Automated manufacturing of composite laminates for structures, preferably structures of an aircraft, by using laying machines. More particularly, a method for determining the energy of debonding between layers of a laminate of composite material by means of a laying machine, and a laying machine for performing the method.

The present invention provides a method for testing strength of a metal roofing material, the metal roofing material comprising: a front substrate made of a metal sheet; a back substrate arranged on the back side of the front substrate; and a core material filled between the front substrate and the back substrate, the method comprising the steps of: tightening the metal roofing material 1 to a base 50; and applying a load 52L for uplifting an end portion 1E of the metal roofing material 1 tightened to the base 50 to the end portion 1E and measuring an uplift amount of the end portion 1E corresponding to the load 52L.

The invention relates to a method for producing a test body (30) for mechanically destructively testing a materially bonded joining connection, wherein the method comprises the following steps: providing an areal fiber composite substrate formed from a fiber composite material which has a fiber material and matrix material in which the fiber material is embedded, applying at least one test fabric and an adhesive to a substrate surface of the areal fiber composite substrate, and curing the adhesive, and therefore a materially bonded joining connection is produced between the test fabric and the substrate surface by way of the cured adhesive,
wherein a Dutch-weave fabric and/or a square-mesh fabric is provided as the test fabric.

An apparatus and method for preparing Double Cantilever Beam (DCB) specimens are disclosed as an apparatus and method for conducting Mode I fracture resistance testing using the DCB specimens. In a first embodiment, a drill jig is used to locate the DCB specimen and guide a drilling process during creation of at least one through-hole in the DCB specimen. The drilling process may employ a traditional drill and drill bit, a laser drill, or a water jet. In another embodiment, a set of rotating pin blocks, each with a full-round or a half-round specimen pin at one end and a hanger full-round pin at the other end, engage the DCB specimen and facilitate the internal application of a fracturing load to the DCB specimen for the Mode I fracture resistance test. The present invention may significantly reduce the time and materials needed to prepare and test a DCB specimen.

A test apparatus used for simulating debonding between a carbon fiber reinforced polymer (CFRP) and concrete in a CFRP-strengthened structure consists of a primary structural block, a secondary structural block, an adjustable hanger, a receiving slot, an attachment mechanism, a pull-off disk, a connecting plate having a plurality of rods. The adjustable hanger and the secondary structural block are slidably positioned into the receiving slot that traverses into a structural body of the primary structural block. The adjustable hanger is mainly used during double-shearing tests and mixed-mode tests, wherein both shearing and peeling is analyzed in mixed-mode tests. The secondary structural block is used in double-shear tests, mixed-mode tests, single-shear tests, tension pull-off tests, and beam-bend tests. The attachment mechanism, which holds the primary structural block, the secondary structural block, and the adjustable hanger together, is also used during single-shear tests and beam-bend tests.

A test apparatus used for simulating debonding between a carbon fiber reinforced polymer (CFRP) and concrete in a CFRP-strengthened structure consists of a primary structural block, a secondary structural block, an adjustable hanger, a receiving slot, an attachment mechanism, a pull-off disk, a connecting plate having a plurality of rods. The adjustable hanger and the secondary structural block are slidably positioned into the receiving slot that traverses into a structural body of the primary structural block. The adjustable hanger is mainly used during double-shearing tests and mixed-mode tests, wherein both shearing and peeling is analyzed in mixed-mode tests. The secondary structural block is used in double-shear tests, mixed-mode tests, single-shear tests, tension pull-off tests, and beam-bend tests. The attachment mechanism, which holds the primary structural block, the secondary structural block, and the adjustable hanger together, is also used during single-shear tests and beam-bend tests.

The invention relates to a testing device that can be transported and used in situ on a structure to be tested to determine the resistance thereof to peeling. The device fundamentally comprises: a drum with attachment elements for attaching to a specimen that is to be peeled from a hybrid adhesive joint of a structure, a movable carriage on which the drum is mounted; a frame along which the drum moves; and an actuation mechanism that determines the linear movement of the carriage or the rotational movement of the drum and which, by the reaction of the specimen, determines, respectively, the rotation of the drum or the linear displacement of the carriage.

First and second operations are executed under control of a peeling inspection control apparatus functioning as a peeling and grasping control unit. In the first operation, a processed surface contact state in which a processed outer peripheral surface of a contact roller and a surface of a lead wire are in contact with each other is maintained, and contact roller rotation operation is executed in which the contact roller is moved on the surface of the lead wire while the contact roller is being rotated. During execution of the first operation, a tip portion of the lead wire is peeled from a glass substrate. Thereafter, in the second operation, grasping operation is executed in which the tip portion of the lead wire peeled from the glass substrate is grasped by a grasping mechanism.

An adhesive film and arrangement and method for verifying an adhesive attachment. A mechanical strength of adhesive film structure is matched to a target binding force of a bond produced using the film where when the film is pulled from the substrate or a material layer with peeling stress on the bond for verification of adhesive attachment, the film fails with exceedance of the mechanical strength of the structure when the strength of the bond attains or exceeds the target binding force, and the adhesive film when pulled apart does not fail when bond strength does not attain target binding force. An arrangement is disclosed for verification of adhesive attachment, having a substrate, a component bonded to the substrate by an adhesive film, and at least one test section. The test section is formed by projection of the film across an edge of the component bonded to the substrate, the projection being bonded to regions of the substrate.

A system and method for performing a tear test are described herein. The system may include a fixed clamping station configured to hold a first portion of a film specimen and a movable clamp coupled to an actuator, the movable clamp may be configured to hold a second portion of the film specimen. The movable clamp may be configured to move in a direction away from the fixed clamping station to tear the film specimen. The system may include a slitter blade configured to cut the film specimen at a location between the fixed clamping station and the movable clamp. The system may include a load cell coupled to one of the fixed clamping station and the movable clamp. The load cell may be configured to measure a force associated with tearing of the film specimen. The actuator may be configured to manipulate the movable clamp along a trajectory.