公开(公告)号：US20180154580A1

公开(公告)日：2018-06-07

申请号：US15829486

申请日：2017-12-01

申请人： MARKFORGED, INC.

发明人： Gregory Thomas Mark

IPC分类号： B29C64/40 ,  B33Y70/00 ,  B33Y10/00 ,  B33Y40/00 ,  B29C64/165 ,  B22F3/00

CPC分类号： B29C64/165 ,  B22D11/01 ,  B22F1/0059 ,  B22F1/0085 ,  B22F3/008 ,  B22F3/1021 ,  B22F3/1055 ,  B22F3/1146 ,  B22F3/24 ,  B22F5/10 ,  B22F2003/1046 ,  B22F2003/1056 ,  B22F2003/1057 ,  B22F2003/1058 ,  B22F2003/244 ,  B22F2005/103 ,  B22F2998/10 ,  B22F2999/00 ,  B29C64/00 ,  B29C64/118 ,  B29C64/153 ,  B29C64/209 ,  B29C64/40 ,  B29K2103/06 ,  B29K2505/00 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y40/00 ,  B33Y50/02 ,  B33Y70/00 ,  B22F3/10 ,  B22F3/003

摘要： To build a part with a deposition-based additive manufacturing system using a polymer-based binder of a composite feedstock, a first tool path of a perimeter contour segment and a second tool path that is parallel and adjacent are deposited in retrograde directions to produce stress-offsetting adjacent paths, where directions of residual stress within the polymer-based binder of the composite are opposite in the stress-offsetting adjacent path.

公开(公告)号：US09988951B2

公开(公告)日：2018-06-05

申请号：US15104512

申请日：2014-12-16

申请人： Bleistahl-Produktions GmbH & Co KG

发明人： Ingwar Hunsche ,  Christian Blecking ,  Ekkehard Kohler ,  Dirk Emde

IPC分类号： F01L3/08 ,  B22F5/10 ,  F01L3/02 ,  B22F3/11 ,  B22F3/26 ,  B22F7/06 ,  C22C33/02 ,  C22C38/00 ,  B22F3/03 ,  B23K20/12 ,  C22C38/04 ,  C22C38/20 ,  C22C38/60

CPC分类号： F01L3/08 ,  B22F3/03 ,  B22F3/11 ,  B22F3/26 ,  B22F5/10 ,  B22F5/106 ,  B22F7/062 ,  B22F2005/103 ,  B22F2301/35 ,  B22F2998/10 ,  B23K20/129 ,  C22C33/0278 ,  C22C38/00 ,  C22C38/008 ,  C22C38/04 ,  C22C38/20 ,  C22C38/60 ,  F01L3/02 ,  B22F3/02 ,  B22F3/10

摘要： The invention relates to a valve guide manufactured by a powder-metallurgical process for combustion engines, said guide comprising a central section, a cam-side end piece, and a duct-side end piece, wherein the central section consists of a first material and the duct-side end piece of a second material, with the second material having a hardness in excess of 70 HRB and the first material having a hardness that is by at least 10 HRB lower than that of the second material.

公开(公告)号：US20170197284A1

公开(公告)日：2017-07-13

申请号：US14994351

申请日：2016-01-13

申请人： United Technologies Corporation

发明人： Wendell V. Twelves, JR. ,  Evan Butcher ,  John P. Rizzo, JR.

IPC分类号： B23P15/02

CPC分类号： B23P15/02 ,  B22F3/1055 ,  B22F5/009 ,  B22F5/10 ,  B22F2003/247 ,  B22F2005/103 ,  B22F2998/10 ,  B23D61/185 ,  B26D1/547 ,  B26D1/553 ,  Y02P10/295

摘要： A method of removing partially sintered powder from an internal passage in a metal component formed by electron beam additive manufacturing (EBAM) includes co-forming a solid wire cutter in the passage during the EBAM forming process and removing partially sintered powder from the cavity by extracting the cutter from the cavity.

公开(公告)号：US20170173681A1

公开(公告)日：2017-06-22

申请号：US14972440

申请日：2015-12-17

申请人： General Electric Company

发明人： Timothy Michael Moricca ,  Stephen Francis Rutkowski ,  Stanley Frank Simpson ,  Joseph Leonard Moroso

IPC分类号： B22D25/02 ,  B22C9/10 ,  B23K26/342 ,  B22D21/02 ,  B22F3/105 ,  B22C1/00 ,  B22C9/24

CPC分类号： B22D25/02 ,  B22C1/00 ,  B22C9/101 ,  B22C9/108 ,  B22C9/24 ,  B22D21/022 ,  B22D21/025 ,  B22F3/1055 ,  B22F5/009 ,  B22F5/04 ,  B22F2999/00 ,  B23K26/342 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  Y02P10/292 ,  Y02P10/295 ,  B22F2005/103

摘要： A method of forming a component having an internal passage defined therein is provided. The method includes positioning a jacketed core with respect to a mold. The jacketed core includes a hollow structure formed at least partially by an additive manufacturing process, and an inner core disposed within the hollow structure. The method also includes introducing a component material in a molten state into a cavity of the mold, and cooling the component material in the cavity to form the component. The inner core is positioned to define the internal passage within the component.

公开(公告)号：US20170022831A9

公开(公告)日：2017-01-26

申请号：US14687173

申请日：2015-04-15

申请人： Pratt & Whitney Canada Corp.

发明人： ERIC DUROCHER ,  GUY LEFEBVRE

IPC分类号： F01D9/04 ,  B22F3/22 ,  B22F3/00 ,  B22F5/00 ,  B22F3/10

CPC分类号： F01D9/04 ,  B22F3/004 ,  B22F3/10 ,  B22F3/225 ,  B22F5/009 ,  B22F5/10 ,  B22F2005/103 ,  F01D11/24 ,  F05D2220/32 ,  F05D2230/22 ,  F05D2230/31 ,  F05D2230/40 ,  F05D2240/11 ,  F05D2260/20 ,  F05D2300/10 ,  F05D2300/17

摘要： A turbine shroud segment is metal injection molded (MIM) about a low melting point material insert. The low melting point material is dissolved using heat during the heat treatment cycle required for the MIM material, thereby leaving internal cooling passages in the MIM shroud segment without extra manufacturing operation.

摘要翻译： 涡轮机护罩段是关于低熔点材料插入件的金属注射模制（MIM）。 在MIM材料所需的热处理循环期间，使用热量溶解低熔点材料，从而在MIM护套段内留下内部冷却通道，而无需额外的制造操作。

公开(公告)号：US20170001340A1

公开(公告)日：2017-01-05

申请号：US15125885

申请日：2015-05-26

申请人： BRIDGESTONE CORPORATION

发明人： Tomo KOYANAGI

IPC分类号： B29C35/02 ,  B29D30/08

CPC分类号： B29C35/02 ,  B22F3/1055 ,  B22F5/007 ,  B22F7/06 ,  B22F2005/103 ,  B29C33/02 ,  B29C33/04 ,  B29C33/048 ,  B29C33/3828 ,  B29C2033/023 ,  B29C2035/0838 ,  B29D30/0606 ,  B29D30/0662 ,  B29D30/08 ,  B29K2995/0015 ,  B33Y10/00 ,  B33Y80/00 ,  Y02P10/292 ,  Y02P10/295

摘要： A mold capable of imparting an appropriate amount of heat depending on a part of an object to be heated, the mold for transferring heat to the object to be heated is provided with a hollow portion inside the mold, and a heat amount adjusting agent, which is accommodated in the hollow portion, for changing heat transfer property of the hollow portion, in which the heat amount adjusting agent is made of a powdery or granular material having a material property different from a material property of the mold.

摘要翻译： 一种能够根据被加热物的一部分赋予适量热量的模具，将热量传递给待加热物体的模具在模具内部设置有中空部分和热量调节剂，其中， 容纳在中空部分中，用于改变中空部分的传热性能，其中热量调节剂由具有与模具的材料性质不同的材料性质的粉末或颗粒材料制成。

公开(公告)号：US09375787B2

公开(公告)日：2016-06-28

申请号：US13637084

申请日：2011-03-22

申请人： Ingo Smaglinski ,  Gerhard Himmelsbach ,  Thomas Petigk

发明人： Ingo Smaglinski ,  Gerhard Himmelsbach ,  Thomas Petigk

IPC分类号： B22F5/10 ,  G02B6/42 ,  B22F3/22

CPC分类号： B22F5/10 ,  B22F3/225 ,  B22F5/106 ,  B22F2005/103 ,  G02B6/4248

摘要： The present invention relates to a method for producing a leadthrough for an optical conductor (V3) in a housing part, comprising the following steps: a) producing granules composed of metal powder and, if appropriate binder, b) providing a mold having a mold space, c) injecting or compressing the granules into the mold in order to produce a molding, d) sintering the molding, e) introducing a passage opening into the molding prior to sintering, f) inserting a tube (V2) into the passage opening prior to sintering, and g) leading the optical conductor through the tube after sintering.

摘要翻译： 本发明涉及一种用于在壳体部分中制造用于光导体（V3）的引线的方法，包括以下步骤：a）生产由金属粉末组成的颗粒，如果合适的话粘合剂，b）提供具有模具的模具 空间，c）将颗粒注入或压缩到模具中以产生模制品，d）烧结模制件，e）在烧结之前将通道开口引入模制件，f）将管（V2）插入通道开口 在烧结之前，g）在烧结之后引导光导体通过管。

公开(公告)号：US09366140B2

公开(公告)日：2016-06-14

申请号：US14141976

申请日：2013-12-27

申请人： Rolls-Royce Corporation

发明人： Adam Lee Chamberlain

IPC分类号： C04B41/91 ,  F01D5/00 ,  C04B35/571 ,  C04B35/573 ,  C04B35/80 ,  C04B37/02 ,  F01D5/28 ,  B28B1/42 ,  B28B21/48 ,  C22C1/04 ,  B22F5/10

CPC分类号： F01D5/005 ,  B22F2005/103 ,  B22F2999/00 ,  B28B1/42 ,  B28B21/48 ,  C04B35/571 ,  C04B35/573 ,  C04B35/803 ,  C04B35/806 ,  C04B37/023 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/6028 ,  C04B2235/614 ,  C04B2235/616 ,  C04B2237/30 ,  C04B2237/363 ,  C04B2237/38 ,  C04B2237/40 ,  C04B2237/402 ,  C04B2237/404 ,  C04B2237/405 ,  C22C1/04 ,  C22C1/0416 ,  F01D5/282 ,  F01D5/284 ,  F05D2300/6033 ,  Y02T50/672 ,  Y10T156/10 ,  Y10T156/1028 ,  Y10T428/20 ,  B22F5/04 ,  B22F2201/00

摘要： A method for modifying a ceramic matrix component is disclosed including identifying a non-conforming region of a composite component capable of operating in a gas turbine engine; removing at least a portion of the non-conforming region to create an exposed surface of the composite component; preparing a preform in response to the removing at least a portion of the non-conforming region; applying a reactive constituent surface region to at least one of the exposed surface of the composite component and the preform, the reactive constituent surface region being capable of producing a non-equilibrium condition; positioning the preform to provide a contact region between the exposed surface of the composite component and the preform proximate the reactive constituent surface region; and reacting the reactive constituent surface region in an equilibrium reaction at the contact region to form a bond structure between the exposed surface of the composite component and the preform.

摘要翻译： 公开了一种用于改变陶瓷基体组分的方法，包括鉴定能够在燃气涡轮发动机中操作的复合部件的不合格区域; 去除所述不合格区域的至少一部分以产生所述复合部件的暴露表面; 响应于去除所述不合格区域的至少一部分而制备预成型件; 将反应性构成表面区域施加到复合构件的暴露表面和预成型体中的至少一个上，反应性构成表面区域能够产生非平衡条件; 定位预成型件以在复合部件的暴露表面和接近反应性构件表面区域的预成型件之间提供接触区域; 并使反应性组分表面区域在接触区域处的平衡反应中反应，以在复合组分的暴露表面和预型体之间形成结合结构。

公开(公告)号：US09328620B2

公开(公告)日：2016-05-03

申请号：US14141956

申请日：2013-12-27

申请人： Rolls-Royce Corporation

发明人： Andrew Joseph Lazur ,  Adam Lee Chamberlain

IPC分类号： C04B35/00 ,  B29C33/52 ,  F01D5/28 ,  C04B35/571 ,  C04B35/573 ,  C04B35/80 ,  C04B37/02 ,  B28B1/42 ,  B28B21/48 ,  C04B35/565 ,  F16D69/02 ,  B22F5/10 ,  C22C1/04

CPC分类号： F01D5/282 ,  B22F2005/103 ,  B22F2999/00 ,  B28B1/42 ,  B28B21/48 ,  B29C33/52 ,  C04B35/565 ,  C04B35/571 ,  C04B35/573 ,  C04B35/803 ,  C04B35/806 ,  C04B37/023 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/6028 ,  C04B2235/614 ,  C04B2235/616 ,  C04B2237/30 ,  C04B2237/363 ,  C04B2237/38 ,  C04B2237/40 ,  C04B2237/402 ,  C04B2237/404 ,  C04B2237/405 ,  C22C1/04 ,  C22C1/0416 ,  C22C19/03 ,  C22C21/02 ,  C22C28/00 ,  F01D5/284 ,  F05D2300/6033 ,  F16D69/023 ,  F16D2200/0052 ,  Y10T156/1028 ,  B22F5/04 ,  B22F2201/00

摘要： A method for making a gas turbine engine matrix composite structure. The method includes providing at least one metal core element, fabricating a matrix composite component about the metal core element, and removing at least part of the metal core element from the matrix composite component by introduction of a halogen gas.

摘要翻译： 一种制造燃气轮机发动机基体复合结构的方法。 该方法包括提供至少一个金属芯元件，围绕金属芯元件制造基体复合元件，并通过引入卤素气体从基质复合元件中去除至少部分金属芯元件。

公开(公告)号：US20160115820A1

公开(公告)日：2016-04-28

申请号：US14895976

申请日：2014-06-06

申请人： GENERAL ELECTRIC COMPANY

发明人： Ian Francis PRENTICE ,  Eric Allen OTT ,  Andrew Philip WOODFIELD

IPC分类号： F01D25/00 ,  F01D9/02 ,  B05D1/02

CPC分类号： F01D25/005 ,  B05D1/02 ,  B22C9/108 ,  B22D23/003 ,  B22D29/001 ,  B22F3/115 ,  B22F5/009 ,  B22F5/04 ,  B22F5/10 ,  B22F2005/103 ,  F01D5/147 ,  F01D5/288 ,  F01D9/02 ,  F05D2220/36 ,  F05D2230/22 ,  F05D2230/31 ,  Y02T50/672 ,  Y02T50/673

摘要： A method of making a hollow metal component comprising the steps of providing at least one core comprising a first side and a reverse side; utilizing a first metal spray process to apply at least one metal or metal alloy to the first side of the core, resulting in a partially-formed structure comprising a first side and a reverse side; and utilizing a second metal spray process to apply at least one metal or metal alloy to the reverse sides of the partially-formed structure and the core, resulting in a rough structure. A hollow metal component comprising a first side having interior and exterior surfaces, a reverse side having interior and exterior surfaces, the interior surfaces of the first side and the reverse side defining at least one cavity. The component is integrally formed and has regions comprising relatively different material compositions, the regions having gradual transitions of materials therebetween.

摘要翻译： 一种制造中空金属部件的方法，包括以下步骤：提供包括第一侧和反面的至少一个芯; 利用第一金属喷涂工艺将至少一种金属或金属合金施加到芯的第一侧，从而形成包括第一侧和反面的部分形成的结构; 并且利用第二金属喷涂工艺将至少一种金属或金属合金施加到部分形成的结构和芯的相反侧，导致粗糙的结构。 一种中空金属部件，包括具有内表面和外表面的第一侧面，具有内表面和外表面的反面，第一侧面和后侧的内表面限定至少一个空腔。 该部件是整体形成的并且具有包括相对不同材料组成的区域，该区域之间具有材料的逐渐过渡。