首页> 外国专利> Mold, used for manufacturing turbine casing of composite material, comprises primary and secondary rings, where primary rings have annular rails having outer contour that corresponds to inner profile of fastening systems of turbine casing

Mold, used for manufacturing turbine casing of composite material, comprises primary and secondary rings, where primary rings have annular rails having outer contour that corresponds to inner profile of fastening systems of turbine casing

机译:用于制造复合材料的涡轮机壳体的模具包括初级和次级环,其中初级环具有环形轨道,环形轨道的外轮廓对应于涡轮机壳体的紧固系统的内部轮廓

摘要

The mold comprises primary rings (504) axially offset from each other, and secondary rings (510) axially positioned between annular rails (506) of the primary rings. Each annular rail projects outwards, and has an outer contour that corresponds to an inner profile of fastening systems of a turbine casing to be manufactured. The casing comprises an annular cover. The fastening systems are fixed on an interior of the cover and axially spaced from each other. The secondary rings have an outer profile corresponding to an inner profile of the cover of the turbine casing to be manufactured. The mold comprises primary rings (504) axially offset from each other, and secondary rings (510) axially positioned between annular rails (506) of primary rings. Each annular rail projects outwards, and has an outer contour that corresponds to an inner profile of fastening systems of a turbine casing to be manufactured. The casing comprises an annular cover. The fastening systems are fixed on an interior of the cover, and are axially spaced from each other. The second rings have an outer profile corresponding to an inner profile of the cover of the turbine casing to be manufactured. The primary rings are independent from each other and axially placed end to end to form an even mold. Each primary ring comprises angular segments, which are tangentially placed end to end to form a single set of primary rings. The rails of the primary rings have a trapezoidal cross section. The secondary rings are made of inflatable bladders. An independent claim is included for a method for manufacturing a turbine casing of composite material.
机译:模具包括彼此轴向偏移的初级环(504)和轴向位于初级环的环形轨道(506)之间的次级环(510)。每个环形轨道向外突出,并且具有与要制造的涡轮机壳体的紧固系统的内部轮廓相对应的外部轮廓。壳体包括环形盖。紧固系统固定在盖的内部并且在轴向上彼此间隔开。次级环具有与要制造的涡轮机壳体的盖的内部轮廓相对应的外部轮廓。模具包括彼此轴向偏移的初级环(504)和轴向位于初级环的环形轨道(506)之间的次级环(510)。每个环形轨道向外突出,并且具有与要制造的涡轮机壳体的紧固系统的内部轮廓相对应的外部轮廓。壳体包括环形盖。紧固系统固定在盖的内部,并且在轴向上彼此间隔开。第二环具有与要制造的涡轮机壳体的盖的内部轮廓相对应的外部轮廓。主环彼此独立,并轴向首尾相连以形成均匀的模具。每个初级环包括角形段,该角形段首尾相切地放置以形成单个初级环组。主环的轨道具有梯形横截面。次级环由可充气的气囊制成。包括用于制造复合材料的涡轮机壳体的方法的独立权利要求。

著录项

  • 公开/公告号FR2993490A1

    专利类型

  • 公开/公告日2014-01-24

    原文格式PDF

  • 申请/专利权人 HERAKLES;SNECMA;

    申请/专利号FR20120056884

  • 发明设计人 FREMONT ELRIC;BEAUJARD ANTOINE;

    申请日2012-07-17

  • 分类号B29C70/24;B29C39/26;F01D25/24;

  • 国家 FR

  • 入库时间 2022-08-21 15:36:37

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