||WO||WO/2014/035248 - SPORTS AND GAME PRODUCT||06.03.2014||
||PCT/NL2013/050630||RUYSSENAARS, Bas Boris||RUYSSENAARS, Bas Boris|
The present invention relates to a combination of at least one stick (10) and a ring device (30) configured for throwing and catching the ring device with the stick, wherein: - the stick comprises: - a main section (12) configured to be held by the hands of a user, - a ring launching member (14) provided at one end (25) of the stick and configured to launch and catch the ring device, - the ring device comprises a central opening (72) and is constructed to fit on the ring launching member and be launched from the ring launching. At take-off, the ring device is launched in a rotary manner.
||WO||WO/2014/035250 - TRANSPORT AIDING DEVICE ADAPTED FOR DESCENDING OR CLIMBING A STAIRCASE||06.03.2014||
||PCT/NL2013/050635||BSURE B.V.||BOUWHUIS, Arnoldus Johannes Antonius|
A transport aiding device adapted for descending or climbing a staircase with a single person sitting in the transport aiding device, which transport aiding device rides on the staircase during the descent or climbing, and can be handled and/or operated by at least one assistant walking on the staircase behind the transport aiding device. The device comprises a wheeled frame structure, including a frame base having at least two rear legs and two rear wheels. The device has a collapsible seat assembly with a seat and at least least one rail assembly including a movable endless belt, which rail assembly is adapted to ride over a staircase with said belt. The rail assembly is pivotally secured to the frame base and is movable between a collapsed storage position and an operative position pivoted backward from the frame base. The frame structure further comprises an extensible rear handle member providing a handle for an assistant walking on the staircase behind the transport aiding device.
||WO||WO/2014/035238 - MICROSCOPIC IMAGING APPARATUS AND METHOD TO DETECT A MICROSCOPIC IMAGE||06.03.2014||
||PCT/NL2013/050618||STICHTING VU-VUMC||WITTE, Stefan Michiel|
The invention relates to amicroscopic imaging apparatus to provide an image of a sample. The apparatus having an illumination system to provide an illumination beam with radiation;and a sensor constructed and arranged to receive: a first image of a first diffraction pattern created by diffraction of the illumination beam on the sample; a second image of a second diffraction pattern created by diffraction of the illumination beam on the sample. The sensor may be connected with a processor running a program to retrieve phase information from the sample from the first and second image received by the sensor. The illumination system may have a first illumination device to provide the illumination beam with radiation of substantially a first wavelength; and a second illumination device to provide the illumination beam with radiation of substantially a second wavelength different than the first wavelength. The sensor may receive a first image of a first diffraction pattern created by diffraction of the illumination beam with radiation of substantially the first wavelength on the sample; and,a second image of a second diffraction pattern created by diffraction of the illumination beam with radiation of substantially the second wavelength on the sample.
||WO||WO/2014/035242 - METHOD FOR MANUFACTURING A SOLAR CELL AND SOLAR CELL OBTAINED THEREWITH||06.03.2014||
||PCT/NL2013/050623||M4SI B.V.||LUCHIES, Johannes Reinder Marc|
The method of manufacturing a solar cell, comprising the steps of providing a solar cell device comprising a semiconductor body (10) and having a first side (11) and an opposed second side (12), which first side is intended for capturing incident light and which second side is intended for assembly to a carrier, which solar cell device comprises a first contact region (13) in the semiconductor body (10) at one of the first (11) and the second side (12); applying an optically transparent structure (22) of electrically insulating material to at least one of the sides (11, 12) of the solar cell device, which structure is patterned to form an aperture to the first contact region (13); providing a contact structure (41, 42, 43) of electrically conducting material in said aperture by means of electrochemical deposition.
||WO||WO/2014/035244 - LOCKING ASSEMBLY FOR LOCKING AN AIRCRAFT INTERIOR STRUCTURE TO AN INTERNAL MOUNTING FRAME IN AN AIRCRAFT CABIN||06.03.2014||
||PCT/NL2013/050625||DRIESSEN AEROSPACE GROUP N.V.||Korenromp, Maarten Michiel|
The invention relates to a locking assembly for locking an aircraft interior structure(13)to an internal mounting frame (2) comprising :a sliding element (1) which is suitable for insertion in the internal mounting frame (2),a height adjustment assembly, comprising a lower and an upper height adjustment part (4, 5). The assembly further comprises a fitting (6) attachable to the aircraft interior structure, having a recess wherein a projection (19) of the upper height adjustment part (5) is received, wherein the fitting (6) can be moved with respect to the projection(19) in a plane defined by X1- and Y1- directions. Further provided is a locking bolt (11) received in the upper height adjustment part (5) for locking the fixation element(9), the fitting(6), and the height adjustment parts(4, 5) to the sliding element (1).
||WO||WO/2014/035243 - PRESSURE SENSING ASSEMBLY||06.03.2014||
||PCT/NL2013/050624||NEDERLANDSE ORGANISATIE VOOR TOEGEPAST-NATUURWETENSCHAPPELIJK ONDERZOEK TNO||CHENG, Lun Kai|
A pressure sensing assembly (1), comprising: an elongate, axially extending tube (100), having a flexible tube wall (102) that encloses an inner pressure chamber (106); and at least one sensor unit (200), including: two tube wall fixation devices (210), connected to the tube wall (102) at respective axially spaced apart positions, and configured to fix respective diameters (D, d) of the tube wall at said positions; and a first strain sensing element (220), connected to the tube wall (102) at a first position axially in between said two tube wall fixation devices (210), and configured to provide a first signal indicative of an axial elongation of the tube wall resulting from a change in axial curvature of the tube wall when a pressure differential between the inner pressure chamber (106) and an outside environment (108) of the tube is applied across the tube wall at said first position.
||WO||WO/2014/035239 - A RETORT AND CORRESPONDING OVEN WITH DUCTWORK||06.03.2014||
||PCT/NL2013/050619||CLEAN FUELS B.V.||SIEMONS, Roland|
Summary: Method and system for processing a substance in a retort (1) wherein the retort comprises at least one flow deflector internal to the retort.A substance (8) is loaded into the retort (1), the retort (1) is positioned or located in an oven (9), a first (10) and second (11) duct are attached to the retort, a heat carrier fluidum is passed through the substance (8) in the retort (1) for drying and/or heating the substance inside the retort,an indirect heat transfer is applied over the wall (3) of the retort (1) and process progress is controlled by means of a controlled indirect heat transfer and/or a flow provided into the retort inlet comprising a heat carrier fluidum.
||WO||WO/2014/035240 - ESTER FORMATION||06.03.2014||
||PCT/NL2013/050621||TECHNISCHE UNIVERSITEIT DELFT||LÓPEZ GARZÓN, Camilo Sixto|
The present invention is in the field of a process for producing an ester, such as a biobased ester, from an aqueous biomass comprising solution, batch wise or continuously, wherein use of raw material is limited and if possible re-used. The present invention is in the field of green technology.
||WO||WO/2014/035241 - LOCKING ASSEMBLY FOR LOCKING AN AIRCRAFT INTERIOR STRUCTURE TO AN AIRCRAFT MAIN SUPPORT STRUCTURE||06.03.2014||
||PCT/NL2013/050622||DRIESSEN AEROSPACE GROUP N.V.||KORENROMP, Maarten Michiel|
The invention relates to a locking assembly (16) for locking an aircraft interior structure, such as a galley, to an aircraft main support structure, such as a floor hard point, comprising : -a cylindrical adjustment bushing (4) having a hollow cylindrical space (15), the adjustment bushing having an outer thread (12) that engages an inner thread of a through-hole (3) arranged in a fitting (7) attachable to or part of the aircraft interior structure, wherein the adjustment bushing can be rotated around its centre line to adjust the height of the fitting in a Z-direction, -a cylindrical outer eccentric bushing (2) inserted in the hollow cylindrical space (So) of the adjustment bushing, the outer eccentric bushing having an eccentric longitudinal hollow cylindrical space whose centre line is placed at a distance from the centre line of the cylindrical outer eccentric bushing, -a cylindrical inner eccentric bushing (1) inserted in the hollow cylindrical space of the outer eccentric bushing, the inner eccentric bushing having an eccentric longitudinal hollow cylindrical space (Si) whose centre line is placed at a distance from the centre line of the inner eccentric bushing, the inner and outer eccentric bushings (1, 2) allowing adjustment of the fitting in a plane perpendicular to the Z-direction, -a locking bolt (8) inserted in the hollow cylindrical space of the inner eccentric bushing, the locking bolt engaging an elongated projection (18) to lock the assembly (16), wherein the adjustment bushing is provided with a visual indicator (17) for indicating its relative position in Z-direction with respect to the fitting. The invention also relates to an aircraft comprising such a locking assembly, as well as a method for locking an aircraft interior structure to an aircraft main support structure.
||WO||WO/2014/035245 - HEMOSTATIC FOAM||06.03.2014||
||PCT/NL2013/050627||POLYGANICS B.V.||CHANDRASHEKHAR-BHAT, Bhushan|
The invention is directed a hemostatic foam, to a process for preparing a biodegradable hemostatic foam, and to the use of said foam. The hemostatic foam comprises a blend of a chitosan hemostatic agent and a polymer, which polymer provides the foam with a porosity of 85-99% and a foam density of 0.01-0.2 g/cm3.