Abstract: A door opening system and method include a mounting base, an engagement protuberance extending from the mounting base, a first securing assembly having a first suction cup coupled to the mounting base, and a second securing assembly having a second suction cup coupled to the mounting base. The first suction cup and the second suction cup are configured to secure the door opening system to a door of a structure. The engagement protuberance is configured to be engaged in a hands-free manner to open the door.

Abstract: A door opening system and method include a securing assembly including a suction cup that is configured to secure the door opening system to a door of a structure. An engagement protuberance is coupled to the suction cup. The engagement protuberance is configured to be engaged in a hands-free manner to open the door.

Abstract: A product display system includes a base, a shelving support assembly coupled to the base, and one or more shelves removably secured to the shelving support assembly. The one or more shelves are securable to the shelving support assembly in a first configuration and a second configuration that differs from the first configuration.

Abstract: A product display system includes a base, a shelving support assembly coupled to the base, and one or more shelves removably secured to the shelving support assembly. The one or more shelves are securable to the shelving support assembly in a first configuration and a second configuration that differs from the first configuration.

Abstract: A locking member is configured to couple to a suction cup and a suction securing nut. The locking member includes a locking ring, and a component support hook extending from the locking ring. The component support hook is configured to support at least a portion of a component.

Abstract: A wing assembly for an aircraft includes a torque box sleeve having an open end and a plurality of integral sides including leading, aft, top and bottom sides that jointlessly form a continuous surface having a generally airfoil shape. The wing assembly includes an internal support subassembly having a plurality of ribs coupled to a central spar. The internal support subassembly is formed into a single component outside the torque box sleeve and inserted into the open end of the torque box sleeve as the single component. The internal support subassembly is coupled to an interior of the torque box sleeve.

Abstract: Disclosed is a growing system that includes a hollow grow tower with planting units configured to hold plants disposed on the tower exterior where the planting units have a passage that extends into the tower interior. The tower also includes a drain port at one end and a water-dispensing nozzle at the other end. The nozzle includes outlet apertures in fluid communication with the interior of the tower where one or more of the nozzle outlet apertures may be square. An enclosure surrounds the tower, and one or more light sources are mounted on the enclosure to direct light towards the tower. The tower and enclosure can be connected to a suspension frame that suspends the entire system off the ground. The system may include a closed-loop irrigation system and a multi-tank cleaning system. System variables, such as water flow, temperature, lighting, and water nutrient level can be computer controlled.

Abstract: The present invention comprises a surface mount secondary containment system comprising prefabricated pieces that may be assembled to form a wall and adjoining corner with overlapping sections to capture leaks, spillage or the like from a primary liquid container member that may be constructed so that no ground damage and or penetration is done during construction and use.

Abstract: A direct bonding method for infrared focal plane arrays, includes steps of depositing a thin adhesion layer on infrared radiation detecting material, removing a portion of the thin adhesion layer with a chemical-mechanical polishing process, forming a bonding layer at a bonding interface, and bonding the infrared radiation detecting material to a silicon wafer with the thin adhesion layer as a bonding layer. The thin adhesion layer may include SiOx, where x ranges between 1.0 and 2.0. The thickness of the thin adhesion layer to form the bonding layer is 500 angstrom or less.

Abstract: One embodiment is an apparatus comprising an aircraft wing; a control surface hingedly connected to a trailing edge of the aircraft wing, wherein a slot is provided between the aircraft wing and the control surface; a seal disposed over the slot, the seal hingedly connected to the aircraft wing; a spring mechanism for preloading the seal against a surface of the control surface such that the gap is sealed with the control surface is in a first position relative to the aircraft wing; and at least one cam blade for lifting the seal from the surface of the control surface as the control surface moves from the first position to a second position relative to the aircraft wing and returning the seal to the surface of the control surface as the control surface moves from the second position to the first position.

Abstract: An off-highway recreational includes a frame, a prime mover, a transmission, an intermediate shaft and a main shaft. The transmission is mechanically coupled to receive power from the prime mover and to provide mechanical power at a transaxle output shaft. The intermediate drive shaft is mechanically coupled to the transaxle output shaft, wherein the intermediate drive shaft has a first diameter. The main drive shaft is mechanically coupled to the intermediate drive shaft, wherein the main drive shaft has a second diameter that is greater than the first diameter.

Abstract: A locking member is configured to couple to a suction cup and a suction securing nut. The locking member includes a locking ring, and a container retaining housing coupled to the locking ring. The container retaining housing is configured to retain a container.

Abstract: A direct bonding method for infrared focal plane arrays, includes steps of depositing a thin adhesion layer on infrared radiation detecting material, removing a portion of the thin adhesion layer with a chemical-mechanical polishing process, forming a bonding layer at a bonding interface, and bonding the infrared radiation detecting material to a silicon wafer with the thin adhesion layer as a bonding layer. The thin adhesion layer may include SiOx, where x ranges between 1.0 and 2.0. The thickness of the thin adhesion layer to form the bonding layer is 500 angstrom or less.

Abstract: A wing assembly for an aircraft includes a torque box sleeve having an open end and a plurality of integral sides including leading, aft, top and bottom sides that jointlessly form a continuous surface having a generally airfoil shape. The wing assembly includes an internal support subassembly having a plurality of ribs coupled to a central spar. The internal support subassembly is formed into a single component outside the torque box sleeve and inserted into the open end of the torque box sleeve as the single component. The internal support subassembly is coupled to an interior of the torque box sleeve.

Abstract: A product displaying holder system that is configured to removably secure to a surface of a component includes a base bar including one or more securing mounts, and one or more securing assemblies coupled to the securing mount(s). The securing assemblies are configured to removably secure the product displaying holder system to the surface of the component. One or more product holders are secured to the base bar.

Abstract: Focal plane arrays and infrared detector device having a transparent common ground structure and methods of their fabrication are disclosed. In one embodiment, a front-side illuminated infrared detector device includes a contact layer and a detector structure adjacent to the contact layer. The detector structure is capable of absorbing radiation. The front-side illuminated infrared detector device further includes a common ground structure adjacent the detector structure, wherein the common ground structure is transmissive to radiation having a wavelength in a predetermined spectral band, and the common ground structure has a bandgap that is wider than a bandgap of the detector structure. The front-side illuminated infrared detector device further includes an optical layer adjacent the common ground structure.

Abstract: A product displaying holder system is configured to be removably coupled to a surface of a component. The product displaying holder system includes a retaining bracket having a longitudinal main beam and one or more securing mounts. Holder channels are formed through the longitudinal main beam. One or more product holders are removably coupled to the retaining bracket. Each product holder includes a bracket-mating stud that is retained within one of holder channels. The holder channels allow the product holder(s) to be selectively positioned at different locations along the main beam. One or more securing assemblies are coupled to the securing mount(s). The securing assemblies are configured to securely couple the product displaying holder system to the surface of the component. In at least one embodiment, the securing mount(s) are perpendicular to the main beam.

Abstract: Disclosed embodiments include identity verification and management services in which users authenticate their identities during an enrollment process, and may access and modify their identity information via a secure portal. The enrollment process includes collecting various identifying data and biometric data of a user. A live interview portion during the enrollment process is used to check the liveness and verify the collected identifying data and biometric data. Once the user is enrolled, the user's identity can be verified for multiple entities using the same enrolled identity, and the user can manage the specific data used to verify their identity with different entities. This provides users with the ability to use their authenticated/verified identity across various industries, markets, locations, and the like, while keeping their identifying data private. Other embodiments may be described and/or claimed.

Abstract: A system and method for managing the qualifications of emergency management personnel through the use of at least partially automated qualification management devices or electronic Position Task Books (ePTBs) is presented herein. The system includes a network of participating organizations comprising governmental agencies, non-governmental organizations (NGOs), academic institutions, and the private sector. The qualification management devices or ePTBs are used to establish the suitability of the personnel or individual participants in the performance of emergency management duties in the areas of emergency preparedness, planning, response, recovery, etc. More specifically, the present invention is directed to a system and/or method for the management (including the issuance, execution, and review) of qualification management devices or ePTBs within a self-managed network of participating organizations using internet and mobile technology to deliver ePTBs.

Abstract: A system for enhancing driver situation awareness and environment perception around a transportation vehicle. The system incorporates a plurality of object detecting sensors. The sensors are arranged for monitoring at least one critical zone around the vehicle. A plurality of addressable light-emitting diodes are operatively associated with the object detecting sensors. The addressable light-emitting diodes are located on the vehicle for visual display to the driver. When a given sensor detects an object in the critical zone, a detection signal is transmitted to a LED controller. Upon receiving the detection signal, the LED controller transmits a control signal to selectively activate only those addressable light-emitting diodes which are associated with the given sensor, such that the activated light-emitting diodes visually communicate to the driver a location of the detected object in the critical zone.