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公开(公告)号：EP3442741A1
公开(公告)日：2019-02-20
申请号：EP17720201.7
申请日：2017-04-10
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公开(公告)号：EP3442741B1
公开(公告)日：2020-10-21
申请号：EP17720201.7
申请日：2017-04-10
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公开(公告)号：EP2834382B1
公开(公告)日：2018-08-08
申请号：EP13720454.1
申请日：2013-04-05
申请人： Safran Aircraft Engines , Centre National de la Recherche Scientifique , Université de Bordeaux 1 , Institut Polytechnique de Bordeaux
发明人： FRANCHET, Jean-Michel Patrick Maurice , KLEIN, Gilles Charles Casimir , SANCHEZ, Gérald , LEPETITCORPS, Yann , ARQUIS, Eric , VERMAUT, Delphine
IPC分类号： C04B41/90 , C04B35/628 , C23C2/02 , C23C2/26 , C23C2/38 , C04B35/565 , C04B41/88 , C23C2/00 , C04B41/00 , C04B41/45 , C04B41/52 , C23C2/04 , C22C47/04 , C22C49/14 , C04B111/00
CPC分类号： C04B41/4523 , C04B35/565 , C04B35/62863 , C04B35/62873 , C04B35/62876 , C04B35/62894 , C04B35/62897 , C04B41/009 , C04B41/4584 , C04B41/52 , C04B41/88 , C04B41/90 , C04B2111/00922 , C04B2235/5244 , C04B2235/5248 , C22C47/04 , C22C49/14 , C23C2/003 , C23C2/02 , C23C2/04 , C23C2/26 , C23C2/38 , C04B41/5001 , C04B41/4558 , C04B41/5061 , C04B41/5133 , C04B14/4693
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公开(公告)号：EP2834382A1
公开(公告)日：2015-02-11
申请号：EP13720454.1
申请日：2013-04-05
申请人： SNECMA , Centre National de la Recherche Scientifique , Université de Bordeaux 1 , Institut Polytechnique de Bordeaux
发明人： FRANCHET, Jean-Michel Patrick Maurice , KLEIN, Gilles Charles Casimir , SANCHEZ, Gérald , LEPETITCORPS, Yann , ARQUIS, Eric , VERMAUT, Delphine
CPC分类号： C04B41/4523 , C04B35/565 , C04B35/62863 , C04B35/62873 , C04B35/62876 , C04B35/62894 , C04B35/62897 , C04B41/009 , C04B41/4584 , C04B41/52 , C04B41/88 , C04B41/90 , C04B2111/00922 , C04B2235/5244 , C04B2235/5248 , C22C47/04 , C22C49/14 , C23C2/003 , C23C2/02 , C23C2/04 , C23C2/26 , C23C2/38 , C04B41/5001 , C04B41/4558 , C04B41/5061 , C04B41/5133 , C04B14/4693
摘要： The invention concerns a method for depositing a coating of a first metal alloy on a fibre (10) extending in main direction D, comprising the following steps: (a) Providing a first mass (20) of a first metal alloy and heating the first mass (20) higher than the melting temperature of same so that said alloy is liquid and occupies space El, (b) Moving this fibre (10) from upstream to downstream through the first liquid mass (20) in the direction in which the fibre (10) extends at first speed VI such that the fibre (10) is covered, on at least one portion of the length of same, with a coating (25) of the first alloy of a non-zero thickness over the entire periphery of same in a plane perpendicular to main direction D. Before step (a), the following steps are carried out: (i) Providing a second mass (220) of a second metal alloy of which melting temperature TF2 is strictly higher than melting temperature TF1 of the first alloy, (j) Heating the second mass (220) higher than the melting temperature of same so that said second alloy is in the liquid state and occupies space E2, then moving the fibre (10) from upstream to downstream through the second alloy, this movement being carried out at second speed V2 which is such that the coating speed of the second alloy during this movement is in the visco-capillary range, such that the fibre (10) is covered on this portion of the length of same with a coating (225) of the second alloy of a non-zero thickness over the entire periphery of same, (k) Cooling this coating (225) until it becomes solid.
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5.发明公开PROCÉDÉ DE FABRICATION DE BOUCLIER DE BORD D'ATTAQUE 审中-公开PROCÉDÉDE FABRICATION DE BOUCLIER DE BORD D'ATTAQUE
公开(公告)号：EP3194112A1
公开(公告)日：2017-07-26
申请号：EP15778363.0
申请日：2015-09-18
发明人： KLEIN, Gilles Charles Casimir , FRANCHET, Jean-Michel Patrick Maurice , MAGNAUDEIX, Dominique Michel Serge
CPC分类号： B23K20/021 , B21D53/78 , B23K2201/001 , B23P15/04 , F01D5/147 , F01D5/282 , F04D29/023 , F04D29/324 , F05D2220/36 , F05D2230/233 , F05D2230/25 , F05D2230/42 , F05D2240/303 , F05D2300/133 , F05D2300/603
摘要： The invention relates to the field of rotary blades and more particularly to a method of manufacturing a leading edge shield intended to protect such a blade. This method involves at least the steps of initial plastic deformation of at least one sheet out of a pressure-face sheet (17) and a suction-face sheet (18), using additive manufacturing to add a reinforcer (15, 16) with fibrous insert (14) to at least one of said pressure-face and suction-face sheets (17, 18), closing said pressure face and suction-face sheets (17, 18) around a core (20), after said initial plastic deformation and the addition of each reinforcer (15, 16), subsequent plastic deformation, by compression against an external surface of the core (20) of said pressure-face and suction-face sheets (17, 18) after they have been closed around the core (20), and extracting the core (20).
摘要翻译： 本发明涉及旋转叶片领域，并且更具体地涉及制造旨在保护这种叶片的前缘护罩的方法。 该方法至少包括以下步骤：将至少一个片材从压力面片（17）和吸面片（18）中初始塑性变形，使用增材制造将增强剂（15,16）与纤维状 在所述初始塑性变形之后，将所述压力面和所述吸力面片（17,18）中的至少一个插入（14）至所述压力面和吸力面片（17,18）中的至少一个， 以及在所述压力面和吸力面片（17,18）围绕所述压力面和吸力面片（17,18）闭合之后，通过压靠在所述压力面和吸力面片（17,18）的芯（20）的外表面上而增加每个增强器 核心（20），并且提取核心（20）。
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