Abstract:
An inbound message including medical record content may be received. The inbound message may indicate a healthcare entity and a vendor entity. It may be determined, from the healthcare entity and stored correspondences between medical record formats and healthcare entities, that the medical record content of the inbound message is in a first medical record format. Which configuration record of stored configuration records specifying combinations of sets of rules may be determined to apply as a translation to the inbound message based upon the medical record content of the inbound message and the first medical record format. The sets of rules as indicated by the configuration record may be accessed and applied to the inbound message to translate the medical record content in the inbound message from the first medical record format to the standardized format. The standardized format may be transmitted to the vendor entity.
Abstract:
A method is performed in a network security system implemented in a computer or electronic device that is coupled to secured online resources for detecting unauthorized accesses of those secured online resources. The method includes monitoring a user activity session. It is determined whether the user activity session is indicative of a hidden session by an attacker, where the determination includes comparing the user activity session to an average user activity session.
Abstract:
A method to detect potential problems within a heterogeneous and diverse application environment. Operations data is received from a plurality of application servers within the application environment. The operations data pertains to operations performed at the plurality of application servers over a predetermined time interval. The operations data is aggregated. The aggregated data is compared to reference data, and a potential problem within the application environment is detected if the aggregated data deviates from the reference data in a predetermined manner.
Abstract:
A fairing kit for a gas turbine engine, where the engine has a core gas turbine engine, a fan rotor, and a plurality of external fan blades attached to the fan rotor and powered by the core gas turbine engine. The core gas turbine engine has an annular splitter for directing a portion of incoming airflow into the core gas turbine engine. The fairing kit comprises: a) a fairing; b) a plurality of fasteners for securing the fairing to the core gas turbine engine; and c) a conformable seal for sealing mating surfaces of the fairing and the core gas turbine engine.
Abstract:
A method for preparing a gas turbine engine for a ferry flight, where the engine has a core gas turbine engine, a spinner, and a plurality of external fan blades powered by the core gas turbine engine. The core gas turbine engine has an annular splitter for directing a portion of incoming airflow into the core gas turbine engine. The method comprises the steps of: a) removing the spinner; b) removing the fan blades; and c) securing a fairing in sealing engagement with the core gas turbine engine.
Abstract:
A liquid, eye-instillable preparation comprises a viscosity-enhancing agent comprised of one or both of sodium hyaluronate and chondroitin sulphate, a preservative comprised of polyhexanide, and one or more carriers in which the agent and the preservative are dispersed.
Abstract:
A method to detect potential problems within a heterogeneous and diverse application environment. Operations data is received from a plurality of application servers within the application environment. The operations data pertains to operations performed at the plurality of application servers over a predetermined time interval. The operations data is aggregated. The aggregated data is compared to reference data, and a potential problem within the application environment is detected if the aggregated data deviates from the reference data in a predetermined manner.
Abstract:
A pair of men s shorts, including under shorts, has a typical chassis with an abdomen opening, a right pant leg and a left pant leg. The user's genitals pass through an opening on the front of the chassis whenever the shorts are being worn. A hammock overlies the opening and is anchored to the chassis at two points on the right out seam, one point below the other, and two points on the left out seam, symmetrical with the right out seam attachment. The hammock is also attached to the chassis at the waist band and at the lower edge of the opening just above the left and right inseam joinder area. The hammock by being anchored at the out seams and being non-stretching in a transverse direction, acts as a sling in supporting the genitals of the user.
Abstract:
A trim panel (10) includes at least one integrally-formed first member (12) and at least one integrally-formed second member (14) extend from an outboard surface (16) of the trim panel (10). The at least one integrally-formed first member (12) engages an inboard surface (42) of a barrier (36) to push the barrier (36) in an outboard direction. The at least one integrally-formed second member (14) extends through an opening or perforation (40) of the barrier (36) to retain the barrier (36) to the trim panel (10). The barrier (36) may be a water/acoustic ingression barrier (36). The at least one integrally-formed first member (12) causes an adhesive bead (44) arranged on an outboard surface (46) of the barrier (36) to positively engage an inboard surface (48) of an inner door panel (38). The at least one integrally-formed second member (14) extends through an opening or perforation (40) of the barrier (36) to retain the barrier (36) with the interior door trim panel (10).
Abstract:
This invention relates to improving the tolerance of composite laminate structures to damage and/or delamination, resulting in weakening of the structure and/or to reducing the possibility of such damage and/or delamination. In particular, but not exclusively the invention relates to protecting the end surfaces of composite laminate structures present on aircraft from impact damage. The invention provides aircraft component comprising a composite laminate structure, the composite laminate structure including an end surface at which a multiplicity of the layers of the laminate structure terminate, wherein the aircraft component further comprises a deflecting surface mounted to the composite laminate structure for protecting the end surface from direct impacts. In one embodiment, the end surface of the composite laminate structure has a convex cross-section and the deflecting surface comprises laminate material laid over the end surface. In a further embodiment, the deflecting surface comprises an inert strip.