Daniel I.
Daniel I. Campean, Portland, OR US
Patent application number | Description | Published |
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20140196351 | LOW PROFILE AUTO-LOCKING PINCH/TURN ADJUSTMENT KNOB - A compact adjustment knob for an optical, mechanical, or electronic device includes a spindle supported on the device for rotation about an axis to control a setting of the device, and a releasable automatically locking lock mechanism supported on the spindle for rotation therewith. The lock mechanism includes at least one manually depressible button accessible on an outer surface of the adjustment knob and connected to an actuator shaft that extends inwardly through a drive hole in an outer side wall of the spindle so that a force manually applied to the button is transmitted by the actuator shaft to drive the lock mechanism and rotate the spindle. The lock mechanism may include a lock sleeve that is biased to a normally locked position and driven along the axis by the actuator shaft when the button is depressed. | 07-17-2014 |
20150198415 | REFLEX SIGHT ADJUSTMENTS, BATTERY COMPARTMENT LID, AND ACCESSORY MOUNTING FEATURES - A battery compartment for a reflex sight is accessed via a pivoting lid that can be unlatched, opened, and closed by hand without tools and without removing the sight from its weapon. A button carried by the lid actuates a switch within the sight for changing a setting of the sight. Also disclosed is a reflex sight having mounting structures for accessories, such as an impact guard, a rain hood, or a rear iron sight for example. Positioning mechanisms for an LED or other aiming point display device of an aiming sight are also disclosed. | 07-16-2015 |
Daniel I. Codner, Isanti, MN US
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20140243946 | IMPLANTABLE MEDICAL DEVICE INCLUDING ASSEMBLY INCORPORATING RADIOPAQUE AGENT AND ELUTABLE DRUG INTO A POLYMERIC LEAD TIP - An assembly for an implantable device can be made from PEEK and can incorporate one or more radiopaque agents and one or more elutable drug components into a polymeric lead tip. The assembly can be machined or injection molded and can be configured, for example, as a housing for an active fixation lead or as an electrode base supporting a foil electrode. | 08-28-2014 |
Daniel I. Handjojo, Fremont, CA US
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20100098518 | IN/OUT DOOR FOR A VACUUM CHAMBER - A load lock chamber sized for a large area substrate is provided. The load lock chamber includes a housing comprising a door and a body having at least two sealable ports, a movable door associated with at least one of the sealable ports, and a door actuation assembly coupled between the door and the housing. The door actuation assembly further includes a pair of first actuators coupled to the door for moving the door in a first direction, and a pair of second actuators for moving the door in a second direction that is orthogonal to the first direction. | 04-22-2010 |
20120113559 | ELECTROSTATIC DISCHARGE PREVENTION FOR LARGE AREA SUBSTRATE PROCESSING SYSTEM - Embodiments of the invention relate to methods and apparatus for minimizing electrostatic discharge in processing and testing systems utilizing large area substrates in the production of flat panel displays, solar panels, and the like. In one embodiment, an apparatus is described. The apparatus includes a testing chamber, a substrate support disposed in the testing chamber, the substrate support having a substrate support surface, a structure disposed in the testing chamber, the structure having a length that spans a width of the substrate support surface, the structure being linearly movable relative to the substrate support, and a brush device having a plurality of conductive bristles coupled to the structure and spaced a distance away from the substrate support surface of the substrate support, the brush device electrically coupling the support surface to ground through the structure. | 05-10-2012 |
Daniel I. Newman, Lafayette Hill, PA US
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20160123182 | MODULAR THRUST SYSTEM - Disclosed herein is one embodiment of a thrust system that includes at least one modular thrust unit and at least one control module. The at least one modular thrust unit includes a base that is made from structural members that are inter-connectable in a plurality of different structural configurations. The at least one modular thrust unit further includes at least one thrust generator coupleable to the base in a thrust configuration and at least one power source operable to deliver power to the at least one thrust generator. The at least one control module is coupleable to the at least one modular thrust unit and operable to control at least one of the at least one thrust generator and the at least one power source. | 05-05-2016 |
Daniel I. Newman, Lafayette, PA US
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20150375860 | TILT-ROTOR VERTICAL-LIFT AIRCRAFT - Described herein is an aircraft that includes a fuselage with a higher portion and a lower portion. The aircraft also includes two fixed wings that are coupled to and extend from opposing sides of the lower portion of the fuselage. Additionally, the aircraft includes a tilt-rotor assembly that is coupled to each of the two fixed wings. | 12-31-2015 |
Daniel I. Resnicow, Boulder, CO US
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20120322862 | Aptamers to 4-1BB and Their Use in Treating Diseases and Disorders - The present disclosure relates generally to the field of nucleic acids and, more particularly, to aptamers capable of binding to 4-1BB; pharmaceutical compositions comprising such 4-1BB aptamers; and methods of making and using the same. | 12-20-2012 |
20140081011 | Aptamers to 4-1BB and Their Use in Treating Diseases and Disorders - The present disclosure relates generally to the field of nucleic acids and, more particularly, to aptamers capable of binding to 4-1BB; pharmaceutical compositions comprising such 4-1BB aptamers; and methods of making and using the same. | 03-20-2014 |
Daniel I. Rodriguez, Austin, TX US
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20150189754 | PRINTED CIRCUIT BOARD COPPER PLANE REPAIR - A device has a base with a mounting surface with a length and a stack, the stack having a diameter smaller than the length and fastened to the mounting surface. The stack may have a plurality of stack conductive layers in addition to a plurality of insulating layers that separate each of the plurality of stack conductive layers. The stack conductive layers may be separated in a manner that aligns them with corresponding printed circuit board conductive layers when the stack portion of the device is inserted into an aperture in a printed circuit board. | 07-02-2015 |
20150282331 | PRINTED CIRCUIT BOARD COPPER PLANE REPAIR - A device has a base with a mounting surface with a length and a stack, the stack having a diameter smaller than the length and fastened to the mounting surface. The stack may have a plurality of stack conductive layers in addition to a plurality of insulating layers that separate each of the plurality of stack conductive layers. The stack conductive layers may be separated in a manner that aligns them with corresponding printed circuit board conductive layers when the stack portion of the device is inserted into an aperture in a printed circuit board. | 10-01-2015 |
Daniel I. Saper, Milwaukee, WI US
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20110278190 | SYSTEM AND METHOD TO COMMUNICATE DRAIN CLEANING BENEFITS TO CONSUMERS - A packaging system for a liquid drain clog remover, the packaging system having: (a) a container; and (b) a product label. The product label includes indicia depicting at least three steps in a drain clog removal process. The three steps may be selected from the group consisting of: an initialization step, an activation step, a contact step, and a removal step. | 11-17-2011 |
Daniel I. Ticle, Turda RO
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20150199514 | Computer Security Systems And Methods Using Virtualization Exceptions - Described systems and methods enable a host system to efficiently perform computer security activities, when operating in a hardware virtualization configuration. A hypervisor exposes a virtual machine on the host system. In some embodiments, the hypervisor further configures a processor of the host system to generate a virtualization exception in response to detecting a memory access violation, and to deliver such exceptions to a computer security program operating within the virtual machine. The hypervisor may further set access permissions to a section of memory containing a part of a function targeted for hooking, so that an attempt to execute the respective target function triggers a virtualization exception. Some embodiments thus achieve hooking of the target function without resorting to conventional methods, such as patching, inline hooking, and MSR hooking. | 07-16-2015 |
Daniel I. Udriste, Weston, FL US
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20080315643 | One-piece dress cover for aircraft seat - A one-piece upholstery cover that covers all the visible surfaces of a typical seat such as seatback cushion, seat pan cushion, seat pan extension cushion, leg rest cushion, and leg rest extension cushion. A seat covering system is also disclosed. The seat covering system includes a single elongated piece of upholstery having a first end and a second end and a loop portion intermediate the first and second ends. A first attachment portion is adjacent to the first end of the upholstery, and at least one spring mechanism attached to the second end. A first and second pivot member are attached to opposite sides of a seat back of a reclining chair. These first and second pivot members are also fixed to a seat pedestal while a connecting member having a first end attached to the first pivot member and a second end attached to the second pivot member extends through the loop portion of the elongated piece of upholstery. | 12-25-2008 |
20080315657 | Seat headrest - A headrest support assembly capable of moving a headrest simultaneously in an up/down and fore/aft position. The headrest support assembly is located in a seat back and includes a headrest frame mounted on a support bracket, the support bracket includes a first and second guide track spaced apart from one another. Each guide track defines a substantially vertical first channel and a curved second channel therein. A first and second support pillar is mounted to the headrest frame. These first and second support pillars are located adjacent to the first and second guide track, respectively. A first and second guide roller is located on each of the first and second support pillars. The first guide roller is positioned within the first channel and the second guide roller is positioned within the second channel of the respective guide tracks. | 12-25-2008 |
20100007185 | ONE-PIECE DRESS COVER FOR AIRCRAFT SEAT - A one-piece upholstery cover that covers all the visible surfaces of a typical seat such as seatback cushion, seat pan cushion, seat pan extension cushion, leg rest cushion, and leg rest extension cushion. A seat covering system is also disclosed. The seat covering system includes a single elongated piece of upholstery having a first end and a second end and a loop portion intermediate the first and second ends. A first attachment portion is adjacent to the first end of the upholstery, and at least one spring mechanism attached to the second end. A first and second pivot member are attached to opposite sides of a seat back of a reclining chair. These first and second pivot members are also fixed to a seat pedestal while a connecting member having a first end attached to the first pivot member and a second end attached to the second pivot member extends through the loop portion of the elongated piece of upholstery. | 01-14-2010 |
20100102611 | SEAT SWIVEL WITH BRAKE FOR INFINITE ROTATIONAL POSITION ADJUSTMENT - A seat swivel for providing angular adjustment of a seat to an infinite number of rotational positions with respect to a seat base. The seat swivel includes a swivel assembly having a swivel plate rotatably supported between a pair of fixed plates, the swivel plate being adapted to be affixed to the seat and the fixed plates being adapted to be affixed to a seat base. The seat swivel further includes a brake assembly having a mechanism for releasably retaining the seat in any one of the infinite number of positions when the seat is subjected to a first dynamic impact loading, the mechanism being either mechanically or electrically actuated, the mechanism being adapted to withstand a dynamic impact loading of up to about 16 g in at least one rotational position of the seat. | 04-29-2010 |
Daniel I. Udriste, Coral Springs, FL US
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20130113250 | ELECTROMECHANICAL ACTUATION SYSTEM FOR AIRCRAFT PASSENGER SUITES AND METHOD - An electromechanical actuation system for an aircraft passenger suite for allowing passenger-initiated adjustment of a passenger seat and related passenger accoutrements including a suite control unit configured to receive command signals from a user interface, and a first line replacement unit comprising a first integral electronic control unit and a second line replacement unit coupled to the first line replacement, wherein the first electronic control unit controls operation of the first line replacement unit and the second line replacement unit in response to command signals received from the suite control unit. | 05-09-2013 |