公开(公告)号：EP3449024A1

公开(公告)日：2019-03-06

申请号：EP17790206.1

申请日：2017-04-24

申请人： Arconic Inc.

发明人： LIN, Jen C. ,  YAN, Xinyan ,  SABOL, Joseph C. ,  HEARD, David W. ,  ZARANDI, Faramarz MH ,  SUN, Fusheng ,  CRIST, Ernest, M., Jr. ,  TAMIRISAKANDALA, Sesh A.

IPC分类号： C22C14/00 ,  B22F3/105 ,  B33Y70/00

公开(公告)号：EP2607507B1

公开(公告)日：2018-12-05

申请号：EP11818260.9

申请日：2011-08-15

申请人： NHK Spring Co., Ltd.

发明人： ARAOKA, Yuji ,  SHIRAISHI, Tohru ,  ONO, Yoshiki

IPC分类号： C22C1/04 ,  B22F1/00 ,  B22F3/14 ,  B22F3/24 ,  C22C14/00 ,  C22F1/18 ,  C23C8/24 ,  B22F9/04 ,  C22F1/00

CPC分类号： C22C14/00 ,  B22F1/004 ,  B22F1/0081 ,  B22F1/0088 ,  B22F3/14 ,  B22F3/24 ,  B22F2003/248 ,  C22C47/14 ,  C22C49/11 ,  C22F1/183 ,  C23C8/02 ,  C23C8/24 ,  C23C8/80

摘要： A titanium alloy material having high overall strength is produced by applying nitrogen to ±-² type titanium alloys that are widely used. A production method for a titanium alloy member includes preparing a titanium alloy material for sintering as a raw material of a sintered body; nitriding the titanium alloy material for sintering, thereby forming a nitrogen compound layer and/or a nitrogen solid solution layer in a surface layer of the titanium alloy material for sintering and yielding a nitrogen-containing titanium alloy material for sintering; mixing the titanium alloy material for sintering and the nitrogen-containing titanium alloy material for sintering, thereby yielding a titanium alloy material for sintering mixed with nitrogen-containing titanium alloy material; sintering the titanium alloy material for sintering mixed with nitrogen-containing titanium alloy material, thereby bonding the material each other and dispersing nitrogen contained in the nitrogen-containing titanium alloy material for sintering in a condition in which nitrogen is uniformly dispersed into an entire inner portion of the sintered body by solid solution.

公开(公告)号：EP3404122A1

公开(公告)日：2018-11-21

申请号：EP18172924.5

申请日：2018-05-17

申请人： Commissariat à l'énergie atomique et aux énergies alternatives

发明人： VINCENT, Denis ,  LAUCOURNET, Richard ,  ROUMANIE, Maryline

IPC分类号： C22C1/05 ,  B22F1/00 ,  C22C1/04 ,  C22C14/00 ,  C22C29/10 ,  B22F5/00 ,  C22C32/00

CPC分类号： C22C1/055 ,  B22F1/0011 ,  B22F5/00 ,  B22F2998/00 ,  B22F2998/10 ,  B22F2999/00 ,  B29C64/00 ,  B33Y10/00 ,  C22C1/0458 ,  C22C14/00 ,  C22C29/10 ,  C22C32/0094 ,  B22F1/0059 ,  B22F3/008 ,  B22F3/1017 ,  B22F2001/0066 ,  B22F2201/20 ,  C22C1/058

摘要： Procédé d'élaboration d'un matériau composite à matrice métallique comprenant au moins les étapes successives suivantes :
a) Fourniture d'une pièce formée d'une poudre métallique dispersée dans un matériau polymère, le matériau polymère comprenant au moins un polymère comprenant une double liaison carbone-carbone et/ou un cycle aromatique,
b) Réalisation d'un premier traitement thermique à une première température T d sur la pièce de manière à dégrader le matériau polymère pour former des résidus carbonés,
c) Réalisation d'un second traitement thermique à une deuxième température T f , supérieure à la première température T d , pour fritter la poudre métallique et, simultanément, diffuser le carbone, provenant des résidus carbonés, dans la poudre métallique de manière à former des précipités de carbure de métal dispersés dans une matrice métallique.

公开(公告)号：EP3380639A1

公开(公告)日：2018-10-03

申请号：EP16805686.9

申请日：2016-11-18

申请人： ATI Properties LLC

发明人： FOLTZ, IV, John, W. ,  GARSIDE, Gavin

IPC分类号： C22C14/00 ,  C22F1/18

CPC分类号： F16B33/00 ,  C22C14/00 ,  C22F1/183 ,  F16B19/04 ,  F16B37/00 ,  F16B39/24 ,  F16B43/00

摘要： A method for increasing tensile strength of a cold workable alpha-beta titanium alloy comprises solution heat treating a cold workable alpha-beta titanium alloy in a temperature range of Tβ-106° C. to Tβ-72.2° C. for 15 minutes to 2 hours; cooling the alpha-beta titanium alloy at a cooling rate of at least 3000° C./minute; cold working the alpha-beta titanium alloy to impart an effective strain in the range of 5 percent to 35 percent in the alloy; and aging the alpha-beta titanium alloy in a temperature range of Tβ-669° C. to Tβ-517° C. for 1 to 8 hours. Fastener stock and fasteners including solution treated, quenched, cold worked, and aged alpha-beta titanium alloys are also disclosed.

公开(公告)号：EP2644307B1

公开(公告)日：2018-08-15

申请号：EP11843305.1

申请日：2011-11-22

申请人： Sumitomo Electric Industries, Ltd. ,  Sumitomo Electric Hardmetal Corp. ,  National Institute of Advanced Industrial Science and Technology

发明人： ISHIDA, Tomoyuki ,  MORIGUCHI, Hideki ,  NAKASHIMA, Takeru ,  KUKINO, Satoru ,  YURUGI, Shinichiro ,  ENAMI, Teruhiro ,  OKAMURA, Katsumi ,  MATSUDA, Yusuke ,  SANO, Koji ,  KOBAYASHI, Keizo ,  OZAKI, Kimihiro

IPC分类号： B23K20/00 ,  B23B27/18 ,  B23B27/20 ,  B23K1/19 ,  B23K35/30 ,  C22C9/06 ,  C22C14/00 ,  C22C19/00 ,  B23K1/008 ,  B23K13/00

CPC分类号： C22C1/023 ,  B23B2222/88 ,  B23B2224/36 ,  B23B2226/125 ,  B23B2240/08 ,  B23K1/0004 ,  B23K1/0008 ,  B23K1/008 ,  B23K1/19 ,  B23K20/023 ,  B23K20/16 ,  B23K20/233 ,  B23K31/025 ,  B23K35/001 ,  B23K35/302 ,  B23K35/3033 ,  B23K2101/20 ,  B23K2103/18 ,  B23K2103/52 ,  C22C1/02 ,  C22C9/00 ,  C22C9/06 ,  Y10T403/479

摘要： The present joined product is a joined product with a cemented carbide sintered compact serving as a first material to be joined (1) and a cBN sintered compact serving as a second material to be joined (2), wherein: the first material to be joined (1) and the second material to be joined (2) are joined together via a joining material (3) disposed therebetween and containing titanium (Ti); and a titanium nitride (TiN) compound layer having a thickness of 10-300 nm is produced at an interface between the second material to be joined (2) and the joining material (3).

公开(公告)号：EP3150305A4

公开(公告)日：2018-07-25

申请号：EP15799359

申请日：2015-06-01

申请人： MITSUBISHI MATERIALS CORP

发明人： YANG JI-BIN ,  KITA KOICHI ,  SAIWAI TOSHIHIKO ,  HOSHINO KOJI ,  KATOH JUN

IPC分类号： B22F5/10 ,  B22F1/00 ,  B22F7/00 ,  B22F7/04 ,  B23K35/02 ,  B23K35/32 ,  B32B15/01 ,  C22C1/08 ,  C22C14/00 ,  C22C21/12

CPC分类号： B22F7/002 ,  B22F1/0011 ,  B22F3/1021 ,  B22F3/11 ,  B22F5/10 ,  B22F7/004 ,  B22F7/04 ,  B22F2301/052 ,  B22F2998/10 ,  B22F2999/00 ,  B23K1/0008 ,  B23K1/19 ,  B23K35/0244 ,  B23K35/325 ,  B32B15/016 ,  B32B15/20 ,  B32B2305/026 ,  C22C1/08 ,  C22C14/00 ,  C22C21/00 ,  C22C21/12 ,  C22C32/0089 ,  B22F7/062 ,  B22F3/002 ,  B22F1/004 ,  B22F1/025 ,  B22F3/10 ,  B22F2201/10 ,  B22F1/0059

摘要： A high quality porous aluminum body, which has excellent joint strength between the porous aluminum body and the aluminum bulk body, and a method of producing the porous aluminum complex, are provided. The porous aluminum complex (10) includes: a porous aluminum body (30) made of aluminum or aluminum alloy; and an aluminum bulk body (20) made of aluminum or aluminum alloy, the porous aluminum body (30) and the aluminum bulk body (20) being joined each other. The junction (15) between the porous aluminum body (30) and the aluminum bulk body (20) includes a Ti-Al compound. It is preferable that pillar-shaped protrusions (32) projecting toward the outside are formed on outer surfaces of one of or both of the porous aluminum body (30) and the aluminum bulk body (20), and the pillar-shaped protrusions (32) include the junction (15).

公开(公告)号：EP2423340B1

公开(公告)日：2018-07-18

申请号：EP11179093.7

申请日：2011-08-26

申请人： United Technologies Corporation

发明人： Das, Gopal

IPC分类号： C22C14/00 ,  C22F1/18 ,  B21K3/04 ,  B23H7/00 ,  B26D1/00 ,  B26F3/00 ,  B30B11/00 ,  F01D5/00 ,  B23P15/02

CPC分类号： C22C14/00 ,  B21J1/00 ,  B21J1/02 ,  B21J1/06 ,  B21J5/002 ,  B21K3/04 ,  B23H1/00 ,  B23P15/02 ,  C22B9/04 ,  C22B9/20 ,  C22B34/1295 ,  C22F1/183

摘要： A process for manufacturing a turbine engine component (10) comprises the steps of: casting ingots made of a gamma TiAl material using a double vacuum arc remelting casting technique; subjecting the cast ingots to a hot isostatic pressing to close porosity; forming at least one pancake of the gamma TiAl material by isothermally forging the hot isostatic pressed ingots; sectioning each pancake into a plurality of blanks; heat treating the blanks to produce a desired microstructure and mechanical properties; and machining the blanks into finished turbine engine components (10). A system for performing the process is also disclosed.

公开(公告)号：EP3099833B1

公开(公告)日：2018-06-27

申请号：EP15703208.7

申请日：2015-01-27

申请人： Titanium Metals Corporation

发明人： THOMAS, Roger ,  KOSAKA, Yoji ,  JAMES, Steven ,  GARRATT, Paul

IPC分类号： C22C14/00 ,  C22F1/18

CPC分类号： C22F1/183 ,  C22C14/00 ,  F04D29/023 ,  F04D29/522

摘要： Titanium alloys formed into a part or component used in applications where a key design criterion is the energy absorbed during deformation of the part when exposed to impact, explosive blast, and/or other forms of shock loading is described. The titanium alloys generally comprise a titanium base with added amounts of aluminum, an isomorphous beta stabilizing element such as vanadium, a eutectoid beta stabilizing element such as silicon and iron, and incidental impurities. The titanium alloys exhibit up to 70% or more improvement in ductility and up to a 16% improvement in ballistic impact resistance over a Ti-6Al-4V alloy, as well as absorbing up to 50% more energy than the Ti-6Al-4V alloy in Charpy impact tests. A method of forming a part that incorporates the titanium alloys and uses a combination of recycled materials and new materials is also described.

公开(公告)号：EP3333274A1

公开(公告)日：2018-06-13

申请号：EP16835206.0

申请日：2016-08-10

申请人： Meidensha Corporation

发明人： ISHIKAWA, Keita ,  YAMAMURA, Kenta ,  HASEGAWA, Kosuke ,  HAYASHI, Shota ,  FURUHATA, Takaaki

IPC分类号： C22C1/04 ,  B22F3/26 ,  C22C5/04 ,  C22C9/00 ,  C22C9/10 ,  C22C14/00 ,  C22C16/00 ,  C22C25/00 ,  C22C27/02 ,  C22C27/04 ,  C22C27/06 ,  C22C30/02 ,  H01H33/662 ,  H01H33/664

CPC分类号： H01H1/0206 ,  B22F3/26 ,  B22F2301/20 ,  B22F2304/10 ,  C22C1/04 ,  C22C5/04 ,  C22C9/00 ,  C22C9/10 ,  C22C14/00 ,  C22C16/00 ,  C22C25/00 ,  C22C27/02 ,  C22C27/04 ,  C22C27/06 ,  C22C30/02 ,  H01H11/048 ,  H01H33/662 ,  H01H33/664

摘要： It is an electrode material that is used as an electrode contact of a vacuum interrupter and that contains one or more parts by weight of a heat-resistant element and one part by weight of Cr, the remainder being Cu and an unavoidable impurity. A part of Cr powder and the heat-resistant element powder are mixed together, and this mixed powder is sintered such that a peak corresponding to Cr element disappears in X-ray diffraction measurement. A solid solution powder obtained by pulverizing a sintered body of the heat-resistant element and Cr obtained by the sintering is mixed with the remaining Cr powder, and this mixed powder is shaped and then sintered. A sintered body obtained by this sintering is infiltrated with Cu.

公开(公告)号：EP3330077A1

公开(公告)日：2018-06-06

申请号：EP16830625.6

申请日：2016-07-29

申请人： Nippon Steel & Sumitomo Metal Corporation

发明人： KITAURA, Tomoyuki ,  SHIRAI, Yoshihisa ,  FUJII, Hideki

IPC分类号： B32B15/01 ,  B23K20/00 ,  B32B3/26 ,  C22C14/00 ,  B21B1/02 ,  B21B3/00

CPC分类号： C22C14/00 ,  B21B1/02 ,  B21B1/22 ,  B21B3/00 ,  B21B2001/225 ,  B23K20/00 ,  B32B3/26 ,  B32B15/01

摘要： Provided is a titanium composite material 1 including: a first surface layer portion 2; an inner layer portion 4; and a second surface layer portion 3; wherein: the first surface layer portion 2 and the second surface layer portion 3 are composed of a titanium alloy; the inner layer portion 4 is composed of a commercially pure titanium including pores; a thickness of at least one of the first surface layer portion 2 and the second surface layer portion 3 is 2 µm or more, and a proportion of the thickness with respect to an overall thickness of the titanium composite material 1 is 40% or less; and a porosity in a cross section perpendicular to a sheet thickness direction is more than 0% and 30% or less.