公开(公告)号：US20180016668A1

公开(公告)日：2018-01-18

申请号：US15644927

申请日：2017-07-10

申请人： MTU Aero Engines AG

发明人： Wilfried SMARSLY ,  Martin SCHLOFFER ,  Helmut CLEMENS ,  Thomas KLEIN

IPC分类号： C22F1/18 ,  C22C14/00

CPC分类号： C22F1/183 ,  C22C14/00 ,  C22C30/00

摘要： Described is α-TiAl alloy which, besides titanium, comprises 42 to 48 at. % aluminum, 3 to 5 at. % niobium, 0.05 to 1 at. % molybdenum, 0.2 to 2.2 at. % silicon, 0.2 to 0.4 at. % carbon, 0.05 to 0.2 at. % boron, and optionally tungsten, zirconium and hafnium, as well as unavoidable impurities, and at room temperature has a microstructure which comprises globular colonies of lamellae of α2-Ti3Al and γ-TiAl, as well as silicide precipitates, and essentially no β phase. A method for producing a component made of this alloy is also described.

公开(公告)号：US20170241271A1

公开(公告)日：2017-08-24

申请号：US15431925

申请日：2017-02-14

申请人： MTU Aero Engines AG

发明人： Markus FRIED ,  Wilfried SMARSLY ,  Andreas BROETZNER

IPC分类号： F01D5/28 ,  C22C30/00 ,  C23C14/16 ,  F01D9/02 ,  C23C14/58 ,  C23C16/42 ,  C23C16/38 ,  C23C16/56 ,  C22C27/04 ,  C23C14/34

CPC分类号： F01D5/28 ,  C22C27/04 ,  C22C30/00 ,  C23C10/04 ,  C23C10/28 ,  C23C14/165 ,  C23C14/34 ,  C23C14/5806 ,  C23C14/5853 ,  C23C16/38 ,  C23C16/42 ,  C23C16/56 ,  C23C28/321 ,  C23C28/322 ,  C23C28/34 ,  C23C28/345 ,  C23C28/36 ,  F01D9/02 ,  F05D2220/323 ,  F05D2230/313 ,  F05D2230/314 ,  F05D2230/40 ,  F05D2300/131 ,  Y02T50/6765

摘要： Disclosed is a method for improving the high-temperature stability of a component, in particular a blade of a turbomachine, formed at least partially from a molybdenum alloy that, besides molybdenum, silicon, boron and titanium, comprises iron and/or yttrium. The method comprises depositing a diffusion barrier layer formed from technically pure molybdenum or tungsten or being an alloy based on molybdenum and/or tungsten at least on an outer surface, which comprises the molybdenum alloy, of the component, and depositing silicon on the diffusion barrier layer to form molybdenum silicides and/or tungsten silicides.

公开(公告)号：US20170122118A1

公开(公告)日：2017-05-04

申请号：US15401483

申请日：2017-01-09

申请人： MTU Aero Engines AG

发明人： Erich STEINHARDT ,  Wilfried SMARSLY ,  André WERNER

IPC分类号： F01D5/30 ,  F01D5/02 ,  F01D5/12

CPC分类号： F01D5/3092 ,  F01D5/02 ,  F01D5/12 ,  F01D5/3007 ,  F05D2300/1723 ,  F05D2300/173 ,  F05D2300/174 ,  F05D2300/501 ,  F05D2300/505 ,  F05D2300/514 ,  F05D2300/518 ,  F05D2300/702 ,  Y02T50/6765

摘要： Disclosed is a blade element of a turbomachine, in particular of a gas turbine, which comprises a fastening element (10) with which the blade element is arranged in a receptacle (11) of the turbomachine. in the region of the fastening element, the blade element has a core region (18) and an envelope region (19) which at least partially envelops the core region. The core region is formed from a blade base material which is more brittle than the envelope material of the envelope region, and the envelope region is formed by a coating. The envelope material is a blade base material which has been modified to achieve a higher ductility or is a pseudoelastic or superelastic material.

公开(公告)号：US20180105901A1

公开(公告)日：2018-04-19

申请号：US15782974

申请日：2017-10-13

申请人： MTU Aero Engines AG

发明人： Wilfried SMARSLY ,  Markus FRIED

IPC分类号： C22C27/04 ,  C22C1/04 ,  C22C1/05 ,  B22F9/08 ,  B22F9/04

CPC分类号： C22C27/04 ,  B22F9/04 ,  B22F9/082 ,  B22F2009/043 ,  B22F2009/088 ,  B22F2301/20 ,  B22F2302/20 ,  C22C1/045 ,  C22C1/058 ,  C22C1/1084 ,  C22C32/0047

摘要： The invention relates to method of making a molybdenum alloy which has a high titanium content and further comprises silicon and/or boron. The method comprises subjecting to pressureless sintering or sintering under pressure in an inert gas atmosphere a mixture of one or more powders (i) of an alloy of Mo and Ti and, optionally, one or more additional metals X and/or (i′) powders of Mo and of TiN, and (ii) one or more powders comprising one or more powders of silicides of Mo and/or Ti and/or (iii) one or more powders of nitrides which comprise Si3N4 powder and/or BN powder.

公开(公告)号：US20170335436A1

公开(公告)日：2017-11-23

申请号：US15600864

申请日：2017-05-22

申请人： MTU Aero Engines AG

发明人： Martin SCHLOFFER ,  Wilfried SMARSLY

IPC分类号： C22C14/00 ,  B22F3/15 ,  B33Y70/00 ,  B23K15/00 ,  B33Y10/00

CPC分类号： C22C14/00 ,  B22F3/1055 ,  B22F3/15 ,  B22F2998/10 ,  B23K15/0086 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C22C1/0416 ,  C22C1/0458 ,  C22C1/0491 ,  Y02P10/295

摘要： Disclosed is a process for producing a component from a TiAl alloy by layer-by-layer deposition of powder on a substrate and/or an already produced semifinished product. The component has a proportion of x at % of aluminum which is in the range from about 34 to about 47 at % of aluminum, the powder having a proportion of x+1 at % to x+6 at % of aluminum. Also disclosed is a component formed from a Tim alloy which has been produced by a corresponding process.

公开(公告)号：US20160273368A1

公开(公告)日：2016-09-22

申请号：US15067430

申请日：2016-03-11

申请人： MTU Aero Engines AG

发明人： Wilfried SMARSLY ,  Markus FRIED

IPC分类号： F01D5/28 ,  B23K20/02 ,  B23K20/12 ,  B23K13/01 ,  B23K15/00 ,  B22F5/04 ,  B23K26/323 ,  B23K20/22 ,  B22F3/15 ,  B22F3/04 ,  B22F3/10 ,  B22F3/14 ,  C22C27/04 ,  B23K26/21

CPC分类号： C22C1/045 ,  B22F3/04 ,  B22F3/10 ,  B22F3/1039 ,  B22F3/12 ,  B22F3/14 ,  B22F3/15 ,  B22F3/17 ,  B22F3/18 ,  B22F3/20 ,  B22F3/24 ,  B22F5/04 ,  B22F2003/175 ,  B22F2301/20 ,  B22F2998/10 ,  B23K13/01 ,  B23K15/0093 ,  B23K20/02 ,  B23K20/12 ,  B23K20/22 ,  B23K26/21 ,  B23K26/323 ,  B23K2101/001 ,  B23K2103/18 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C22C1/0491 ,  C22C27/04 ,  C22C30/00 ,  F01D5/282 ,  F01D5/286 ,  F01D5/288 ,  F05D2230/22 ,  F05D2230/233 ,  F05D2230/234 ,  F05D2230/236 ,  F05D2230/239 ,  F05D2230/25 ,  F05D2230/42 ,  F05D2300/13 ,  F05D2300/131 ,  F05D2300/172 ,  F05D2300/177 ,  F05D2300/222 ,  Y02T50/672 ,  Y02T50/6765

摘要： The present invention relates to a blade for a turbomachine, in particular for an aircraft engine, which comprises a blade root (2) for arranging the blade (1) in the turbomachine and a main blade part (3) for interaction with a fluid flowing through the turbomachine, the blade root and the main blade part being formed from different materials and the main blade part being formed from a metal-intermetallic composite material. The metal matrix, in which intermetallic phases are incorporated for forming the metal-intermetallic composite material, is formed by a molybdenum alloy. The invention also relates to a corresponding method for producing such a blade.

摘要翻译： 本发明涉及一种用于涡轮机的叶片，特别是用于飞行器发动机，其包括用于将叶片（1）布置在涡轮机中的叶根（2）和用于与流体流动相互作用的主叶片部分（3） 通过涡轮机，叶片根部和主叶片部分由不同的材料形成，主叶片部分由金属 - 金属间复合材料形成。 通过钼合金形成用于形成金属 - 金属间复合材料的金属间相的金属基体。 本发明还涉及用于生产这种叶片的相应方法。

公开(公告)号：US20160060734A1

公开(公告)日：2016-03-03

申请号：US14835866

申请日：2015-08-26

申请人： MTU Aero Engines AG

发明人： Wilfried SMARSLY ,  Markus FRIED

IPC分类号： C22C27/04

CPC分类号： C22C27/04

摘要： The present invention relates to a quaternary or multinary molybdenum alloy for the production of structural components, in particular of vanes of a turbomachine having the main constituents molybdenum, silicon, boron and titanium, which, as minor alloying elements, additionally comprises at least one of iron and yttrium.

摘要翻译： 本发明涉及一种用于生产结构部件，特别是具有主要成分钼，硅，硼和钛的涡轮机的叶片的四元或多元钼合金，其作为次要合金元素另外包含以下各项中的至少一种： 铁和钇。

公开(公告)号：US20170145837A1

公开(公告)日：2017-05-25

申请号：US15351797

申请日：2016-11-15

申请人： MTU Aero Engines AG

发明人： Martin SCHLOFFER ,  Wilfried SMARSLY

IPC分类号： F01D5/30

CPC分类号： F01D5/3061 ,  B23K20/1205 ,  B23K20/129 ,  B23K20/16 ,  B23K20/233 ,  B23K26/342 ,  B23K2101/001 ,  B23K2103/14 ,  B23K2103/18 ,  B23K2103/26 ,  F01D5/147 ,  F01D5/18 ,  F01D5/34 ,  F05D2220/323 ,  F05D2230/234 ,  F05D2230/236 ,  F05D2230/239 ,  F05D2230/31 ,  F05D2230/40 ,  F05D2230/42 ,  F05D2230/50 ,  F05D2300/174 ,  Y02T50/672

摘要： A method of making a bladed rotor for a turbomachine, in particular for an aircraft engine, is disclosed. The method comprises the steps a) providing a rotor base of the rotor, b) providing at least one blade root, c) providing at least one blade body, d) making at least one blade by connecting the blade body to the blade root by means of a diffusion barrier layer, at least the blade body, the diffusion barrier layer and the blade root consisting of respectively different materials, and e) joining the at least one blade root to the rotor base. The invention furthermore relates to a bladed rotor and to a turbomachine having such a bladed rotor.

公开(公告)号：US20160376689A1

公开(公告)日：2016-12-29

申请号：US15191038

申请日：2016-06-23

申请人： MTU Aero Engines AG

发明人： Martin SCHLOFFER ,  Wilfried SMARSLY ,  Marc HALTRICH

IPC分类号： C22F1/18 ,  B21K3/04 ,  B22D13/04 ,  B21J5/00 ,  C22C14/00 ,  B22D21/00

CPC分类号： C22F1/183 ,  B21J5/002 ,  B21K3/04 ,  B22D13/023 ,  B22D13/04 ,  B22D13/066 ,  B22D13/101 ,  B22D21/005 ,  C22C14/00

摘要： An apparatus and a process for producing forged components composed of TiAl alloys, wherein a melt of a TiAl alloy is provided and is cast by horizontal centrifugal casting so as to produce at least one semifinished TiAl cast part and the semifinished TiAl cast part is converted by forging into a forged TiAl part.

摘要翻译： 一种用于生产由TiAl合金组成的锻造部件的设备和方法，其中提供TiAl合金的熔体并通过水平离心铸造铸造，以便产生至少一个半成品的TiAl铸造部件，并且将半成品的TiAl铸造部件转化为 锻造成锻造TiAl零件。

公开(公告)号：US20160273074A1

公开(公告)日：2016-09-22

申请号：US15066186

申请日：2016-03-10

申请人： MTU Aero Engines AG

发明人： Wilfried SMARSLY ,  Markus FRIED

IPC分类号： C22C1/04 ,  B22F3/24 ,  B22F3/17 ,  C22C30/00 ,  B22F3/20 ,  B22F3/15 ,  B22F3/14 ,  C22C27/04 ,  B22F3/12 ,  B22F3/18

CPC分类号： C22C1/045 ,  B22F3/04 ,  B22F3/10 ,  B22F3/1039 ,  B22F3/12 ,  B22F3/14 ,  B22F3/15 ,  B22F3/17 ,  B22F3/18 ,  B22F3/20 ,  B22F3/24 ,  B22F5/04 ,  B22F2003/175 ,  B22F2301/20 ,  B22F2998/10 ,  B23K13/01 ,  B23K15/0093 ,  B23K20/02 ,  B23K20/12 ,  B23K20/22 ,  B23K26/21 ,  B23K26/323 ,  B23K2101/001 ,  B23K2103/18 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C22C1/0491 ,  C22C27/04 ,  C22C30/00 ,  F01D5/282 ,  F01D5/286 ,  F01D5/288 ,  F05D2230/22 ,  F05D2230/233 ,  F05D2230/234 ,  F05D2230/236 ,  F05D2230/239 ,  F05D2230/25 ,  F05D2230/42 ,  F05D2300/13 ,  F05D2300/131 ,  F05D2300/172 ,  F05D2300/177 ,  F05D2300/222 ,  Y02T50/672 ,  Y02T50/6765

摘要： The present invention relates to a method for producing a component of a composite material comprising a metal matrix and incorporated intermetallic phases, which method comprises providing powders of at least one member of the group which comprises pure chemical elements, alloys, chemical compounds and material composites, the powder corresponding overall to the chemical composition which the composite material to be produced is intended to have, each individual powder being different to the chemical composition of the composite material to be produced, compacting the powders, bonding the powders to one another to form a unit and thermoplastically shaping the unit.

摘要翻译： 本发明涉及一种用于涡轮机的叶片，特别是用于飞行器发动机，其包括用于将叶片（1）布置在涡轮机中的叶根（2）和用于与流体流动相互作用的主叶片部分（3） 通过涡轮机，叶片根部和主叶片部分由不同的材料形成，主叶片部分由金属 - 金属间复合材料形成。 通过钼合金形成用于形成金属 - 金属间复合材料的金属间相的金属基体。 本发明还涉及用于生产这种叶片的相应方法。