公开(公告)号：US09452562B2

公开(公告)日：2016-09-27

申请号：US14352856

申请日：2012-10-17

Applicant: SNECMA

Inventor： Richard Mathon ,  Olivier Patrigeon

IPC: B29C53/82 ,  B29C70/32 ,  B29C70/54 ,  B29C53/56 ,  B29L31/00 ,  B29C53/80

CPC classification number: B29C53/821 ,  B29C53/56 ,  B29C53/562 ,  B29C53/8075 ,  B29C70/32 ,  B29C70/54 ,  B29C70/541 ,  B29L2031/7504

Abstract: An impregnation mandrel for production of gas turbine casings made from composite material, the mandrel including: an annular wall with a profile of an outer surface that corresponds to that of an internal surface of the casing to be produced; two side plates, with profiles that correspond to those of external casing flanges to be produced; and a removable device for clamping a layer having a fibrous texture, which is wound around the mandrel.

Abstract translation: 一种用于生产由复合材料制成的燃气轮机壳体的浸渍心轴，所述心轴包括：环形壁，其外表面的轮廓对应于待生产的壳体的内表面; 两个侧板，具有对应于要生产的外壳法兰的轮廓; 以及用于夹紧缠绕在心轴上的具有纤维织构的层的可移除装置。

公开(公告)号：US20140283977A1

公开(公告)日：2014-09-25

申请号：US14352856

申请日：2012-10-17

Applicant: SNECMA

Inventor： Richard Mathon ,  Olivier Patrigeon

IPC: B29C53/82 ,  B29C70/32 ,  B29C70/54 ,  B29C53/56

CPC classification number: B29C53/821 ,  B29C53/56 ,  B29C53/562 ,  B29C53/8075 ,  B29C70/32 ,  B29C70/54 ,  B29C70/541 ,  B29L2031/7504

Abstract: An impregnation mandrel for production of gas turbine casings made from composite material, the mandrel including: an annular wall with a profile of an outer surface that corresponds to that of an internal surface of the casing to be produced; two side plates, with profiles that correspond to those of external casing flanges to be produced; and a removable device for clamping a layer having a fibrous texture, which is wound around the mandrel.

Abstract translation: 一种用于生产由复合材料制成的燃气轮机壳体的浸渍心轴，所述心轴包括：环形壁，其外表面的轮廓对应于待生产的壳体的内表面; 两个侧板，具有对应于要生产的外壳法兰的轮廓; 以及用于夹紧缠绕在心轴上的具有纤维织构的层的可移除装置。

公开(公告)号：US20140262046A1

公开(公告)日：2014-09-18

申请号：US14352159

申请日：2012-10-17

Applicant: SNECMA

Inventor： Richard Mathon ,  Olivier Patrigeon ,  Louis Bettega

IPC: B29C70/44 ,  F02C7/04

CPC classification number: B29C70/443 ,  B29C33/30 ,  B29C43/36 ,  B29C70/446 ,  B29C2043/3205 ,  B29L2031/7504 ,  F01D25/285 ,  F02C7/04 ,  F05D2300/603 ,  Y02T50/672

Abstract: An impregnation mandrel for production of a gas turbine casing made from composite material, including: a mandrel having a central wall and two side plates; compaction bars, each including (i) a wedge configured to bear against a fibrous reinforcing part covering angles formed between the central wall and the side plates of the mandrel, and (ii) an attachment flange configured to be attached to the corresponding side plate of the mandrel; a flexible casing forming a vacuum bag and configured to be applied at least against the fibrous reinforcing part covering the central wall of the mandrel; and a mechanism for injecting resin into a space defined between the vacuum bag and the mandrel at one of longitudinal ends of the fibrous reinforcement and for extracting the resin at the opposite end.

Abstract translation: 一种用于生产由复合材料制成的燃气涡轮机壳体的浸渍心轴，包括：具有中心壁和两个侧板的心轴; 压紧杆，每个包括（i）楔形构件，用于承受覆盖形成在心轴的中心壁和侧板之间的角度的纤维增强部分，以及（ii）附接凸缘，其构造成附接到相应的侧板 心轴 形成真空袋的柔性套管，并构造成至少施加在覆盖心轴的中心壁的纤维增强部分上; 以及用于在纤维增强件的纵向端部之一处将树脂注入位于真空袋和心轴之间的空间中并用于在相对端抽出树脂的机构。

公开(公告)号：US09889611B2

公开(公告)日：2018-02-13

申请号：US14351987

申请日：2012-10-23

Applicant: SNECMA

Inventor： Richard Mathon ,  Olivier Patrigeon ,  Micah Gummel

IPC: B29C70/32 ,  B29C70/54 ,  B29C53/56 ,  B29C53/80 ,  B29L31/00

CPC classification number: B29C70/32 ,  B29C53/562 ,  B29C53/8016 ,  B29C70/543 ,  B29C2053/8025 ,  B29L2031/7504

Abstract: A device for holding a fiber texture on an impregnation mandrel of a winding machine, the device including a cross-member forming a support having each of its ends for fastening on one of cheekplates of the mandrel, a central pad carrier mounted on the cross-member and including a pad for pressing against a fiber texture layer wound on the mandrel, two lateral pad carriers mounted on the cross-member and each including a main pad for pressing against the fiber texture layer wound on the mandrel and a lateral pad for pressing against a lateral margin of the fiber texture layer wound on the mandrel, and a mechanism exerting a clamping force urging the pads against the fiber texture layer wound on the mandrel.

公开(公告)号：US09415549B2

公开(公告)日：2016-08-16

申请号：US14352159

申请日：2012-10-17

Applicant: SNECMA

Inventor： Richard Mathon ,  Olivier Patrigeon ,  Louis Bettega

IPC: B29C65/00 ,  B32B37/00 ,  B29C70/44 ,  B29C33/30 ,  F01D25/28 ,  F02C7/04 ,  B29L31/00 ,  B29C43/32 ,  B29C43/36

CPC classification number: B29C70/443 ,  B29C33/30 ,  B29C43/36 ,  B29C70/446 ,  B29C2043/3205 ,  B29L2031/7504 ,  F01D25/285 ,  F02C7/04 ,  F05D2300/603 ,  Y02T50/672

Abstract: An impregnation mandrel for production of a gas turbine casing made from composite material, including: a mandrel having a central wall and two side plates; compaction bars, each including (i) a wedge configured to bear against a fibrous reinforcing part covering angles formed between the central wall and the side plates of the mandrel, and (ii) an attachment flange configured to be attached to the corresponding side plate of the mandrel; a flexible casing forming a vacuum bag and configured to be applied at least against the fibrous reinforcing part covering the central wall of the mandrel; and a mechanism for injecting resin into a space defined between the vacuum bag and the mandrel at one of longitudinal ends of the fibrous reinforcement and for extracting the resin at the opposite end.

Abstract translation: 一种用于生产由复合材料制成的燃气涡轮机壳体的浸渍心轴，包括：具有中心壁和两个侧板的心轴; 压紧杆，每个包括（i）楔形构件，用于承受覆盖形成在心轴的中心壁和侧板之间的角度的纤维增强部分，以及（ii）附接凸缘，其构造成附接到相应的侧板 心轴 形成真空袋的柔性套管，并构造成至少施加在覆盖心轴的中心壁的纤维增强部分上; 以及用于在纤维增强件的纵向端部之一处将树脂注入位于真空袋和心轴之间的空间中并用于在相对端抽出树脂的机构。

公开(公告)号：US20170361512A1

公开(公告)日：2017-12-21

申请号：US15691024

申请日：2017-08-30

Applicant: SNECMA

Inventor： Romain PLANTE ,  Lise Lacroix ,  Olivier Patrigeon ,  Jean-Pierre Cauchois ,  Pascal Burek

IPC: B29C45/00 ,  B29D99/00 ,  B29C70/48

CPC classification number: B29C45/0005 ,  B29C70/48 ,  B29D99/0025

Abstract: A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.