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公开(公告)号:US20240124149A1
公开(公告)日:2024-04-18
申请号:US18351022
申请日:2023-07-12
Applicant: Safran Nacelles
Inventor: Jean-Baptiste DELARUE , Laurent Georges VALLEROY , Vianney HUS , Hugo BOISTELLE
Abstract: An assembly includes a nacelle panel of an aircraft engine, the nacelle panel including an outer skin, an inner skin and a central layer interposed between the outer and inner skins. The central layer has a housing, the outer skin has an opening which opens into the housing, and a linking member extends in the opening and in the housing, the linking member to be connected to an actuator.
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公开(公告)号:US20240359421A1
公开(公告)日:2024-10-31
申请号:US18686592
申请日:2022-08-29
Applicant: SAFRAN NACELLES
Inventor: Marc VERSAEVEL , Pierre-Yves GINI , Hugo BOISTELLE , Bertrand Léon Marie DESJOYEAUX
IPC: B32B3/30 , B29C35/02 , B29C65/70 , B29C70/44 , B29K63/00 , B29K105/08 , B29K105/20 , B29K307/04 , B29K705/02 , B29L31/38 , B32B3/26 , B32B5/02 , B32B7/12 , B32B15/14 , B32B15/20
CPC classification number: B32B3/30 , B29C35/0227 , B29C65/70 , B29C70/44 , B32B3/266 , B32B5/02 , B32B7/12 , B32B15/14 , B32B15/20 , B29K2063/00 , B29K2105/08 , B29K2105/20 , B29K2307/04 , B29K2705/02 , B29K2995/0063 , B29K2995/0097 , B29L2031/38 , B32B2250/40 , B32B2255/02 , B32B2255/26 , B32B2260/023 , B32B2260/046 , B32B2262/106 , B32B2307/102 , B32B2307/72 , B32B2605/18
Abstract: A method for manufacturing an acoustic panel including a first skin, a second skin and an intermediate structure enclosed between these skins and forming oblique cavities with respect to the latter. The method includes an intermediate polymerization step for fastening the intermediate structure to the first skin in order to increase the compressive strength thereof and in particular to support an automated operation of draping the second skin.
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公开(公告)号:US20220324129A1
公开(公告)日:2022-10-13
申请号:US17753458
申请日:2020-09-03
Applicant: SAFRAN NACELLES
Inventor: Boris HAUCOURT , Hugo BOISTELLE , Benjamin PERSYN , Eric PILLON , Yanhaël LABAT
Abstract: The disclosure relates in particular to a method of cutting one or more draping elements in a strip of material comprising a fabric layer comprising a film on at least one face. Each draping element is delimited along a determined outline comprising at least one angle, each draping element being cut by means of a cutting blade. At each angle of the outline, the fabric layer and each one film are cut along a curve so as to obtain one or more draping elements without overcutting.
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