-
公开(公告)号：EP3640435A1
公开(公告)日：2020-04-22
申请号：EP19214582.9
申请日：2013-03-19
摘要： A hybrid airfoil (142) for a gas turbine engine comprises a leading edge portion (148), a trailing edge portion (150) and an intermediate portion (151) between said leading edge portion (148) and said trailing edge portion (150). The leading edge portion (148) is made of a first material, the trailing edge portion (150) is made of a second material, and the intermediate portion (151) is made of a third material. At least two of said first material, said second material and said third material are different materials. A a portion (115) between said leading edge portion and said intermediate portion includes a pocket (127) that receives a non-metallic portion (102A). A connection interface is established between said leading edge portion (148) and said non-metallic portion (102A).
-
公开(公告)号：EP3321472B1
公开(公告)日：2020-04-22
申请号：EP17201688.3
申请日：2017-11-14
-
3.发明授权
公开(公告)号：EP2969321B1
公开(公告)日：2019-05-01
申请号：EP14778329.4
申请日：2014-03-11
IPC分类号： B22F3/105 , B29C64/153 , B29C64/371 , B33Y30/00 , B33Y40/00
-
4.发明公开TOUGHENED BOND LAYER AND METHOD OF PRODUCTION 审中-公开VERSTÄRKTEHAFTVERMITTLUNGSSCHICHT UND VERFAHREN ZUR HERSTELLUNG
公开(公告)号：EP3059333A1
公开(公告)日：2016-08-24
申请号：EP16156050.3
申请日：2016-02-17
CPC分类号： C04B35/62222 , C23C4/073 , C23C4/11 , C23C4/18 , C23C14/22 , C23C24/085 , C23C28/3215 , C23C28/324 , C23C28/345 , C23C28/3455 , C23F1/04 , C23F4/00 , C25D13/02 , C25D13/22 , F01D5/288 , F05D2230/31 , F05D2230/90 , F05D2300/1723 , F05D2300/20 , F05D2300/614
摘要： According to one embodiment of this disclosure, a coating includes a plurality of elongated reinforcing materials 56. The coating includes a bond coat 58 in which a first portion of a first elongated reinforcing material is embedded. The coating further includes a ceramic coat 70 adjacent the bond coat in which a second portion of the first elongated reinforcing material is embedded.
摘要翻译： 根据本公开的一个实施例，涂层包括多个细长的增强材料56.涂层包括粘合涂层58，嵌入第一细长增强材料的第一部分。 涂层还包括邻近粘合涂层的陶瓷涂层70，其中第一细长增强材料的第二部分被嵌入其中。
-
5.发明公开ADDITIVE MANUFACTURE SYSTEM WITH A CONTAINMENT CHAMBER AND A LOW PRESSURE OPERATING ATMOSPHERE 审中-公开麻醉药物微生物研究所EINGRENZUNGSKAMMER UNDNIEDERDRUCKBETRIEBSATMOSPHÄRE
公开(公告)号：EP3028841A1
公开(公告)日：2016-06-08
申请号：EP15197346.8
申请日：2015-12-01
发明人： OTT, Joe , MIRONETS, Sergey
CPC分类号： B22F3/1055 , B22F2003/1056 , B22F2003/1057 , B22F2003/1059 , B22F2999/00 , B29C64/153 , B29C64/20 , B29C64/35 , B29C64/386 , B33Y10/00 , B33Y30/00 , B33Y40/00 , Y02P10/24 , Y02P10/295 , B22F2201/20
摘要： A additive manufacturing system (20) includes a containment housing (22) operable to form a containment chamber (34) with a low pressure operating atmosphere and an additive manufacturing build housing (24) within said containment housing (22).
摘要翻译： 添加剂制造系统（20）包括容纳壳体（22），其可操作以在所述容纳壳体（22）内形成具有低压操作气氛的容纳室（34）和添加剂制造构造壳体（24）。
-
6.发明公开ADDITIVE MANUFACTURING OF CERAMIC TURBINE COMPONENTS BY TRANSIENT LIQUID PHASE BONDING USING METAL OR CERAMIC BINDERS 审中-公开添加剂制造陶瓷涡轮部件BY临时液体相结合物使用金属或陶瓷关系
公开(公告)号：EP2989064A2
公开(公告)日：2016-03-02
申请号：EP14829417.6
申请日：2014-04-22
CPC分类号： C04B35/65 , B33Y10/00 , B33Y70/00 , C04B35/117 , C04B35/44 , C04B35/46 , C04B35/48 , C04B35/486 , C04B35/565 , C04B35/584 , C04B35/6303 , C04B35/6316 , C04B2235/3217 , C04B2235/3225 , C04B2235/3244 , C04B2235/3281 , C04B2235/3298 , C04B2235/3409 , C04B2235/3418 , C04B2235/386 , C04B2235/3865 , C04B2235/40 , C04B2235/402 , C04B2235/6026 , C04B2235/665 , C04B2235/764 , C04B2235/9653
摘要： A ceramic turbine component is formed by a process including mixing a ceramic powder with an inorganic binder powder. The powder mixture is then formed into a turbine component that is subsequently densified by transient liquid phase sintering. In an embodiment, the turbine component may be formed by an additive manufacturing process such as selective laser sintering.
摘要翻译： 一种陶瓷涡轮机部件是由一种方法，包括将陶瓷粉末与无机粉末的粘合剂混合形成。 然后将粉末混合物成形为涡轮机部件所做的是随后通过瞬间液相烧结致密化。 实施例在中，涡轮机组件可以通过在添加制造工艺形成：诸如选择性激光烧结。
-
公开(公告)号：EP2988888A1
公开(公告)日：2016-03-02
申请号：EP14787566.0
申请日：2014-04-25
CPC分类号： B22F3/1055 , B22F2003/1056 , B22F2003/1057 , B22F2201/20 , B23K15/0026 , B23K15/0086 , B23K15/06 , B23K26/03 , B23K26/342 , B29C64/153 , B29C64/20 , B33Y10/00 , B33Y30/00 , B33Y50/02 , H01J49/00 , Y02P10/295
摘要： An additive manufacturing system comprises a build chamber, a powder bed additive manufacturing device disposed in the build chamber, and a powder contamination detection system. The powder contamination detection system is in communication with an atmosphere in the build chamber.
-
公开(公告)号：EP2831377B1
公开(公告)日：2019-12-11
申请号：EP13817339.8
申请日：2013-03-19
-
公开(公告)号：EP3094436B1
公开(公告)日：2019-04-03
申请号：EP15736998.4
申请日：2015-01-16
-
公开(公告)号：EP2823085B1
公开(公告)日：2018-08-08
申请号：EP13790628.5
申请日：2013-02-19
发明人： MIRONETS, Sergey , NARDI, Aaron T.
CPC分类号： F01D5/286 , B22F5/04 , B22F7/06 , B64D2045/009 , C23C24/04 , F04D29/324 , F05D2240/303 , Y02T50/673 , Y10T29/49316
摘要： A method of forming a leading edge protection component includes depositing particles using a cold spray process on a mandrel to form a leading edge protection component; and removing the leading edge protection structure from the mandrel. The leading edge protection can be formed in one or more pieces and involve using one or more mandrels.
-
-
-
-
-
-
-
-
-
搜索结果
40 条记录 (耗时 0.015 秒)
