Abstract: Methods and systems are disclosed for obtaining a first image of a tray, determining a presence or absence of one or more first patterns in the first image, determining a rotation of each the one or more first patterns in the first image, and performing an action based on the presence or absence and the rotation of the one or more first patterns in the first image.

Abstract: Methods and systems are disclosed for obtaining a first image of a tray, determining a presence or absence of one or more first patterns in the first image, determining a rotation of each the one or more first patterns in the first image, and performing an action based on the presence or absence and the rotation of the one or more first patterns in the first image.

Abstract: Methods and systems are disclosed for obtaining a first image of a tray, determining a presence or absence of one or more first patterns in the first image, determining a rotation of each the one or more first patterns in the first image, and performing an action based on the presence or absence and the rotation of the one or more first patterns in the first image.

Abstract: Methods and systems are disclosed for obtaining a first image of a tray, determining a presence or absence of one or more first patterns in the first image, determining a rotation of each the one or more first patterns in the first image, and performing an action based on the presence or absence and the rotation of the one or more first patterns in the first image.

Abstract: Methods and systems are disclosed for obtaining a first image of a tray, determining a presence or absence of one or more first patterns in the first image, determining a rotation of each the one or more first patterns in the first image, and performing an action based on the presence or absence and the rotation of the one or more first patterns in the first image.

Abstract: A nacelle for a turbofan aircraft engine having a fan case with a fan case forward edge includes an inlet inner barrel having an inner barrel forward edge and an inner barrel aft edge. The inner barrel aft edge is configured to be affixed to the fan case forward edge in a stationary position on the engine. The nacelle also includes a translating inlet cowl having an inlet lip with an aft inlet lip edge and an outer skin with rear edge. The translating inlet cowl is configured to be movably attached to one or more stationary portions of the engine such that the inlet cowl is selectively movable between a stowed flight position and an extended service position.

Abstract: A nacelle for a turbofan aircraft engine having a fan case with a fan case forward edge includes an inlet inner barrel having an inner barrel forward edge and an inner barrel aft edge. The inner barrel aft edge is configured to be affixed to the fan case forward edge in a stationary position on the engine. The nacelle also includes a translating inlet cowl having an inlet lip with an aft inlet lip edge and an outer skin with rear edge. The translating inlet cowl is configured to be movably attached to one or more stationary portions of the engine such that the inlet cowl is selectively movable between a stowed flight position and an extended service position.

Abstract: The adjustable to a user's upper extremity the exoskeleton structure provides testing and exercising of the whole upper extremity in a realistic manner without infringement of a locomotor act and with selective biomechanical information and exercise loading in each anatomical motion direction of every joint simultaneously. The exoskeleton structure comprises jointed means for connection with a user's shouldergirdle, upperarm, forearm, and hand. Those means include measuring-loading blocks to measure muscle forces and joint angles and to apply a dosed exercise load. All measuring-loading blocks in the exoskeleton structure are identical. The exoskeleton structure is able to provide a realistic and comprehensive information about both a complex locomotor act and a selective mono-planar motion for both isometric and isotonic muscular contractions.

Abstract: Disclosed are personal care compositions, such as haircare, cosmetic and nail compositions containing linear toughened silicone grafted polymers.

Abstract: Disclosed is a high precision resistance device that allows a user to set and hold exact load amount and pattern of loading in exercise machine. The one embodiment of the device includes a hydraulic cylinder having a piston and two valves, two driving members, a driven member, a cam, and a connecting rod. Each valve can change flow section area in the hydraulic cylinder. One valve manually sets an original level of an exercise load. Second valve is adjusted by the cam to maintain a predetermined pattern of the exercise load. The cam can be easily change for another one having different shape and providing accordingly the predetermined pattern of the exercise load, that is pattern of loading applied to a user's muscular system in operation. Driving members are adapted to receive a plurality of exercise accessories. The resistance device can be installed in actually any conventional fitness machine to transform it into precise equipment for medical research, therapy, and rehabilitation.

Abstract: A personal care composition comprising: (a) a silicone grafted adhesive polymer, said polymer being characterized by an organic polymeric backbone wherein said backbone comprises: (i) at least one monomer wherein when said monomer is polymerized as a homopolymer having a Tg of from about −120° C. to about 25° C. and (ii) at least one monomer wherein when said monomer is polymerized as a homopolymer having a Tg of from above about 25° C. to about 250° C. wherein said silicone grafted adhesive polymer has silicone macromers grafted to said backbone and wherein the number average molecular weight of said silicone macromers is greater than about 1000; and (b) a personal care carrier.

Abstract: Disclosed are linear toughened silicone grafted polymers useful in personal care compositions and the like.