Abstract: A propulsion system for an aircraft, comprising at least one rotor and a nacelle fairing extending around the at least one rotor with respect to an axis of rotation of the rotor, the nacelle fairing comprising: an upstream section forming an inlet section of the nacelle fairing; a downstream section wherein a downstream end forms an outlet section of the nacelle fairing; and an intermediate section connecting the upstream and downstream sections, wherein the downstream section comprises a radially inner wall and a radially outer wall made of a deformable shape memory material, and further comprising at least one actuator mechanism with at least one cylinder configured to cooperate with one or more components, projections, etc., embedded in an inner surface of the radially outer wall so as to vary an outer diameter of the outlet section between a minimum diameter and a maximum diameter.

Abstract: Method for using an air intake of a turbojet engine nacelle comprising at least one elastically deformable portion, at least one connecting member mounted in an annular cavity integrally with the elastically deformable portion, and at least one controllable displacement member, in which method: during a thrust phase of the turbojet engine, the controllable displacement member moves the connecting member into a first position in which the elastically deformable portion of the air intake lip has an aerodynamic profile, and during a thrust reversal phase of the turbojet engine the controllable displacement member moves the connecting member into a second position in which the elastically deformable portion of the air intake lip has an irregular profile so as to allow a release of the reverse air flow from the elastically deformable portion.

Abstract: A personal watercraft with cargo-carrying surface and an anchor rail mounted on a surface of the personal watercraft. The anchor rail being adjacent to the cargo-carrying surface and exposed to an environment. The anchor rail can include an outwardly facing surface exposed to the environment, and the anchor rail is secured to the personal watercraft in such a manner that the outwardly facing surface is recessed relative to the cargo-carrying surface to form a recess or that the outwardly facing surface is flush with the cargo-carrying surface.

Abstract: A propulsion system for an aircraft includes a rotor and a nacelle fairing that extends around the rotor in relation to an axis. The nacelle fairing includes an upstream portion forming an inlet section of the nacelle fairing as well as a downstream portion, a downstream end of which forms an outlet section of the nacelle fairing. The downstream portion includes radially inner and outer walls, both of which are made of a deformable shape memory material. The wall has independently actuatable piston actuator mechanisms, each actuator mechanism being actuatable independently of the others and being designed to cooperate with means built into an inner surface of the wall to deform the wall in a radial direction in relation to the axis under the effect of a predetermined displacement command.

Abstract: A personal watercraft with cargo-carrying surface and an anchor rail mounted on a surface of the personal watercraft. The anchor rail being adjacent to the cargo-carrying surface and exposed to an environment. The anchor rail can include an outwardly facing surface exposed to the environment, and the anchor rail is secured to the personal watercraft in such a manner that the outwardly facing surface is recessed relative to the cargo-carrying surface to form a recess or that the outwardly facing surface is flush with the cargo-carrying surface.

Abstract: A deck extender for a personal watercraft can include a deck member supported in a cantilevered configuration over an edge of the deck of the personal watercraft. The deck extender can include mounting sleeves fixed to an upper deck of a personal watercraft with mounting tabs of the deck member received within the mounting sleeves. The deck member can include mounting mechanisms having a receptacle and a pivoting cleat mounted above the receptacle configured for mounting accessories to the deck member. The deck member can have recessed channel members for mounting accessories.

Abstract: A propulsion system for an aircraft, comprising at least one rotor and a nacelle fairing extending around the at least one rotor with respect to an axis of rotation of the rotor, the nacelle fairing comprising: an upstream section forming an inlet section of the nacelle fairing; a downstream section, a downstream end of which forms an outlet section of the nacelle fairing; and an intermediate section connecting the upstream and downstream sections, wherein the downstream section comprises a radially inner wall and a radially outer wall made of a deformable shape memory material, and wherein the downstream end forming the outlet section has a pneumatic or hydraulic annular actuator extending around the axis of rotation and configured to deform radially under a predetermined control pressure so as to vary an outer diameter of the outlet section between a minimum diameter and a maximum diameter.

Abstract: Internal structure for a turbomachine nacelle, the internal structure being intended to surround at least one part of a compartment capable of receiving a gas generator of the turbomachine, the internal structure comprising a ventilation cavity of said compartment, the ventilation cavity being provided with a main ventilation outlet and an auxiliary ventilation outlet separate to the main ventilation outlet, the internal structure comprising a shut-off member movable relative to the ventilation cavity between a flow position and a shut-off position in which the shut-off member shuts off the auxiliary ventilation outlet to a greater extent than in the flow position.

Abstract: A noninvasive method of sensing an arterial pulse on a paw pad includes providing an instrument having a probe; placing the probe housing a tactile transducer and a reflective optical coupler comprising an infrared emitter and an infrared detector on a subject's metatarsal or metacarpal pad; emitting infrared light from the emitter; detecting infrared light with the detector; maintaining a linear direct current bias of the detector; converting a signal emitted by the infrared detector into a digital pulse that drives the tactile transducer to emit tactile pulses; and counting the tactile pulses over a predetermined time. An arterial pulse detection system includes a probe. The probe contains an optical sensor and a tactile transducer to which instrumentation is electrically connected. The optical sensor includes an infrared emitter and an infrared detector.

Abstract: A customer in a computing resource service provider environment provisions a virtual machine instance configured with access to sensitive data in a secure storage facility. The virtual machine instance is provisioned specifically to generate reports using a subset of the sensitive data to satisfy different reporting requirements associated with governing entities and agencies. After generating the reports, the virtual machine instance is then removed from the computing resource service environment such that the sensitive data is inaccessible.

Abstract: Method for using an air intake of a turbojet engine nacelle comprising at least one elastically deformable portion, at least one connecting member mounted in an annular cavity integrally with the elastically deformable portion, and at least one controllable displacement member, in which method: during a thrust phase of the turbojet engine, the controllable displacement member moves the connecting member into a first position in which the elastically deformable portion of the air intake lip has an aerodynamic profile, and during a thrust reversal phase of the turbojet engine the controllable displacement member moves the connecting member into a second position in which the elastically deformable portion of the air intake lip has an irregular profile so as to allow a release of the reverse air flow from the elastically deformable portion.

Abstract: A plurality of virtual machines instances are instantiated and configured to use a subset of sensitive data to generate reports such that the reports can be visually inspected by authorized personnel or entities for potential abnormalities. After completion of the inspection, the virtual machine instances are then deleted such that the sensitive data that were used to generate the reports become inaccessible.

Abstract: Disclosed are sulfonamide compounds with GPR17 modulating properties, which are useful for treating or preventing a variety of CNS and other diseases, in particular for preventing and treating myelinating diseases or disorders.

Abstract: A noninvasive method of sensing an arterial pulse on a paw pad includes providing an instrument having a probe; placing the probe housing a tactile transducer and a reflective optical coupler comprising an infrared emitter and an infrared detector on a subject's metatarsal or metacarpal pad; emitting infrared light from the emitter; detecting infrared light with the detector; maintaining a linear direct current bias of the detector; converting a signal emitted by the infrared detector into a digital pulse that drives the tactile transducer to emit tactile pulses; and counting the tactile pulses over a predetermined time. An arterial pulse detection system includes a probe. The probe contains an optical sensor and a tactile transducer to which instrumentation is electrically connected. The optical sensor includes an infrared emitter and an infrared detector.

Abstract: Disclosed are sulfonamide compounds with GPR17 modulating properties, which are useful for treating or preventing a variety of CNS and other diseases, in particular for preventing and treating myelinating diseases or disorders.

Abstract: A propulsion system for an aircraft, including at least one rotor and a nacelle cowling extending around the at least one rotor, said nacelle cowling being sectored and including at least one sector. which is fixed and sectors which are retractable in the peripheral direction relative to an axis of rotation of the rotor. The retractable sectors include at least a first series of sectors which are telescopically retractable in or on at least one fixed sector and at least a second series of sectors which are telescopically retractable in or on at least one fixed sector, the at least one fixed sector having an angular extent around the axis which is less than or equal to 90°.

Abstract: Disclosed are sulfonamide compounds with GPR17 modulating properties, which are useful for treating or preventing a variety of CNS and other diseases, in particular for preventing and treating myelinating diseases or disorders.

Abstract: A deck extender for a personal watercraft can include a deck member supported in a cantilevered configuration over an edge of the deck of the personal watercraft. The deck extender can include mounting sleeves fixed to an upper deck of a personal watercraft with mounting tabs of the deck member received within the mounting sleeves. The deck member can include mounting mechanisms having a receptacle and a pivoting cleat mounted above the receptacle configured for mounting accessories to the deck member. The deck member can have recessed channel members for mounting accessories.

Abstract: According to some aspects, a system for identifying a printed object is provided. The system may include an imaging device configured to image a three-dimensional (3D) printed object and a processor coupled to the imaging device. The processor may be configured to receive information generated as a result of imaging the 3D printed object with the imaging device, identify a set of features for the 3D printed object using the received information, compare the set of features with multiple reference sets of features, each of the multiple reference sets of features being associated with a respective 3D object in a plurality of 3D objects, and identify, based at least in part on results of the comparison, a 3D object from the plurality of 3D objects that matches the 3D printed object.

Abstract: A plyometric exercise ladder. A frame has two, spaced-apart, upright posts. A fixed arm is mounted to each upright post, each fixed arm being adjustable along the length of the frame. A removable pull-up bar is supported by the fixed arms. Two spring-loaded arms disposed above the fixed arms are pivotally mounted to the upright posts of the frame. An electromagnet is connected to each spring-loaded arm for initiating movement. A freestanding bracket having at least one scissor arm is connected to the frame and to a wall or other solid structure to support the ladder. In place of the spring-loaded arms and electromagnet, a set of pegs can be removably placed along the length of the upright posts for retaining the pull-up bar as an athlete progresses upwardly. The ladder frame itself can be replaced with a skeletal frame when the ladder is used in conjunction with a conventional squat rack.