 Ati Properties, Inc. Metastable beta-titanium alloys and methods of processing the same by direct aging
US8539659B2 (en) 2008-04-23 2013-09-24 United Technologies Corporation Method of repairing an article
US10053758B2 (en) 2010-01-22 2018-08-21 Ati Properties Llc Production of high strength titanium
US9255316B2 (en) 2010-07-19 2016-02-09 Ati Properties, Inc. Processing of α+β titanium alloys
US9206497B2 (en) 2010-09-15 2015-12-08 Ati Properties, Inc. Methods for processing titanium alloys
US8613818B2 (en) 2010-09-15 2013-12-24 Ati Properties, Inc. Processing routes for titanium and titanium alloys
US10513755B2 (en) 2010-09-23 2019-12-24 Ati Properties Llc High strength alpha/beta titanium alloy fasteners and fastener stock
US8652400B2 (en) 2011-06-01 2014-02-18 Ati Properties, Inc. Thermo-mechanical processing of nickel-base alloys
US9869003B2 (en) 2013-02-26 2018-01-16 Ati Properties Llc Methods for processing alloys
US9192981B2 (en) 2013-03-11 2015-11-24 Ati Properties, Inc. Thermomechanical processing of high strength non-magnetic corrosion resistant material
US9777361B2 (en) 2013-03-15 2017-10-03 Ati Properties Llc Thermomechanical processing of alpha-beta titanium alloys
US11111552B2 (en) 2013-11-12 2021-09-07 Ati Properties Llc Methods for processing metal alloys
US10094003B2 (en) 2015-01-12 2018-10-09 Ati Properties Llc Titanium alloy
US10502252B2 (en) 2015-11-23 2019-12-10 Ati Properties Llc Processing of alpha-beta titanium alloys
CN115491620B (en) * 2022-09-14 2023-03-21 浙江大学 Under-aging heat treatment process of nickel-based wrought superalloy

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2557145A1 (en) * 1983-12-21 1985-06-28 Snecma THERMOMECHANICAL TREATMENT PROCESS FOR SUPERALLOYS TO OBTAIN STRUCTURES WITH HIGH MECHANICAL CHARACTERISTICS
EP0148688A2 (en) * 1983-12-21 1985-07-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Method for the thermomechanical treatment of superalloys to obtain structures with great mechanical characteristics
EP0148688A3 (en) * 1983-12-21 1985-08-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Method for the thermomechanical treatment of superalloys to obtain structures with great mechanical characteristics
FR2557148A1 (en) * 1983-12-27 1985-06-28 United Technologies Corp PROCESS FOR INCREASING THE FORGEABILITY OF A NICKEL-BASED SUPERALLIAGE ARTICLE
FR2557147A1 (en) * 1983-12-27 1985-06-28 United Technologies Corp PROCESS FOR FORGING HIGH-RESISTANCE NICKEL-BASED SUPERALLIER MATERIALS, ESPECIALLY IN MOLDED FORM
US5417782A (en) * 1992-06-03 1995-05-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Heat treatment process for a NI-based superalloy

Also Published As

Publication number Publication date
SE379212B (en) 1975-09-29
DE2130518A1 (en) 1971-12-30
US3676225A (en) 1972-07-11
CA940806A (en) 1974-01-29
GB1342831A (en) 1974-01-03

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Legal Events

Date Code Title Description
ST Notification of lapse