Abstract: The present description relates to in-plane isotropic products derived from cellulosic filament based compositions that are substantially free of binders; and comprising inorganic fillers with an average particle size of less than 5 ?m; and methods for producing these in-plane isotropic products. The method comprising providing a cellulosic filament substantially free of any binder; providing an inorganic filler comprising an average particle size of less than 5 ?m; mixing the cellulosic filament and the filler to produce a slurry; transferring the slurry in a preforming jig to produce a wet mat in the jig; and hot press compression molding the mat to produce the in-plane isotropic product. The inorganic fillers were uniquely shown substantially useful to accelerate the final dewatering (drying) in the hot press at 150° C./250 psi and to eliminate delamination issue insitu the molded products.

Abstract: The present disclosure relates to a method and an apparatus for identifying line-of-responses (LOR) of photons. A radiation detection machine measures the photons. LOR identification errors are then mitigated using pattern recognition of the measurements. In some embodiments, the photons may comprise positron annihilation photons, each position annihilation photon being associated with one or more scattered photons. In yet some embodiments, pattern recognition may be implemented in a neural network.

Abstract: An axial compressor for a turbomachine is fitted with a device for centripetally bleeding turbine-cooling air. The compressor includes at least two rings of blades, an outer shroud having holes, and a fixed ring of stator vanes placed in the stream between the moving rings of blades. The holes are inlets for the bleed device, opening out into an annular groove beneath the interstice separating the inner platforms of the stator vanes from the rim of the upstream disk. The groove is fitted with fixed air guide devices to impart a centripetal swirling motion to the air flowing therein in the same direction as the compressor so as to reduce the velocity of the air relative to the rotating holes.

Abstract: The invention provides an axial compressor for a turbomachine, the compressor being fitted with a device for centripetally bleeding turbine-cooling air from a stream of air flowing through said compressor, said compressor comprising two rings of moving blades extending radially outwards from the peripheries of two consecutive disks joined together by an outer shroud having holes, and further comprising a fixed ring of stator vanes placed in the stream between said moving rings of blades, said holes serving as air inlets to said bleed device and opening out into an annular groove provided beneath the interstice separating the inner platforms of the stator vanes from the rim of the upstream disk, said groove communicating with said stream via said interstice, wherein the groove is fitted with fixed air guide means imparting centripetal swirling motion on the air flowing in said groove, the motion rotating in the same direction as the compressor so as to reduce the velocity of the air entering into the holes rel