公开(公告)号：US20160327061A1

公开(公告)日：2016-11-10

申请号：US15110314

申请日：2015-01-08

Applicant: SNECMA ,  SAFRAN

Inventor： Robin MANDEL ,  Emilie GONCALVES ,  Benedicte LE BORGNE ,  Helene QUILLENT ,  Jean-Christophe RIETSCH

IPC: F04D29/58 ,  B29C65/02 ,  F04D29/02 ,  B29C65/48 ,  F04D29/52 ,  F04D29/64

CPC classification number: F04D29/5853 ,  B29C65/02 ,  B29C65/48 ,  B29L2031/7504 ,  F01D25/24 ,  F02C7/25 ,  F04D29/023 ,  F04D29/522 ,  F04D29/644 ,  F05B2220/303 ,  F05B2230/40 ,  F05B2230/60 ,  F05B2260/231 ,  F05B2280/6003 ,  F05B2280/6015 ,  F05D2300/601 ,  F05D2300/603 ,  Y02T50/672 ,  Y02T50/675 ,  Y02T50/6765

Abstract: The invention relates to a method for fire protection (S) of a part (1) of a gas-turbine engine made of a composite material comprising a main fibrous reinforcement compregnated by a main matrix, the protection method (S) comprising the following steps: preforming (S1) a panel of pre-preg (20) such as to grant same a shape corresponding to the shape of a surface (3) of the part (1) to be protected against fire, said panel of prepreg (20) comprising a secondary fibrous reinforcement compregnated by a secondary matrix; applying (S2) the panel of prepreg (20) thus preformed to the part (1); and securing (S3) the panel of prepreg (20) to the surface (3) by thermal treatment of the part (1) provided with said panel of prepreg (20) in order to obtain a fire-protection layer (2).

Abstract translation: 本发明涉及一种由复合材料制成的燃气涡轮发动机的部分（1）的防火方法，所述复合材料包括由主基体浸渍的主纤维增强材料，所述保护方法（S）包括以下步骤 ：预先形成（S1）预浸料（20）的面板，以便赋予相同于待保护的防止部件（1）的表面（3）形状的形状，所述预浸料坯（20） 包括由次级基体浸渍的次级纤维增强材料; 将预浸料坯（20）的面板（S2）施加（S2）从而预成型到部分（1）上; 并且通过对设置有所述预浸料坯（20）的面板的部分（1）进行热处理，将预浸料坯（20）的板固定（S3）到表面（3），以获得防火层（2）。

公开(公告)号：US20170023013A1

公开(公告)日：2017-01-26

申请号：US15105756

申请日：2014-12-17

Applicant: SNECMA

Inventor： Helene QUILLENT ,  Thomas LANGEVIN ,  Jean-Pierre Andre Joseph MOURLAN ,  Adrien PAIXAO ,  Francois SFARTI

IPC: F04D29/52 ,  F02C7/25 ,  F01D25/00 ,  B64D27/16 ,  F01D25/24

CPC classification number: F04D29/526 ,  B64D27/16 ,  F01D25/005 ,  F01D25/24 ,  F02C7/05 ,  F02C7/25 ,  F05D2300/603 ,  Y02T50/672

Abstract: A gas turbine casing made of organic matrix composite material includes reinforcement densified by an organic matrix defines an inside volume. On its inside face the casing has a structural part with a first face facing the inside face of the casing, and an opposite second face defining a flow passage portion. Recesses opening out into the inside volume of the casing are present between the inside face of the casing and the first face of the structural part facing the inside face of the casing. In the event of a fire, the recesses allow gas coming from degradation of the resin of the casing to be discharged into the flow passage.

Abstract translation: 由有机基质复合材料制成的燃气轮机壳体包括由有机基质致密化的增强物，其限定内部体积。 在其内表面上，壳体具有结构部分，其具有面向壳体内表面的第一面和限定流路部分的相对的第二面。 在壳体的内表面和与壳体的内表面相对的结构部件的第一面之间存在开口到壳体的内部容积的凹部。 在发生火灾的情况下，凹部允许来自壳体的树脂的降解的气体排放到流动通道中。