176results about How to "Increase pitch" patented technology

A coaxial connector with a connector body is provided with a connector body bore. An annular coupling groove is provided in the connector body bore open to a cable end of the connector body. A clamp sidewall of the coupling grove is angled inward from a bottom of the coupling groove. A slip ring seated within the coupling body bore is provided with a grip surface. An annular compression body is positioned between the slip ring and the clamp sidewall. The connector body and the coupling body are coupled together via threads. The slip ring is dimensioned for axial advance of the coupling body along the threads to exert a compression force against the compression body to clamp a leading edge of the outer conductor between the compression body and the clamp sidewall.

A catheter comprising an elongate tubular member having a proximal end and a distal end, and a deflectable tip at the distal end of the elongate tubular member. The deflectable tip comprises a first helical coil having a first diameter and a second helical coil having a second diameter, the first diameter being larger than the second diameter. The first and second helical coils are arranged in the manner of a double helix. When viewed in cross-section, the first helical coil and the second helical coil are aligned at a first point on a circumference of each coil and misaligned at a second point on the circumference of each coil, where the second point is approximately 180 degrees from the first point. In certain embodiments the catheter further includes a dilatation balloon. Methods of use for crossing a chronic total occlusion are also described.

A catheter comprises an elongate tubular member having a proximal end and a distal end, and a deflectable tip at the distal end of the elongate tubular member. The deflectable tip comprises a first helical coil having a first diameter and a second helical coil having a second diameter, the first diameter being larger than the second diameter. The first and second helical coils are arranged in the manner of a double helix. When viewed in cross-section, the first helical coil and the second helical coil are aligned at a first point on a circumference of each coil and misaligned at a second point on the circumference of each coil, where the second point is approximately 180 degrees from the first point. In certain embodiments the catheter further includes a dilatation balloon. Methods of use for crossing a chronic total occlusion are also described.

A coaxial connector with a connector body is provided with a connector body bore. An annular coupling groove is provided in the connector body bore open to a cable end of the connector body. A clamp sidewall of the coupling grove is angled inward from a bottom of the coupling groove. A slip ring seated within the coupling body bore is provided with a grip surface. An annular compression body is positioned between the slip ring and a compression surface of the coupling body. The connector body and the coupling body are coupled together via threads. The slip ring is dimensioned for axial advancement of the coupling body along the threads to exert a compression force against the compression body to clamp a leading edge of the outer conductor between the slip ring and the clamp sidewall.

A personal respiratory protection device 10 that comprises a mask body 12 that has a structure 35 located on it for receiving a clean air supply source such as a filter cartridge 14. The clean air receiving structure 35 has a first threaded portion 34. The clean air supply source has a second threaded portion 58 that has a thread 60 that mates with a thread 36 of the first threaded portion 34. The first and second threaded portions 34 and 58 engage each other at a high thread pitch and include an integral détente. A stop prevents over-rotation of the clean air supply source 14 relative to the mask body 12 during the securement operation. The inventive device allows the clean air supply source 14 to be attached to the mask body 12 with minimal rotation and is sufficiently intuitive that users may only need one hand to attach and replace the clean air source component 14 without having to remove the respirator 10 from their face.

A mechanism for a rocker recliner chair is caused to have enhanced comfort and stability, to have enhanced ease of operation, and to require fewer parts for manufacture. The mechanism includes a rocker locking linkage arranged to include a drive link slidingly connected to a drive element, to drive a locking member for locking of the chair against rocking when the ottoman of the chair is extended. The drive link of the rocker locking linkage may also be arranged to be slidingly connected to a rocker cam assembly of the chair. The rocker locking linkage preferably includes a pair of locking links moveable to a substantially aligned orientation to lock a chair against forward rocking movement. The chair preferably includes an ottoman linkage including a slotted guide member.

A mechanism for a rocker recliner chair is caused to have enhanced comfort and stability, to have enhanced ease of operation, and to require fewer parts for manufacture. The mechanism includes a rocker locking linkage arranged to include a drive link slidingly connected to a drive element, to drive a locking member for locking of the chair against rocking when the ottoman of the chair is extended. The drive link of the rocker locking linkage may also be arranged to be slidingly connected to a rocker cam assembly of the chair. The rocker locking linkage preferably includes a pair of locking links moveable to a substantially aligned orientation to lock a chair against forward rocking movement. The chair preferably includes an ottoman linkage including a slotted guide member.

Instruments and methods for measuring a property of a shape memory alloy are provided. The instrument includes a base plate, a non-contact movable mass, a force gauge, an actuator, a biasing spring, a heater for heating the shape memory alloy, and a non-contact displacement detector. The biasing spring and the shape memory alloy are disposed whereby a force applied thereby is applied substantially through a center of stiffness of the movable mass. The displacement detector measures a displacement of the movable mass in a colinear direction with a direction of movement of the movable mass and with a direction of the force applied by the biasing spring and the shape memory alloy. The linear motion stage comprises a housing and at least one guide bar, and wherein a calculated axial expansion of the guide bar is substantially equal to a calculated axial expansion of the base plate.

Flow velocity sensor and a length sensor are provided on or near an edge of the lip plate which the air jet from the embouchure hole impinges against. Jet flow velocity Ue at the edge and a jet-blowout-outlet-to-edge distance d are detected by the sensors. Jet transfer time τe is calculated by an equation of τe=d / Ue, and a jet traveling angle θe′ is calculated by an equation of θe′=2πfso1×τe (where fso1 represents a frequency of a tone to be generated). When θe′ has decreased to π / 2 during tone generation in a primary mode, the mode changes to a secondary mode to raise the pitch of the currently generated tone by one octave. When θe′ has increased to 3π / 4 during tone generation in the secondary mode, the mode changes to the primary mode to lower the pitch of the currently generated tone by one octave.

The invention provides a single column maritime wind power generation device with a circumferential stabilizing column, and belongs to the technical field of ocean energy resource utilization. The single column maritime wind power generation device with the circumferential stabilizing column comprises a wind power generation set, a single column base, the circumferential stabilizing column, a supporting structure, a berthing system and a fixed ballast system; the wind power generation set is fixed on the single column base; the circumferential stabilizing column is fixed at the periphery of the single column base; both ends of the supporting structure are connected with the circumferential stabilizing column and the single column base respectively; the middle part and the bottom of the single column base are connected with the berthing system and the fixed ballast system respectively; and the berthing system is connected with the seabed. By arranging the circumferential stabilizing column, a larger waterline plane inertial moment can be obtained in a smaller waterline plane area; meanwhile, due to the low gravity center of the single column base, the stability requirement is met and the high water power performance is gained; therefore, a stable, economic and flexible floating base is provided for the wind power generation set, so the single column maritime wind power generation device with the circumferential stabilizing column is particularly applicable to deep water regions of the open sea.

The invention relates to an apparatus for inspecting a surface of a sample, wherein the apparatus comprises: at least one charged particle source for generating an array of primary charged particle beams, a condenser lens for directing all charged particle beams to a common cross-over, a lens system for directing the primary charged particle beams from the common cross-over towards the sample surface and for focusing all primary charged particle beams into an array of individual spots on the sample surface, and a position sensitive secondary electron detector positioned at least substantially in or near a plane comprising said common cross-over.

A towed personal watercraft apparatus includes a submergible unit and a platform. The submergible unit comprises at least two independent vertical stabilizers and one or more hydrofoil units mounted to at least one of the vertical stabilizers. One or more of the hydrofoil units is pivotally attached to the vertical stabilizers. Pivotal attachment can include a torsion spring or roller bearing to allow the hydrofoil units to pivot or rotate about the pitch axis of the platform, thereby improving stability of the towed personal watercraft. Rotation of the hydrofoil units can be limited for functional concerns and performance. For example, rotation of the hydrofoils about the pivot can be allowed in a first direction to prevent a nose dive, while being restricted in a second direction to facilitate a launch of the watercraft out of the water. The platform includes a user mount, such as foot holds or equivalents.

A winglet comprising a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. The winglet is manufactured by co-curing the upper skin to the upper main spar cap and the upper front spar cap; and co-curing the lower skin to the lower main spar cap and the lower front spar cap.

Disclosed herein is a display apparatus including a pixel-array unit, a scanner unit and a signal unit. The pixel-array unit has pixels laid out to form a matrix and each provided at an intersection of first and second scanning lines each oriented in a row direction of the matrix and a signal line oriented in a column direction of the matrix. The signal unit provides a video signal to the signal line. The scanner unit sequentially scans the pixels of the matrix in row units by supplying first and second control signals to the first and second scanning lines respectively.

A magnetic recording head for use in perpendicular magnetic recording having a design that allows the write coil to be manufactured by a damascene process for increased coil pitch and reduced coil resistance. The magnetic write head includes a photoresist dam structure that allows a hard baked photoresist to be formed that does not extend to the air bearing surface (ABS). Since the photoresist dam prevents the hard baked photoresist from reaching the ABS, the damascene process, in which the hard baked photoresist remains in the finished write head, can be used to produce the write head. The use of such a damascene process advantageously allows the space between the coil turns to be reduced, which maximizes the number of turns that can be used and also maximizes the number width to which the coil turns can be constructed, thereby minimizing the electrical resistance of the write coil.

Computerized tomography apparatus for reconstructing attenuation values within a volume comprising: an x-ray source situated operative to rotate about said volume, in a rotation plane, while irradiating at least a portion of the volume; a plurality of rows of x-ray detectors illuminated by said rotating x-ray source situated on an opposite side of the volume; a patient support operative to move a patient through a space between the source and detectors at an angle to the normal to the rotation plane, while the x-ray source illuminates the detectors; and a controller operative to compute the angle based on at least one of a radius R of said rotation, a radius r of said volume and a helix pitch, m, defined as a distance the patient support moves during a single rotation of the x-ray source.

The invention provides a high-frequency vertical spring probe card structure including a plurality of probes. Each of the probes includes at least one conducting layer and at least one insulating layer. The conducting layer includes a first contact end and a second contact end used for electrically contacting an external component while the probe is compressed and includes a probe body including at least one plate portion and at least one resilient portion connected to each other. The plate portion is used for supporting deformation of the resilient portion while the resilient portion is compressed vertically. The insulating layer includes at least one plate member tightly attached to the plate portion of the conducting layer correspondingly. The probe structure of the invention is simple and can be formed as multi-layer stack structure by electroplating through Lithographie GaVanoformung Abformung (LIGA) technology.

A method for measuring flatness of a sheet material in which a light and dark pattern composed by a light portion and a dark portion is projected onto a surface of the sheet material running in a longitudinal direction, a pattern image is acquired by photographing the light and dark pattern by an image pickup device having an image pickup visual field larger than a width of the sheet material, and the flatness of the sheet material is measured by analyzing the acquired pattern image. A staggered pattern is used for the projecting step and for light to be specularly reflected for receipt by the image pickup device. Calculating the flatness also includes steps of setting a shape measurement line, averaging picture element concentrations, calculating a distribution of the concentrations, and calculating the flatness based on surface shape using the distribution.

A process is disclosed for creating semiconductor devices such as RFID assemblies wherein an array of dies is spaced apart at a pitch matching the pitch of straps on a web of straps before they are mounted to a chip carrier substrate. The substrate is then cut into strips to form one or more linear aggregations of dies. The linear aggregation of dies is then transferred by an assembly mechanism onto the web of straps and electrically attached to a plurality of straps or interposers arranged in a corresponding array. The spacing, or pitch, between the dies in the die array may be changed to match the pitch of the straps or interposers in the corresponding array before or after a wafer substrate is removed from the die array. An RFID device created using the process inventive is also disclosed.

A vertical mixer having an improved auger for mixing bulk material is disclosed herein. The vertical mixer comprises a mixing chamber for receiving the bulk material. The mixing chamber being defined by a floor and a peripheral wall and includes a door for allowing exit of mixed bulk material. The vertical auger in the mixing chamber has an auger post and flighting including a bottom flight. The bottom flight has a front leading edge and an outside edge defining an outside footprint of the bottom flight. A slide plate is connected to the bottom flight for guiding bulk material at least inwards towards the auger post. The slide plate comprises a front corner; a bottom edge; and a top edge opposite the bottom edge. The bottom edge has a portion closer to the auger post than the front corner, and a portion extending inward on the bottom flight away from the outside edge of the bottom flight. The slide plate extends from the bottom flight at a shallow angle β relative the floor of the mixing chamber.

An optical filter for a plasma display device with improved shielding angle and transmittance, and a method of manufacturing the optical filter. The optical filter includes an external light shielding layer having a plurality of first openings; and an electromagnetic wave shielding layer integrated with the external light shielding layer on one surface of the external light shielding layer, where the electromagnetic wave shielding layer has a plurality of second openings corresponding to the plurality of first openings.

A system for controlling inbound transition of an aircraft includes a fuselage and first and second freewings pivotably mounted on opposing sides thereof. The system includes an airspeed sensor that outputs an airspeed indication signal. The system includes a controller for increasing aircraft engine thrust to substantially maximum for inbound transition, and for generating pitch and freewing control signals. The system includes actuators for actuating aircraft control surfaces in response to the pitch control signal to rapidly increase pitch of the fuselage to decelerate the aircraft, and for actuating freewing control surfaces in response to the freewing control signal to adjust lift produced by the freewings to oppose climbing of the aircraft due to the increase in engine thrust and the increase in the fuselage pitch. The controller is configured to decrease the engine thrust as the aircraft decelerates until the aircraft is in a hover mode.