The present invention relates to a thermoplastic composition, comprising: A) aromatic polycarbonate and B) Ba) reinforcing fibers and/or Bb) spherical particles of oxides of metals or metalloids of the 3rd main group, 4th main group and/or 4th transition group. The composition further comprises: C) PMMI copolymer and D) phosphite stabilizer and/or phosphine stabilizer, wherein, furthermore, the proportion of B) is ≥35% by weight to ≤40% by weight and the proportion of C) is >0.1% by weight in each case based on the total weight of the composition. The invention further relates to a layered arrangement comprising a substrate layer and a reflection layer distinct from the substrate layer and at least partially covering the substrate layer, wherein the reflection layer at least partially reflects light in the wavelength range from 380 nm to 750 nm, an illumination apparatus comprising a light source and a reflector, wherein the reflector is arranged such that at least a portion of the light transmitted by the light source is reflected by the reflector, and to a process for producing a molded article.

The invention relates to a battery housing (1) for an electrical battery, comprising a basic body (2) which extends in a direction of extent (E) and at least partially delimits a housing interior space (3) on the inside. The battery housing (1) moreover comprises at least one stiffening rib (4), which is shaped integrally on the inside or the outside of the basic body (2) and protrudes from the basic body (2). The stiffening rib (4) of the battery housing (1) runs on the basic body (2) in a rib direction (R) oriented at an angle to the direction of extent (E). In this respect, a body material of the basic body (2) comprises first reinforcing fibres (5), which run substantially in the direction of extent (E) and a rib material of the stiffening rib (4) comprises second reinforcing fibres (6), which run substantially in the rib direction (R).

The present invention prevents internal cracks occurring when an impeller molded using a fiber reinforced resin is manufactured by injection molding. This method for manufacturing an impeller is provided with: an injection step of filling a cavity with a molten resin containing reinforced fibers, from a gate side into which the molten resin flows, toward an opposite-gate side opposite to the gate side; and a dwell step of applying required pressure to the filled molten resin. In the injection step and the dwell step, directional cooling is performed with a temperature gradient such that the temperature becomes lower from the gate side toward the opposite-gate side. According to this method for manufacturing the impeller, the opposite-gate side shrinks with a decrease in the temperature of the molten resin since the temperature of the opposite-gate side is lower. Meanwhile, because the temperature on the gate side is increased, the molten resin can be replenished from the gate side so as to correspond to the amount of shrinkage on the opposite-gate side, and therefore the occurrence of internal tensile residual stress and cracks due to the shrinkage can be prevented.

A reinforcement fiber conveying apparatus, comprises: a reinforcement fiber conveying tubular body having one end arranged in a vicinity of a reinforcement fiber body comprised of a reinforcement fiber that is continuously pulled out and the other end arranged in a vicinity of a reinforcement fiber supplying port formed in a heating cylinder used for injection molding; and an air flow generation unit configure to generate an air flow from the one end toward the other end in the reinforcement fiber conveying tubular body.

A floor panel for an aircraft or spacecraft. The floor panel has a panel-like portion and an additional structure. A first side of the panel-like portion forms part of a floor surface in the aircraft or spacecraft. The additional structure is connected to the panel-like portion on a second side of the panel-like portion that is opposite the first side. The panel-like portion and the additional structure each comprise a matrix material formed by a thermoplastic material. Endless reinforcing fibers are embedded in the matrix material of the panel-like portion. Discontinuous reinforcing fibers are embedded in the matrix material of the additional structure. An aircraft or spacecraft may have a floor area which is formed by a planar arrangement of floor panels of this type. The method for producing a floor panel for an aircraft or spacecraft is provided.

A composition including at least one polyamide polymer obtained from at least one reactive polyamide prepolymer including at least one chain extender (PA.sub.1-All.sub.1-PA.sub.1), the polyamide polymer being prepared at a temperature T.sub.1 no lower than the temperature melting temperature or glass transition temperature of the polymer and having a mean molecular weight Mn.sub.1. The composition has a melt viscosity which can be modulated according to the temperature to which the composition is exposed, wherein the temperature is between T.sub.2 and T.sub.3, T.sub.2 and T.sub.3 being higher than T.sub.1, and the melt viscosity η.sub.2 or η′.sub.3 observed at the temperature T.sub.2 or T.sub.3, respectively, being lower than the melt viscosity η.sub.2 or η.sub.3 of the polyamide polymer, which does not include a chain extender and has the same mean molecular weight Mn.sub.1(PA.sub.1) observed at the same temperature T.sub.2 or T.sub.3. The composition includes one or more polyamides.

A housing part includes a base section having a pair of oppositely disposed flat sides, a pair of housing sections each extending away from one of the pair of oppositely disposed flat sides, and a plurality of fibers disposed in the base section and the housing sections. A main fiber orientation of the fibers in each of the housing sections is oriented away from the base section.

Recycled carbon fibers are processed by rotational tumbling in a mixture with binder material to prepare fiber-containing particles having a dual-tapered shape and general alignment of fibers with a longitudinal direction of the particles. Bulk products including such fiber-containing particles are compounded with polymer and pelletized to prepare fiber-reinforced composite pellets, which are useful for applications such as injection molding to prepare molded products of carbon fiber-reinforced composite material with recycled carbon fibers.

Disclosed herein is a process for the production of a moulded article (MA). Additionally disclosed herein is a method of using at least one blowing gas (C) in the production of a moulded article (MA) for reducing the warpage of the moulded article (MA), where the moulded article (MA) includes at least one thermoplastic polymer (A) and at least one reinforcing fibre (B). Further disclosed herein is the moulded article (MA) obtained by the process.

A forced extraction molded article that can prevent damage during forced extraction is provided. The force extraction molded article (1) is formed of a polyarylene sulfide resin composition so as to include a cylindrical portion, wherein the cylindrical portion (10) has at a forward end portion a bulge (11), and an inner surface including a step in the outer diameter direction at the forward end portion, a portion excluding the step has a gradient such that the inner diameter of the cylindrical portion increases toward the forward end portion, and equation (a) below using a thickness D2 between a connection portion at the step on the inner surface of the cylindrical portion and the outer surface excluding the bulge, a height D4 of the step, and a height Dt of the gradient excluding the step on the inner surface of the cylindrical portion is satisfied.

[00001]$\begin{array}{cc}\left[\mathrm{Equation}1\right]& \\ 0.001\le \frac{\frac{D2}{2}-D4}{D2}\times \frac{Dt}{D2}\le 0.44& \mathrm{Equation}\left(a\right)\end{array}$