摘要:
The present invention relates to a method of making a composite sandwich structure. The method comprises the steps of: providing a base lay-up on a surface, wherein the base lay-up comprises a first reinforcement material layer; providing a core layer on to the base lay-up, wherein the core layer comprises an open cellular structure and wherein the open cellular structure is at least partially filled with unbound particles; providing a top lay-up on top of the core layer, wherein the top lay-up comprises a second reinforcement material layer; sealing the arrangement within a hermetically sealed enclosure; introducing matrix material into the arrangement via the at least one conduit through a pressure differential; and curing the matrix material.
摘要:
In a method for manufacturing an acoustic panel (20), a core structure (25) is provided between and bonded to a top skin (22) and a septum (23). A plurality of perforations (32) are formed in the top skin (22) using an energy beam device (52). A plurality of perforations (34) are formed in the septum (23) through the top skin holes (32) using the energy beam device (56). A plurality of cavities (44) in the core structure (25) fluidly couple at least some of the perforations (32) in the top skin (22) with at least some of the perforations (34) in the septum (23).
摘要:
The invention relates to a method for producing a sandwich metal part (1) having a non-developable shape, said part comprising a metal honeycomb core (2) and two metal skins (4) arranged to either side of the core, the method comprising: - a step of plastically deforming metal sheets (4') for obtaining the two metal skins (4); then, - a step of rigidly connecting the two skins (4) to the core (2).
摘要:
A manufacturing method 1 of a honeycomb structure includes a forming step S1 of forming a quadrangular pillar-shaped honeycomb formed body, a firing step S2 of firing the honeycomb formed body and forming a quadrangular pillar-shaped honeycomb fired body, a coating step S3 of coating at least a part of side surfaces of the honeycomb fired body with a paste-like bonding material, a honeycomb block body preparing step S4 of bonding the plurality of honeycomb fired bodies while performing pressurizing, to prepare a honeycomb block body, and a circumference grinding step S7 of grinding a circumferential surface of the honeycomb block body and obtaining the honeycomb structure, and in the honeycomb block body preparing step S4, the bonding is performed without interposing any member other than the bonding material between the honeycomb fired bodies, and the bonding material has a shear thinning property.
摘要:
The invention relates to a honeycomb (120… 420), in particular deformable honeycomb, for example for lightweight components having a curved surface. The honeycomb comprises elongate strips (122...422) and a plurality of connecting regions (123... 423) each provided between two opposite strips, which connecting regions connect the strips integrally to one another in sections in the transverse direction (W) and are arranged at regular intervals along the longitudinal direction (L) of a strip at a periodic center spacing (I). Honeycomb-like cells (124… 424) form hollow spaces between the strips. The invention is characterized in that based on three successive strips (122…, 422) an offset (SI') of the connecting regions between the first and second strips (122-1, 122-2… 422-1, 422-2) in relation to the connecting regions between the second and third strips (122-2, 122-3… 422-2, 422-3) towards a first side (D1) of the longitudinal direction (L) is considerably smaller than towards the other, second side (D2) of the longitudinal direction (L). In this way, in cross section in the L/W plane, at least some of the cells (24) have a shape having at least one longer limb (S2) corresponding to the greater offset and preferably at least one shorter limb (S1) corresponding to the smaller offset.
摘要:
A method of making a composite sandwich panel comprises the steps of (i) making a core structure, (ii) making at least one facesheet, (iii) bonding at least one of the at least one facesheets to the core structure, wherein the growth of a carbon nanotube structure is achieved during the making the core structure and occurs on or inside of the core structure.
摘要:
Embodiments disclosed herein relate to polymer resins having a first thermoset and one or more additional components (e.g., a second thermoset and/or a thermoplastic), composite laminates including the same, methods of making and using the same, and composite laminate structures including the same.
摘要:
Embodiments disclosed herein relate to polymer resins having a first thermoset and one or more additional components (e.g., a second thermoset and/or a thermoplastic), composite laminates including the same, methods of making and using the same, and composite laminate structures including the same.