A multilayer protective tape for rotor blades of wind energy turbines said tape having a protective top layer comprising a polymer film and an adhesive bottom layer, wherein the top layer has a continuous surface (S) that is outwardly curved or outwardly trapezoidal surface such that the tape has a cross-sectional profile having an inner section between two lateral sections and wherein the inner section has a thickness (Ti) made up by the thickness of the top layer and adhesive bottom layer that is greater than the thickness of at least one of the lateral sections (T1,T2) made up by the thickness of the top layer and adhesive bottom layer and wherein the thickness (T1 or T2) of at least one lateral section is at most 600 μm and the thickness of the inner section (Ti) is at least 330 μm. Also provided are processes for making profiled tapes and methods for applying the tapes to rotor blades and blades containing protective tapes.

The present disclosure relates to a pressure sensitive adhesive foam comprising a rubber-based elastomeric material and at least one hydrocarbon tackifier, wherein the hydrocarbon tackifier(s) have a Volatile Organic Compound (VOC) value of less than 1000 ppm and a Volatile Fogging Compound (FOG) value of less than 1500 ppm, when measured by thermogravimetric analysis according to the weight loss test methods described in the experimental section. The present disclosure also relates to a method of manufacturing such a pressure sensitive adhesive foam and uses thereof.

The present disclosure relates to a pressure sensitive adhesive foam comprising a rubber-based elastomeric material and at least one hydrocarbon tackifier, wherein the hydrocarbon tackifier(s) have a Volatile Organic Compound (VOC) value of less than 1000 ppm and a Volatile Fogging Compound (FOG) value of less than 1500 ppm, when measured by thermogravimetric analysis according to the weight loss test methods described in the experimental section. The present disclosure also relates to a method of manufacturing such a pressure sensitive adhesive foam and uses thereof.

The invention relates to a reinforcement member comprising a heatcurable structural adhesive on a carrier member, wherein the carrier member comprises a fiber-reinforced polyester material. The invention further relates to a method to produce such a reinforcement member and its use.

Heat-curing epoxy resin compositions are characterized by high impact strength, good storage stability, and a low curing temperature. The epoxy resin compositions are suitable for use as a construction shell adhesive and for producing structural foams. They can already be cured in so-called bottom-baking conditions. Furthermore, it has been found that the use of an accelerator of the formula (Ia) or (Ib) results in an increase of the impact strength of heat-curing epoxy resin compositions.

A thermosettable precursor of an expanded structural adhesive composition comprising: an epoxy compound; an epoxy curing agent; an expanding agent; and a mineral pigment selected from the group of phosphate metal complexes. In addition, a method of bonding two parts and to uses of the thermosettable precursor of an expanded structural adhesive composition.

A thermosettable precursor of an expanded structural adhesive composition comprising: an epoxy compound; an epoxy curing agent; an expanding agent; and a mineral pigment selected from the group of phosphate metal complexes. In addition, a method of bonding two parts and to uses of the thermosettable precursor of an expanded structural adhesive composition.

A method for manufacturing a core-material-containing garment, the method includes: a feeding step of feeding fabric (2) in a wound state onto a conveyor table (1) without relaxing or substantially relaxing the fabric (2); a core material application step of applying a reactive hot-melt adhesive to the fabric (2) on the conveyor table (1) to form a core material (12); an adhesive application step of applying a bonding hot-melt adhesive (13) configured to bond the fabric (2); and a drying step of drying the applied bonding hot-melt adhesive (13), and in the core material application step, the reactive hot-melt adhesive is mixed with nitrogen gas and foamed, and the reactive hot-melt adhesive is applied using an application device provided with a resin discharge unit that is movable in at least two axial directions of vertical and horizontal directions.

A method for manufacturing a core-material-containing garment, the method includes: a feeding step of feeding fabric (2) in a wound state onto a conveyor table (1) without relaxing or substantially relaxing the fabric (2); a core material application step of applying a reactive hot-melt adhesive to the fabric (2) on the conveyor table (1) to form a core material (12); an adhesive application step of applying a bonding hot-melt adhesive (13) configured to bond the fabric (2); and a drying step of drying the applied bonding hot-melt adhesive (13), and in the core material application step, the reactive hot-melt adhesive is mixed with nitrogen gas and foamed, and the reactive hot-melt adhesive is applied using an application device provided with a resin discharge unit that is movable in at least two axial directions of vertical and horizontal directions.

The invention relates to a reinforcement member comprising a heatcurable structural adhesive on a carrier member, wherein the carrier member comprises a fiber-reinforced polyester material. The invention further relates to a method to produce such a reinforcement member and its use.