RU2018120734A - Способ изготовления детали из композиционного материала, имеющей тело, составляющее одно целое с одной или более платформами - Google Patents

Способ изготовления детали из композиционного материала, имеющей тело, составляющее одно целое с одной или более платформами Download PDF

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RU2018120734A
RU2018120734A RU2018120734A RU2018120734A RU2018120734A RU 2018120734 A RU2018120734 A RU 2018120734A RU 2018120734 A RU2018120734 A RU 2018120734A RU 2018120734 A RU2018120734 A RU 2018120734A RU 2018120734 A RU2018120734 A RU 2018120734A
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parts
layers
warp
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fiber
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RU2717808C2 (ru
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Николя Пьер ЛАНФАН
Себастьен ПОТАР
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Сафран
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    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
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    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
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    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
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    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
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    • B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C70/28—Shaping operations therefor
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    • B29D99/00—Subject matter not provided for in other groups of this subclass
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • C04B35/628—Coating the powders or the macroscopic reinforcing agents
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    • C04B35/628—Coating the powders or the macroscopic reinforcing agents
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    • C04B35/83—Carbon fibres in a carbon matrix
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
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  • Engineering & Computer Science (AREA)
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  • General Engineering & Computer Science (AREA)
  • Woven Fabrics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Moulding By Coating Moulds (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Claims (10)

1. Способ изготовления детали из композиционного материала, имеющей тело, прикрепленное по меньшей мере к одной платформе, присутствующей на одном конце упомянутого тела, который содержит
использование многослойного переплетения между множеством слоев нитей основы для формирования волоконной болванки, имеющей продольное направление, соответствующее продольному направлению тела детали, которая должна быть изготовлена, причем эта волоконная болванка делится в направлении ее толщины на первую, вторую и третью части по меньшей мере в одной зоне несвязывания, смежной с одним из ее концов, причем первая часть располагается между второй и третьей частями, с которыми она соединена путем переплетения снаружи упомянутой по меньшей мере одной зоны несвязывания;
использование волоконной болванки для формирования заготовки для детали, которая должна быть изготовлена, путем складывания сегментов второй и третьей частей, которые не связаны с первой частью, на противоположных сторонах первой части, с помощью формирования сложенных сегментов второй и третьей частей так, чтобы сформировать части заготовки для платформы изготовляемой детали, а также складывания сегмента первой части для заполнения канавки, присутствующей в зазоре между второй и третьей частями; и
уплотнение этой заготовки с помощью матрицы для того, чтобы получить деталь, сделанную из композиционного материала, имеющую по меньшей мере одну интегрированную платформу.
2. Способ по п. 1, в котором первая, вторая и третья части вместе имеют то же самое количество слоев нитей основы, что и остальная часть волоконной болванки, расположенная снаружи упомянутой по меньшей мере одной зоны несвязывания.
3. Способ по п. 1, в котором первая, вторая и третья части вместе содержат больше слоев нити основы, чем количество слоев нити основы в остальной части волоконной болванки, расположенной снаружи упомянутой по меньшей мере одной зоны несвязывания.
4. Способ по п. 3, в котором один или более дополнительных слоев основы ткутся вместе со слоями нитей основы по меньшей мере второй и третьей частей.
5. Способ по п. 1, в котором первая, вторая и третья части вместе содержат меньше слоев нити основы, чем количество слоев нити основы в остальной части волоконной болванки, расположенной снаружи упомянутой по меньшей мере одной зоны несвязывания.
6. Способ по п. 5, в котором один или более слоев основы убираются во время переплетения по меньшей мере упомянутых второй и третьей частей.
7. Способ по п. 1, в котором деталь из композиционного материала соответствует авиационной детали, выбираемой из по меньшей мере одной из следующих деталей: лопатка турбинного двигателя, лопасть турбинного двигателя, профиль усиления и подвеска.
RU2018120734A 2015-11-06 2016-11-03 Способ изготовления детали из композиционного материала, имеющей тело, составляющее одно целое с одной или более платформами RU2717808C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1560649 2015-11-06
FR1560649A FR3043355B1 (fr) 2015-11-06 2015-11-06 Procede de fabrication d'une piece en materiau composite comprenant un corps solidaire d'une ou plusieurs plates-formes
PCT/FR2016/052848 WO2017077240A1 (fr) 2015-11-06 2016-11-03 Procede de fabrication d'une piece en materiau composite comprenant un corps solidaire d'une ou plusieurs plates-formes

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RU2018120734A true RU2018120734A (ru) 2019-12-06
RU2018120734A3 RU2018120734A3 (ru) 2020-02-03
RU2717808C2 RU2717808C2 (ru) 2020-03-25

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EP (1) EP3370951B1 (ru)
JP (1) JP6862440B2 (ru)
CN (1) CN108367524B (ru)
BR (1) BR112018009047B1 (ru)
CA (1) CA3004161C (ru)
FR (1) FR3043355B1 (ru)
RU (1) RU2717808C2 (ru)
WO (1) WO2017077240A1 (ru)

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FR3116753B1 (fr) * 2020-12-01 2023-05-26 Safran Aircraft Engines Procédé de fabrication d'une aube en matériau composite avec plateformes et pattes de fixation intégrées
FR3120910A1 (fr) * 2021-03-17 2022-09-23 Safran Aircraft Engines Pièce de turbomachine composite formée d’une âme entourée par deux préformes fibreuses tissées 3D
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CN108367524A (zh) 2018-08-03
RU2018120734A3 (ru) 2020-02-03
US20180319101A1 (en) 2018-11-08
FR3043355B1 (fr) 2017-12-22
BR112018009047A8 (pt) 2019-02-26
FR3043355A1 (fr) 2017-05-12
CA3004161C (fr) 2023-03-21
EP3370951B1 (fr) 2020-01-01
RU2717808C2 (ru) 2020-03-25
CA3004161A1 (fr) 2017-05-11
JP2019500533A (ja) 2019-01-10
WO2017077240A1 (fr) 2017-05-11
BR112018009047A2 (pt) 2018-10-30
EP3370951A1 (fr) 2018-09-12
CN108367524B (zh) 2020-08-14
US10532521B2 (en) 2020-01-14
JP6862440B2 (ja) 2021-04-21
BR112018009047B1 (pt) 2022-02-22

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