Abstract: A golf club has a first shaft coupled to a club head, a second shaft configured to slidably engage a portion of the first shaft, a grip coupled to the second shaft, and an adjustable length shaft assembly received by the second shaft and configured to allow a portion of the first shaft to slide in relation to the second shaft in a first configuration, and to restrict a portion of the first shaft from sliding in relation to the second shaft in a second configuration. The grip is restricted from rotation about the first shaft or the second shaft as the first shaft slides in relation to the second shaft.

Abstract: A display system for sensing a finger of a user applied to the display system includes a display panel; a sensor for sensing the finger; a sensing light source configured to emit a first light having a first wavelength W1; and a reflective polarizer disposed between the display panel and the sensor. For a substantially normally incident light, an optical transmittance of the reflective polarizer versus wavelength for a first polarization state has a band edge such that for a first wavelength range extending from a smaller wavelength L1 to a greater wavelength L2 and including W1, where 30 nm?L2?L1?50 nm and L1 is greater than and within about 20 nm of a wavelength L3 corresponding to an optical transmittance of about 50% along the band edge, the optical transmittance has an average of greater than about 75%.

Abstract: A joint assembly joins first and second components about a common axis. The first component has a first end portion having a radially outwardly facing surface shaped to fit radially inside a second surface of a hollow second end portion of the second component to form an interface between the opposing first and second surfaces. The first and second surfaces have a concavity extending laterally with respect to the axis such that when the first and second surfaces are opposingly arranged the opposing concavities define a cavity at the interface. A retaining member is insertable into the cavity at the interface to prevent axial separation of the first and second components. One of the first and second end portions has a free end protrusion axially spaced from the concavity and the other of the first and second end portions has an axially extending recess arranged to receive the free end.

Abstract: An article includes a structural core, one or more friction pads, and a plurality of elongated fasteners. The structural core includes two core surfaces and a plurality of pockets extending between the core surfaces. Each friction pad includes a pad surface and a friction surface opposite the pad surface. Each pad surface includes a planar pad surface configured to contact the core surface and a plurality of bosses extending from the first planar pad surface and including a bore. Each planar pad surface is at least about 50% of a surface area of the respective first and second pad surfaces. The plurality of bosses engages with the plurality of pockets to position the respective first and second friction pads relative to the structural core. The plurality of elongated fasteners passes through bores of corresponding bosses of friction pads to fasten the friction pads to the structural core.

Abstract: A gas turbine engine for an aircraft comprising an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor; a fan located upstream of the engine core, the fan comprising a plurality of fan blades; a gearbox that receives an input from the core shaft and outputs drive to the fan so as to drive the fan at a lower rotational speed than the core shaft, and a front mount and a rear mount, the front and rear mounts being configured to connect the gas turbine engine to the aircraft, wherein the front mount is coupled to a casing of the engine core and the front mount is located at substantially the same axial position as a centre of gravity (CG) of the gas turbine engine or forward of the centre of gravity of the gas turbine engine.

Abstract: An article includes a structural core, one or more friction pads, and a plurality of elongated fasteners. The structural core includes two core surfaces and a plurality of pockets extending between the core surfaces. Each friction pad includes a pad surface and a friction surface opposite the pad surface. Each pad surface includes a planar pad surface configured to contact the core surface and a plurality of bosses extending from the first planar pad surface and including a bore. Each planar pad surface is at least about 50% of a surface area of the respective first and second pad surfaces. The plurality of bosses engages with the plurality of pockets to position the respective first and second friction pads relative to the structural core. The plurality of elongated fasteners passes through bores of corresponding bosses of friction pads to fasten the friction pads to the structural core.

Abstract: An article includes a structural core, one or more friction pads, and a plurality of elongated fasteners. The structural core includes two core surfaces and a plurality of pockets extending between the core surfaces. Each friction pad includes a pad surface and a friction surface opposite the pad surface. Each pad surface includes a planar pad surface configured to contact the core surface and a plurality of bosses extending from the first planar pad surface and including a bore. Each planar pad surface is at least about 50% of a surface area of the respective first and second pad surfaces. The plurality of bosses engages with the plurality of pockets to position the respective first and second friction pads relative to the structural core. The plurality of elongated fasteners passes through bores of corresponding bosses of friction pads to fasten the friction pads to the structural core.

Abstract: A joint assembly joins first and second components about a common axis. The first component has a first end portion having a radially outwardly facing surface shaped to fit radially inside a second surface of a hollow second end portion of the second component to form an interface between the opposing first and second surfaces. The first and second surfaces have a concavity extending laterally with respect to the axis such that when the first and second surfaces are opposingly arranged the opposing concavities define a cavity at the interface. A retaining member is insertable into the cavity at the interface to prevent axial separation of the first and second components. One of the first and second end portions has a free end protrusion axially spaced from the concavity and the other of the first and second end portions has an axially extending recess arranged to receive the free end.

Abstract: An article includes a structural core, one or more friction pads, and a plurality of elongated fasteners. The structural core includes two core surfaces and a plurality of pockets extending between the core surfaces. Each friction pad includes a pad surface and a friction surface opposite the pad surface. Each pad surface includes a planar pad surface configured to contact the core surface and a plurality of bosses extending from the first planar pad surface and including a bore. Each planar pad surface is at least about 50% of a surface area of the respective first and second pad surfaces. The plurality of bosses engages with the plurality of pockets to position the respective first and second friction pads relative to the structural core. The plurality of elongated fasteners passes through bores of corresponding bosses of friction pads to fasten the friction pads to the structural core.

Abstract: A gas turbine engine for an aircraft comprising an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor; a fan located upstream of the engine core, the fan comprising a plurality of fan blades; a gearbox that receives an input from the core shaft and outputs drive to the fan so as to drive the fan at a lower rotational speed than the core shaft, and a front mount and a rear mount, the front and rear mounts being configured to connect the gas turbine engine to the aircraft, wherein the front mount is coupled to a casing of the engine core and the front mount is located at substantially the same axial position as a centre of gravity (CG) of the gas turbine engine or forward of the centre of gravity of the gas turbine engine.

Abstract: A mechanism is provided for identifying an inter-relationship between a first process and the second process of a computer system. A correlation is detected between the first process and the second process based on a timing of the first process and the second process accessing a system resource of the computer system. An inter-relationship is then identified between the first process and the second process based on the detected correlation between the first process and the second process.

Abstract: A power supply apparatus receives a voltage from power rails on a circuit board. The power supply apparatus comprises a frame and arms connected to the frame. Each of the arms comprises a contact end. The frame positions the contact end of each of the arms to contact the power rails of the circuit board. The contact end is biased towards the power rails to maintain the contact end in contact with the power rails. The contact end comprises a curved planar surface having a first edge and a second edge that terminates at an end edge. The first edge and the second edge follow a curved line, while the end edge follows a straight line. The contact end comprises a non-linear slot extending from the end edge along the curved planar surface and is positioned equally between the first edge and the second edge.

Abstract: A power supply apparatus receives a voltage from power rails on a circuit board. The power supply apparatus comprises a frame and arms connected to the frame. Each of the arms comprises a contact end. The frame positions the contact end of each of the arms to contact the power rails of the circuit board. The contact end is biased towards the power rails to maintain the contact end in contact with the power rails. The contact end comprises a curved planar surface having a first edge and a second edge that terminates at an end edge. The first edge and the second edge follow a curved line, while the end edge follows a straight line. The contact end comprises a non-linear slot extending from the end edge along the curved planar surface and is positioned equally between the first edge and the second edge.

Abstract: A mechanism is provided for identifying an inter-relationship between a first process and the second process of a computer system. A correlation is detected between the first process and the second process based on a timing of the first process and the second process accessing a system resource of the computer system. An inter-relationship is then identified between the first process and the second process based on the detected correlation between the first process and the second process.

Abstract: A printing apparatus includes a media path within a body of the printing apparatus. The media path moves sheets of media through the body of the printing apparatus. A marking engine is also within the body of the printing apparatus. The media path supplies the printing media to the marking engine. A processor is within the body of the printing apparatus. The processor is operatively connected to the marking engine, and the processor controls actions of the marking engine. Sensors are within the body of the printing apparatus. The sensors are operatively connected to the processor, and the sensors are positioned along the media path. The sensors detect locations and conditions of the sheets of media as the sheets of media travel along the media path. The sensors have a first clip shape. Further, clip connectors are located within the body of the printing apparatus. The clip connectors are connected to the sensors. Additionally, light structures are connected to the clip connectors.

Abstract: A printing apparatus includes a media path within a body of the printing apparatus. The media path moves sheets of media through the body of the printing apparatus. A marking engine is also within the body of the printing apparatus. The media path supplies the printing media to the marking engine. A processor is within the body of the printing apparatus. The processor is operatively connected to the marking engine, and the processor controls actions of the marking engine. Sensors are within the body of the printing apparatus. The sensors are operatively connected to the processor, and the sensors are positioned along the media path. The sensors detect locations and conditions of the sheets of media as the sheets of media travel along the media path. The sensors have a first clip shape. Further, clip connectors are located within the body of the printing apparatus. The clip connectors are connected to the sensors. Additionally, light structures are connected to the clip connectors.

Abstract: Method for making carbon-carbon composite friction product, by: fabricating carbon fiber preform; heat-treating the carbon fiber preform; infiltrating the carbon fiber preform with a high carbon-yielding pitch using VPI (vacuum pressure infiltration) or resin transfer molding (RTM) processing; carbonizing the preform with an intermediate heat-treatment at 800-2000° C.; repeating the pitch infiltration and carbonization steps to achieve a final density of >1.75 g/cc; machining the surfaces of the preform; and applying an oxidation protection system. This approach overcomes problems inherent in lower density carbon-carbon composites by employing high carbon-yielding pitches to densify the carbon-carbon composites to a high density. The high carbon yielding pitches may include isotropic pitches, 100% anisotropic (mesophase) pitches, or mixtures of the two. They may be derived from petroleum, coal tar, or synthetic feedstocks.

Abstract: Method for making carbon-carbon composite friction product, by: fabricating carbon fiber preform; heat-treating the carbon fiber preform; infiltrating the carbon fiber preform with a high carbon-yielding pitch using VPI (vacuum pressure infiltration) or resin transfer molding (RTM) processing; carbonizing the preform with an intermediate heat-treatment at 800-2000° C.; repeating the pitch infiltration and carbonization steps to achieve a final density of >1.75 g/cc; machining the surfaces of the preform; and applying an oxidation protection system. This approach overcomes problems inherent in lower density carbon-carbon composites by employing high carbon-yielding pitches to densify the carbon-carbon composites to a high density. The high carbon yielding pitches may include isotropic pitches, 100% anisotropic (mesophase) pitches, or mixtures of the two. They may be derived from petroleum, coal tar, or synthetic feedstocks.

Abstract: Method of manufacturing carbon-carbon composite brake disc by: (a) providing textile-based preform in shape of annular brake disc, the preform having a volume 30% or more greater than the volume of the brake disc to be manufactured; (b) subjecting the preform to a first CVD processing for not more than 7.5 days to density it to not more than 1.0 g/cc; (c) machining the densified preform to a shape having a volume no more than 15% greater than the volume of the carbon-carbon composite brake disc to be manufactured: and (d) subjecting the preform to one or two additional cycles of CVD processing, to further densify it to a density of more than 1.7 g/cc. The preform is then machined to provide the carbon-carbon composite brake disc. The total CVD processing time in steps (b) and (c) is no longer than about 32.5 days.