Abstract: A seat back frame assembly and seat assembly are provided. The seat back frame assembly includes a pair of side members spaced apart from each other, a top member spaced apart from a bottom member, each of the top and bottom members interconnecting each of the pair of side members so as to define a peripheral edge, the peripheral edge enclosing a back space. An interference member is disposed within the back space and spaced apart from an inner surface of one of the pair of side members. The interference member disposed above a midpoint of the one of the pair of side members and includes a sliding surface angled obtusely with respect to the back space so as to direct an occupant forward of the back space and away from the side member when experiencing a side load.

Abstract: An aircraft store ejector systems and subsystems thereof. Embodiments can include a two-reservoir re-pressurization system wherein a remote reservoir is used to maintain desired pressure in a local ejector reservoir. The system can include a release valve having a vent valve and valve piston. The release valve can control release of pressurized gas to a pitch control valve. The pitch control valve can be configured to distribute the pressurized gas between two or more ejector piston assemblies. One or more of the ejector piston assemblies can include multiple concentric piston stages and piston chambers, the piston chambers configured to contain a volume of gas. The ejector piston assemblies can be configured to compress the volume of gas within the piston chambers as the piston stages are extended out from the aircraft. Such compression can provide a return force to the piston stages.

Abstract: A mobile concrete pump includes a supporting structure that can be placed directly or indirectly via an assembly frame on the running gear of an HGV chassis, for receiving functional units that form a support device and a placing boom. The placing boom is rotatably mounted on a boom pedestal that is integrated into the supporting structure, while the support device includes two telescopic tubes which are integrated into the supporting structure, cross over one another at different heights and have diagonal passages that are open at the front. A respective open space in the supporting structure lies below the upper and above the lower telescopic tube, each open space being separated from the neighboring telescopic tube by an intermediate base. A pre-fabricated liquid tank is inserted into at least one of the open spaces, the outer contour of the tank being geometrically adapted to the supporting structure and the tank supplementing and reinforcing the supporting structure.

Abstract: An expandable building assembly is provided, the building assembly having a retracted condition, in which the roof of the building has a first area, and an extended condition, in which the roof of the building has a second area, the second area being greater than the first, the assembly comprising a roof portion; and means for displacing and rotating the roof portion between the retracted condition and the expanded condition; whereby in the retracted condition, the roof portion is in a first position and at a first orientation, and in the extended condition, the roof portion is in a second position and at a second orientation, wherein the second position is displaced from the first position and the second orientation is rotated with respect to the first orientation. A building comprising one or more of the building assemblies is also provided.

Abstract: Provided is a system for monitoring temperature and pressure of an enclosed derrick structure communicating with a moonpool, which senses abnormal internal temperature and pressure of the enclosed derrick structure by monitoring the temperature and pressure of the enclosed derrick structure, thereby effectively coping with dangers. The system may include: one or more temperature sensors installed in the inside of the enclosed derrick to monitor an internal temperature of the enclosed derrick; one or more pressure sensors installed in the inside of the moonpool to monitor an internal pressure difference of the moonpool; and one or more damping units installed in a side of the enclosed derrick to supply air to the inside of the enclosed derrick or exhaust air to the outside of the enclosed derrick in order to cope with an abnormal internal temperature of the enclosed derrick and an abnormal internal pressure variation of the moonpool.

Abstract: A single-lance reel assembly comprising a reel assembly received onto and disposed to rotate about an axle at a rotary union. The reel assembly further comprises a plurality of spokes separating a rim from a hub. Hoses, electrical conduits, conductors or other similar carrier hardware deployed within hollow lances spooled on the reel assembly may be supplied via the rotary union and by further hose connection structure deployed on the hub and/or the rim. Embodiments of the reel assembly are powered by either a direct or indirect drive.

Abstract: Provided is an arctic ship with a derrick, which can stably maintain an internal environment of an enclosed derrick. The arctic ship with a derrick includes: the derrick forming an enclosed space blocked from outside air; a moonpool coupled to a lower portion of the derrick to communicate with the derrick and blocked from the outside air; and an air supply/exhaust device installed to communicate an inner space of the derrick or the moonpool with the exterior, wherein air condition of the inner space is maintained or controlled at a predetermined range by the air supply/exhaust device.

Abstract: A flow meter for measuring the flow of fluid through a pipe. The flow meter has an elongate member attached to an interior surface of the pipe. The elongate member has a leading end, a trailing end, a longitudinal axis, a first side, and a second side. The first side extends from the leading end to the trailing end and defines a cylindrical cross-sectional shape with a radius of curvature corresponding to the radius of curvature of the pipe and extending along an arc of less than 180 degrees. The second side extends from the leading end to the trailing end and is exposed to the interior of the pipe. The second side forms a constriction in a cross-sectional area of the pipe. Pressure sensors determine a pressure differential caused by the elongate member which is used to determine the volume of fluid flowing through the pipe.

Abstract: A programmable processor and method for improving the performance of processors by expanding at least two source operands, or a source and a result operand, to a width greater than the width of either the general purpose register or the data path width. The present invention provides operands which are substantially larger than the data path with of the processor by using the contents of a general purpose register to specify a memory address at which a plurality of data path widths of data can be read or written, as well as the size and shape of the operand. In addition, several instructions and apparatus for implementing these instructions are described which obtain performance advantages if the operands are not limited to the width and accessible number of general purpose registers.

Abstract: A plug element for an electrical contact of at least one electrical cable with plural electrical conductors includes a multi-part housing with a base element and at least one closure element and multiple contact pieces each including at least one plug contact for connecting an electrical conductor. A first group of at least one contact piece is allotted to a first service provided by the electrical conductors of a cable, and is assigned to a first formation of one or more chambers. At least one second group of at least one contact piece is allotted to at least one second service provided by a cable, and is assigned to at least one second formation of one or more chambers. A plug system includes a first plug element including male plug contacts and a second plug element including female plug contacts.

Abstract: A multi-flute ball end mill comprising a shank portion, a cutting edge portion having a ball-shaped tip portion, and 3 or more cutting edges formed in the cutting edge portion; each cutting edge being constituted by a peripheral cutting edge having a twist angle ? of 35-45°, and a ball-end cutting edge having a twist angle ? at the outermost peripheral point, the twist angle ? and the twist angle ? meeting the relation of ????7°, such that the ball-end cutting edge is smoothly connected to the peripheral cutting edge; the ball-end cutting edge having a radial rake angle of ?37° to ?11°; the peripheral cutting edge having a radial rake angle of 2-8°; and a center-lowered, inclined cutting edge integrally extending from a tip end of each ball-end cutting edge to a rotation center point, in a tip end portion of the ball portion near the rotation center point.

Abstract: Adsorbent materials comprising a core, for example CHA, and at least one coating, for example DDR, are provided herein. Adsorbent contactors and gas separation processes using the adsorbent materials are also provided herein.

Abstract: Structured adsorbent beds comprising a high cell density substrate, such as greater than about 1040 cpsi, and a coating comprising adsorbent particles, such as DDR and a binder, such as SiO2 are provided herein. Methods of preparing the structured adsorbent bed and gas separation processes using the structured adsorbent bed are also provided herein.

Abstract: Methods are provided for characterizing an aviation gasoline for use in a spark-ignited engine based on analysis methods traditionally used for compression-ignition fuels. For example, an aviation gasoline can be characterized based on a combustion delay for the aviation gasoline, a heat release rate for the aviation gasoline, or a combination thereof. Analyzing an aviation gasoline based on characteristics traditionally used for compression-ignition fuels can allow for distinction between types of aviation gasolines that may appear to be similar under conventional octane tests but that have substantially different performance characteristics.

Abstract: A method of predicting the tendency of a heavy oil feed to generate coke deposits in the FCC riser under a given set of operating parameters in the unit; thus, by utilizing operating parameters appropriate to the feed, the formation of coke deposits in the riser may be minimized. The margin between the theoretical dew point of the hydrocarbon feed established from unit operating parameters and the theoretical mix zone temperature in the feed injection zone of the unit is developed by applying a regression-derived linear model from multiple rigorous model runs. The mix zone of the unit is then operated at a temperature which reduces the level of riser coking predicted from this ascertainable margin or, at least, maintains it within levels which are predictable and acceptable.

Abstract: The present invention discloses an oil-in-water emulsion containing no surfactant, which comprises a metabolizable oil phase, an aqueous phase and oil-water amphipathic solid particles dispersed in the aqueous phase and having biocompatibility, wherein the oil phase comprises squalene or/and tocol; the aqueous phase is any one selected from the group consisting of purified water, water for injection, glycerine aqueous solution, buffering salts aqueous solution or clinically usable transfusion, or the combination of at least two selected therefrom; the solid particles have an average particle size in a scale of from nanometer to micrometer. The emulsion of the present invention can be used as vaccine adjuvant, drug delivery carrier or sustained/controlled-release carrier, and have the controllable properties. The resultant emulsion is stable, avoids the use of surfactants and can reduce the human poisoning and environmental pollution.

Abstract: Described herein are processes for production of hydrocarbon products comprising contacting a feed comprising methanol and/or dimethyl ether with a catalyst composition, which comprises a zeolite having a constraint index from 1-12 and an active binder comprising a metal oxide with a dehydrogenation function, under conditions sufficient to form the hydrocarbon product, wherein the hydrocarbon product comprises aromatics, olefins, and/or paraffins. Also described herein are catalyst compositions comprising a zeolite having a 10-/12-membered ring framework and a microporous surface area of at least 150 m2/g, and from ˜1 wt % to ˜10 wt % of a zinc oxide binder, the catalyst composition having a zinc to aluminum atomic ratio from ˜0.08 to ˜8.5.

Abstract: In a process for the catalytic conversion of organic oxygenates to hydrocarbons, a feed comprising at least one organic oxygenate is contacted with a zeolite catalyst under conditions effective to produce a hydrocarbon product comprising aromatics, olefins and paraffins. At least a fraction of the hydrocarbon product containing C4+ hydrocarbons, including at least part of the olefins, is then contacted with hydrogen in the presence of a hydrogenation catalyst under conditions effective to saturate at least part of the olefins in the C4+-containing fraction and produce a hydrogenated effluent containing less than 1 wt % olefins. The hydrogenated effluent is useful as a diluent for heavy crude oils.

Abstract: Power electronics modules having modular jet impingement assembly utilized to cool heat generating devices are disclosed. The modular jet impingement assemblies include a modular manifold having a distribution recess, one or more angled inlet connection tubes positioned at an inlet end of the modular manifold that fluidly couple the inlet tube to the distribution recess and one or more outlet connection tubes positioned at an outlet end of the modular manifold that fluidly coupling the outlet tube to the distribution recess. The modular jet impingement assemblies include a manifold insert removably positioned within the distribution recess and include one or more inlet branch channels each including an impinging slot and one or more outlet branch channels each including a collecting slot. Further a heat transfer plate coupled to the modular manifold, the heat transfer plate comprising an impingement surface including an array of fins that extend toward the manifold insert.

Abstract: An airbag system includes an inflatable airbag including an aperture and an indicator, the indicator viewable through the aperture when the inflatable airbag is in a packaged condition. A method of packaging an inflatable airbag includes rolling an inflatable airbag into a packaged configuration and confirming the indicator is visible through the aperture when the inflatable airbag is in the packaged condition.