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公开(公告)号：US20140026974A1
公开(公告)日：2014-01-30
申请号：US13953368
申请日：2013-07-29
Applicant: AIRCELLE
Inventor： Bertrand DESJOYEAUX , Olivier Hubier
CPC classification number: B29D99/001 , B29C70/48 , B29C70/84 , B29L2031/087 , B29L2031/7504 , B64D29/00 , B64D33/02 , F02C7/04 , Y10T137/0536
Abstract: A method for manufacturing a nacelle air intake lip including a plurality of components includes the following steps. The first step is positioning, inside a mold, two components within a set of fibrous layers encompassing all or part of the components so that a preform is formed. Next step is performing impregnation of the obtained preform to obtain molding of the nacelle air intake lip.
Abstract translation: 包括多个部件的制造机舱进气口的方法包括以下步骤。 第一步是在模具内部定位一组包含全部或部分组件的纤维层中的两个部件，从而形成预制件。 下一步是对获得的预制件进行浸渍以获得机舱进气口的模制。
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2.发明授权Method for manufacturing an air intake structure for a turbojet engine nacelle 有权制造涡轮喷气发动机机舱的进气结构的方法公开(公告)号：US09481054B2
公开(公告)日：2016-11-01
申请号：US13958246
申请日：2013-08-02
Applicant: AIRCELLE
Inventor： Bertrand Desjoyeaux , Olivier Hubier
CPC classification number: B23P15/008 , B29C70/44 , B29C70/48 , B29C70/84 , B64D33/02 , B64D2033/0286 , Y10T29/49346
Abstract: A method for manufacturing an air-intake structure for a turbojet-engine nacelle includes two component parts, i.e. one air-intake lip structure and one outer cowl for the air-intake structure. In particular, the method includes the following steps: separately manufacturing the component parts such that each integrates one overlapping portion with a part to which is to be attached. The overlapping portion is configured such that an outer surface of the outer overlapping portion provides continuity with an outer surface of the outer cowl associated with the inner overlapping portion. To secure the overlapping portions, glue or a fastener may be used.
Abstract translation: 用于制造涡轮喷气发动机机舱的进气结构的方法包括两个部件，即一个进气口结构和一个用于进气结构的外罩。 特别地，该方法包括以下步骤：分开制造组成部件，使得每个部件将一个重叠部分与要附接的部分集成。 重叠部分构造成使得外部重叠部分的外表面与外部整流罩的与内部重叠部分相关联的外表面提供连续性。 为了固定重叠部分，可以使用胶水或紧固件。
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3.发明申请METHOD FOR MANUFACTURING AN AIR INTAKE STRUCTURE FOR A TURBOJET ENGINE NACELLE 有权用于制造涡轮发动机空气吸入结构的方法公开(公告)号：US20130312263A1
公开(公告)日：2013-11-28
申请号：US13958246
申请日：2013-08-02
Applicant: Aircelle
Inventor： Bertrand DESJOYEAUX , Olivier Hubier
IPC: B23P15/00
CPC classification number: B23P15/008 , B29C70/44 , B29C70/48 , B29C70/84 , B64D33/02 , B64D2033/0286 , Y10T29/49346
Abstract: A method for manufacturing an air-intake structure for a turbojet-engine nacelle includes two component parts, i.e. one air-intake lip structure and one outer cowl for the air-intake structure. In particular, the method includes the following steps: separately manufacturing the component parts such that each integrates one overlapping portion with a part to which is to be attached. The overlapping portion is configured such that an outer surface of the outer overlapping portion provides continuity with an outer surface of the outer cowl associated with the inner overlapping portion. To secure the overlapping portions, glue or a fastener may be used.
Abstract translation: 用于制造涡轮喷气发动机机舱的进气结构的方法包括两个部件，即一个进气口结构和一个用于进气结构的外罩。 特别地，该方法包括以下步骤：分开制造组成部件，使得每个部件将一个重叠部分与要附接的部分集成。 重叠部分构造成使得外部重叠部分的外表面与外部整流罩的与内部重叠部分相关联的外表面提供连续性。 为了固定重叠部分，可以使用胶水或紧固件。
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