Abstract: An air swirler arrangement comprises a coaxial arrangement of an inner and an outer air swirler passage. Each air swirler passage comprises a radial flow swirler. Air swirler arrangement comprises a coaxial arrangement of first, second and third members. Second member has radially extending upstream portion spaced axially from first member and a convergent portion. Third member has a radially extending upstream portion spaced axially from the upstream portion of second member and a radially inner surface having convergent and divergent downstream portions and a radially outer surface having a divergent downstream portion. First, second and third members the vanes of the radial flow swirlers is a monolithic structure. Plurality of circumferentially spaced passages are provided within the third member and each passage has an inlet in the surface and an outlet arranged to direct fluid onto the divergent portion of the surface or the surface of the third member.

Abstract: A composite panel composed of a fibre reinforced resin matrix composite material, wherein the panel comprises: a panel portion comprised of a first multilayer laminate including a plurality of first plies of fibre reinforced resin matrix composite material, wherein at least one of the first plies includes a first fibrous layer of a plurality of non-woven carbon fibres which are substantially randomly oriented, and a reinforcement portion which is integrally moulded with the panel portion and is located at one or more locations on a surface of the panel portion to provide one or more primary structural regions of the composite panel, the reinforcement portion being comprised of a second multilayer laminate including a plurality of second plies of fibre reinforced resin matrix composite material, wherein at least one of the second plies includes a second fibrous layer of a plurality of non-woven carbon fibres which are substantially randomly oriented, wherein in at least one primary structural region both the p

Abstract: Illustrative embodiments may provide for an apparatus and method of controlling the folding of a wing. The apparatus may include a sensor, an actuator, and a wing fold controller. The method may include receiving a status of at least one of an aircraft and a wing fold system of the aircraft by the wing fold controller of the wing fold system. The method may also include receiving an automated command by the wing fold controller in response to receiving the status. The method may also include operating the wing fold system by the wing fold controller based on the automated command and the status. The method may also include transitioning a wingtip of a wing of the aircraft to one of a flight position and a folded position by an actuator of the wing fold system in response to commands from the wing fold controller.

Abstract: A method of moulding a moulding material to form a laminated moulded part of fibre-reinforced resin matrix composite material, the method comprising the steps of: i. providing in a mould tool a preform comprising a central layer portion and a peripheral edge portion around at least a part of a periphery of the central layer portion, the central layer portion including at least one fibrous layer and a first resin, and the edge portion comprising a second resin including a plurality of individual fibres dispersed therein; ii. closing the mould tool to define a closed mould cavity containing the moulding material; and iii.

Abstract: A motor adapter assembly can couple a motor shaft for a ceiling fan motor to a downrod. The motor adapter assembly can include a base plate, a cradle with arms extending through the base plate, and a threaded bushing secured between the arms of the cradle. Threading a cap to the threaded bushing can be used to pivot the downrod between an upright position and a pivoted position.

Abstract: A kit or assembly for a ceiling fan can include a downrod and a set of electrical wires. The downrod can include a sidewall defining an interior. An opening can be provided in the sidewall for accessing the interior. The set of electrical wires can extend through the interior of the downrod, having first and second sets of wire tips, and can be longer than the downrod. An optional electrical connector can be provided on one of the first or second sets of wire tips.

Abstract: A data collection and display system for use in a combat sport including: i. A trunk protector for a combat sport participant, the trunk protector including: a. protective padding, b. at least one impact sensor, c. at least one microprocessor integral with the protective padding, for collecting and analyzing data from the at least one impact sensor, d. at least one display area, integral with the trunk protector, for displaying information related to the combat sport and combat sport participant; and an energy based method for scoring combat sports.

Abstract: Systems and methods for sequencing HVAC equipment of an HVAC system using data recorded in situ to build a model capable of making predictions about equipment efficiency and using that information, in combination with predictions about building load, to produce an operational sequence for the HVAC equipment that promotes an improved or optimized overall energy efficiency for the HVAC system. In one embodiment, the process is automated and utilizes Bayesian computational models or algorithms to generate an initial sequence. The process reduces engineering hours and may advantageously provide a means to predict potential sequencing problems for similar types of HVAC equipment.

Abstract: A method of press molding a molding material to form a vehicle body panel of fiber-reinforced resin matrix composite material, the vehicle body panel having a front A-surface and a rear B-surface, the method comprising the steps of: i. providing a heated mold tool having a lower mold part and an upper mold part, the upper mold part having a first molding surface for molding a front A-surface of the vehicle body panel and the lower mold part having a second molding surface for molding a rear B-surface of the vehicle body panel; ii. providing a multilaminar panel of molding material comprising at least one layer of fibers and at least one layer of resin, the multilaminar panel having first and second opposite major surfaces, a surface resin layer of the multilaminar panel being at or adjacent to the first major surface; iii. locating the molding material in the mold tool; iv. closing the mold tool to define a substantially closed mold cavity containing the molding material; v.

Abstract: The present proposals relate to an insecticide or miticide composition which demonstrates low phytotoxicity even at relatively high concentrations combined with highly effective insecticidal and miticidal activity. The composition comprises: a fatty acid/amino acid salt, the fatty acid component comprising: one or more unsaturated fatty acids having from 14 to 22 carbon atoms; and one or more saturated fatty acids having from 8 to 18 carbon atoms; wherein the one or more saturated fatty acids having from 8 to 18 carbon atoms forms at least 15 wt. % of the fatty acid component, and wherein the weight ratio of (unsaturated fatty acids having from 14 to 22 carbon atoms) to (saturated fatty acids having from 8 to 18 carbon atoms) is at least 1. Uses of the compositions and methods of killing insects or mites using the compositions also form part of the proposals.

Abstract: An improved chafer rack and panel assembly having hingedly attached and removable wind-shield panels connected to integral wire bars of the chafer rack.

Abstract: A kit or assembly for a ceiling fan can include a downrod and a set of electrical wires. The downrod can include a sidewall defining an interior. An opening can be provided in the sidewall for accessing the interior. The set of electrical wires can extend through the interior of the downrod, having first and second sets of wire tips, and can be longer than the downrod. An optional electrical connector can be provided on one of the first or second sets of wire tips.

Abstract: A closet storage system generally includes a hang rod, a back channel, first and second side brackets, first and second shelf trims, first and second end cups, a shelf supportable by the back channel and the first and second side brackets, and at least one support bracket. The back channel is mountable along a back wall of a closet. The first and second side brackets are mountable along sidewalls of the closet. The first end cup is configured to be coupled and/or supported generally between portions of the first shelf trim and the first side bracket. The second end cup is configured to be coupled and/or supported generally between portions of the second shelf trim and the second side bracket. The hang rod is supportable beneath the shelf when first and second end portions of the hang rod are supported by the respective first and second end cups.

Abstract: A shock absorber assembly is configured to be operatively connected to a drive shaft of a power drive unit (PDU) of an aircraft. The shock absorber assembly may include a first hub, a second hub, and a bull gear having at least a portion sandwiched between the first and second hubs. The bull gear is configured to rotate independently of the first and second hubs a controlled distance in response to a mechanical malfunction of the PDU.

Abstract: A method of manufacturing a foam body having an anisotropic cell structure, the method including the steps of: expanding a polymer at an elevated temperature to form an initial foam body; and cooling the initial foam body under a negative pressure. There is also provided a method of manufacturing a foam body having an anisotropic cell structure, the method including the steps of: (a) in a first expansion step, expanding a foamable polymer composition substantially isotropically to form an initial foam body having an isotropic cell structure; and (b) in a second expansion step, expanding the initial foam body anisotropically in a selected direction under a negative pressure which applies an expanding force in the selected direction to provide a final foam body having an anisotropic cell structure. Apparatus for the methods are also disclosed.

Abstract: A flap skew detection system is configured to detect flap skew of one or more flaps moveably secured to one or more wings of an aircraft. The flap skew detection system includes a flap support assembly that couples a flap to a wing. The flap support assembly includes a fixed portion that is configured to secure to the wing, a moveable portion that is moveably coupled to the fixed portion and configured to securely support the flap, and a link moveably coupled to the fixed portion and the moveable portion. The link includes a cylinder defining an internal chamber including a hydraulic fluid chamber, a piston having a piston head within the internal chamber, and hydraulic fluid retained within the hydraulic fluid chamber. A pressure detector is fluidly coupled to the hydraulic fluid chamber. The pressure detector is configured to detect a fluid pressure of the hydraulic fluid pressure within the hydraulic fluid chamber.

Abstract: Methods for rapidly concentrating a food sample for efficient detection of bacteria are disclosed. A microfiltration approach followed by centrifugation was used to concentrate the cells with an enzyme (e.g., a protease) added at the beginning of the process to facilitate more efficient micro-filtering. The enzyme was found to have no significant effect on cell viability.

Abstract: A composite panel including a multilayer laminate with a plurality of central plies of fibre reinforced resin matrix composite material, wherein at least one of the central plies includes a first fibrous layer of a plurality of non-woven carbon fibres which are substantially randomly oriented, and a rear reinforcement layer which is integrally moulded with the central multilayer portion the reinforcement layer being comprised of a rear ply of fibre reinforced resin matrix composite material, wherein the rear ply includes a second fibrous layer of a plurality of continuous fibres which extend continuously from at least one portion of a first edge of the rear ply to at least one portion of an opposite second edge of the rear ply.

Abstract: A method of press molding a molding material to form a molded part of fiber-reinforced resin matrix composite material, the method comprising the steps of: i. providing a mold tool having a lower mold part and an upper mold part, the upper mold part having a first molding surface for molding a first molded surface of the molded part and the lower mold part having a second molding surface for molding a second molded surface of the molded part; ii. providing a multilaminar panel of molding material comprising at least one layer of dry fibers and at least one layer of resin, the multilaminar panel having first and second opposite major surfaces; iii. locating the molding material in the mold tool; iv. progressively closing the mold tool to define a substantially closed mold cavity containing the molding material, the closing step having: I. a first stage prior to both the first molding surface contacting the first major surface and the second molding surface contacting the second major surface and II.

Abstract: A method of press molding a molding material to form a molded part of fiber-reinforced resin matrix composite material, the method comprising the steps of: i. providing a mold tool having a lower mold part and an upper mold part, the upper mold part having a first molding surface for molding a first molded surface of the molded part and the lower mold part having a second molding surface for molding a second molded surface of the molded part; ii. providing a multilaminar panel of molding material comprising at least one layer of fibers and at least one layer of resin, the multilaminar panel having first and second opposite major surfaces; iii. locating the molding material in the mold tool; iv. progressively closing the mold tool to define a substantially closed mold cavity containing the molding material, the closing step including: a. a preliminary closing phase to achieve mutual engagement between the lower and upper mold parts, b.