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公开(公告)号：EP3354766B1
公开(公告)日：2020-01-22
申请号：EP18153751.5
申请日：2018-01-26
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公开(公告)号：EP3187281A1
公开(公告)日：2017-07-05
申请号：EP16206050.3
申请日：2016-12-22
摘要： A dynamic compaction process comprising providing (200) a container (20;118) having a cylinder shape; filling said container (20;118) with a first powder material (16;110;114); and dynamically compacting (210) said first powder material (16; 110; 114). Aerospace component manufactured by dynamic compaction.
摘要翻译： 一种强力压实方法，包括提供（200）具有圆柱形状的容器（20; 118） 用第一粉末材料（16; 110; 114）填充所述容器（20; 118）; 并且动态地压实（210）所述第一粉末材料（16; 110; 114）。 航空零部件由强力压实生产。
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公开(公告)号：EP3187284B1
公开(公告)日：2020-02-05
申请号：EP16206426.5
申请日：2016-12-22
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公开(公告)号：EP2809884B1
公开(公告)日：2019-11-13
申请号：EP13743677.0
申请日：2013-01-10
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公开(公告)号：EP3047043A1
公开(公告)日：2016-07-27
申请号：EP14846311.0
申请日：2014-09-05
CPC分类号： C22C1/0416 , B22F3/14 , B22F3/20 , B22F3/24 , B22F2998/10 , C22C1/0491 , C22C21/00 , C22F1/04 , B22F9/082 , B22F2003/145
摘要： Dispersion strengthened aluminum-cerium-manganese alloys containing from about 0.05 to about 23.0 weight percent cerium and about 0.03 to about 9.5 weight percent manganese exhibit mechanical properties that make them useful alloys as a result of age hardening for extended periods at temperatures between 350° C (662° F) and 450° C (842° F).
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公开(公告)号：EP3019638B1
公开(公告)日：2020-03-18
申请号：EP14822973.5
申请日：2014-07-09
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公开(公告)号：EP3187284A1
公开(公告)日：2017-07-05
申请号：EP16206426.5
申请日：2016-12-22
摘要： A dynamic compaction process comprising providing a container (22; 116) having a non-cylindrical shape; filling said container (22; 116) with a first powder material (18; 110, 114); sealing the container (22; 116) and dynamically compacting said first powder material (18; 110, 114).
摘要翻译： 一种强力压实方法，包括提供具有非圆柱形形状的容器（22; 116） 用第一粉末材料（18; 110,114）填充所述容器（22; 116）; 密封容器（22; 116）并且动态地压实所述第一粉末材料（18; 110,114）。
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公开(公告)号：EP2901023A2
公开(公告)日：2015-08-05
申请号：EP13864424.0
申请日：2013-09-25
IPC分类号： F04D29/38
摘要： A fan blade includes first and second titanium portions that are secured to one another with an aluminum alloy braze. A method of manufacturing a fan blade includes providing first and second titanium portions, applying an aluminum alloy braze to at least one of the first and second titanium portions, and heating the fan blade to melt the aluminum alloy braze and join the first and second portions to one another to provide a fan blade with an airfoil exterior contour.
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公开(公告)号：EP3047043B1
公开(公告)日：2020-12-02
申请号：EP14846311.0
申请日：2014-09-05
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公开(公告)号：EP2867473B1
公开(公告)日：2020-07-29
申请号：EP13886385.7
申请日：2013-06-20
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