Abstract: An aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation. The aircraft has a blended wing body and includes an engine, a binary lift fan system, a forced air bypass system and an exhaust system. The engine has a turboshaft mode and a turbofan mode. The lift fan system includes a plurality of ducted fans in a tandem lateral orientation. In the VTOL orientation of the aircraft, the engine is in the turboshaft mode coupled to the lift fan system such that the engine provides rotational energy to the ducted fans generating the thrust-borne lift. In the forward flight orientation of the aircraft, the engine is in the turbofan mode coupled to the forced air bypass system such that the bypass air combines with the engine exhaust in the exhaust system to provide forward thrust generating the wing-borne lift.

Abstract: A propulsion system for an aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation. The propulsion system includes an turboshaft engine, a lift fan system, a forced air bypass system and an exhaust system. The engine has a turboshaft mode and a turbofan mode. The lift fan system includes at least one ducted fan. In the VTOL orientation of the aircraft, the engine is in the turboshaft mode coupled to the lift fan system such that the engine provides rotational energy to the at least one ducted fan generating the thrust-borne lift. In the forward flight orientation of the aircraft, the engine is in the turbofan mode coupled to the forced air bypass system such that the bypass air combines with the engine exhaust in the exhaust system to provide forward thrust generating the wing-borne lift.

Abstract: A power input terminal block includes terminals received in terminal channels of a housing each having a main body defining a wire pocket receiving a supply wire and a take-off tab electrically connected to the main body. The power input terminal block includes clamp contacts coupled to the take-off tabs each having a base, a spring beam extending from the base, and a cap extending from the spring beam having a poke-in window configured to receive a take-off wire. An edge defining the poke-in window engages the take-off wire and pulls the take-off wire against the wire side of the take-off tab. The power input terminal block includes release levers coupled to the housing to move the spring beam to an extended position to allow loading and removal of the take-off wire from the clamp contact and the take-off tab.

Abstract: An aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a forward flight orientation. The aircraft has a blended wing body and includes an engine, a unitary lift fan system, a forced air bypass system and an exhaust system. The engine has a turboshaft mode and a turbofan mode. The lift fan system includes a ducted fan. In the VTOL orientation of the aircraft, the engine is in the turboshaft mode coupled to the lift fan system such that the engine provides rotational energy to the ducted fan generating the thrust-borne lift. In the forward flight orientation of the aircraft, the engine is in the turbofan mode coupled to the forced air bypass system such that the bypass air combines with the engine exhaust in the exhaust system to provide forward thrust generating the wing-borne lift.

Abstract: An infrared thermal desorber includes a desorption housing; an infrared source receiver that receives an infrared emission source; an infrared absorber receiver that receives an infrared absorber, such that the infrared absorber receiver produces thermal energy emission; an analyte target receiver that receives an analyte target, such that the analyte target receiver is in infrared communication with the infrared absorber disposed in the infrared source receiver so that the analyte target receives the thermal energy emission from the infrared absorber, desorbs the adsorbed analyte as volatilized analyte from the analyte target in response to receipt of the thermal energy emission from the infrared absorber, and communicates the volatilized analyte from the analyte target; and an effluent communicator that receives the volatized analyte.

Abstract: A computer-implemented method for propagating access to assets across a plurality of datasources. The method may include receiving user input via an administrative user interface that comprises selection of the datasources. A plurality of provisionable assets including at least one provisionable asset from each of the datasources may be automatically retrieved. Asset designations of at least some of the provisionable assets may be received via the administrative user interface. A plurality of asset paths corresponding to the designated assets may be automatically determined. The asset paths may be automatically assigned to an authorized role and automatically consolidated for collective invocation in response to queries.

Abstract: A data management and storage (DMS) cluster of peer DMS nodes manages resources of a multi-tenant environment. The DMS cluster provides an authorization framework that provides user access which is scoped to the resources within a tenant organization and the privileges of the user within the organization. To authorize an action on a resource by a user, the DMS cluster determines determine user authorizations associated with the user defining privileges of the user on the resources of the multi-tenant environment, and organization authorizations associated defining resources of the multi-tenant environment that belong to the organization. The DMS cluster authorizes the action when the user authorizations and organizations authorized indicate that the action on the resource is authorized.

Abstract: A suspension travel control system (1046) for a vehicle suspension is disclosed. The suspension travel control system includes a stop post (834) secured to the vehicle frame and a suspension travel control formation that includes a base (1042) and a body (1048). The stop post (834) is positioned in a space defined by the body (1048). The suspension travel control formation may be secured to the axle, the main support member or incorporated into the axle coupling assembly to provide a rebound and jounce stop as well as longitudinal redundancy in the event of the failure or loss of a longitudinal linkage.

Abstract: The present disclosure relates to methods for detecting and targeting genomic rearrangements, in particular gene fusion events, by targeting a DNA molecule of interest with a set or pool of primers, wherein the forward primers and reverse primers produce a PCR amplification product when a genomic rearrangement is present. The present disclosure also relates to methods of bioinformatic analysis to determine whether or not the detection of an amplification product from the selective PCR is actually indicative of the presence of a gene fusion. The present disclosure also related to related methods of diagnosis and treatment of diseases and conditions associated with such genomic rearrangements, in particular cancers, such as lung cancer.

Abstract: A direct interaction network in which resources are more efficiently transferred between entities having resource pools with the same organization. The interaction network may be implemented by transforming a user computer system into the interaction terminal for the interaction such that the provider entity does not require interaction terminals to enter into interactions. Alternatively, the interaction network may be entered through interaction terminals of the provider entity without the user having a user computer system and without the user providing a physical instrument for the interaction. These implementations may be possible due at least in part to being able to determine that the entity resource pools are administered by the same organization. Furthermore, one or more sensors may be utilized with the user computer system and/or interaction terminals in order to determine the presence or identity of a user, and/or the subject of the interaction.

Abstract: A direct interaction network in which resources are more efficiently transferred between entities having resource pools with the same organization. The interaction network may be implemented by transforming a user computer system into the interaction terminal for the interaction such that the provider entity does not require interaction terminals to enter into interactions. Alternatively, the interaction network may be entered through interaction terminals of the provider entity without the user having a user computer system and without the user providing a physical instrument for the interaction. These implementations may be possible due at least in part to being able to determine that the entity resource pools are administered by the same organization. Furthermore, one or more sensors may be utilized with the user computer system and/or interaction terminals in order to determine the presence or identity of a user, and/or the subject of the interaction.

Abstract: A modular tandem tiltrotor aircraft in which the tiltrotor assemblies are operably coupled at the forward and aft ends of the fuselage of the aircraft is disclosed. The modular tandem tiltrotor assemblies are capable of rotating between a vertical lift position and a horizontal flight position. The modular tandem tiltrotor aircraft can be structurally more efficient and lower drag than a conventional tiltrotor, has better control authority and lifting capacity than hybrid-quads and tail-sitters, and has more range than a helicopter or multi-rotor. The modular tandem tiltrotor aircraft can orbit and search over a broad area, or can hover for long periods, depending on the application. Instead of providing a multi-function tandem tiltrotor aircraft that is generally suited for all applications, but not optimized for any, the modular tandem tiltrotor aircraft allows for customized configuration to optimize the aircraft for a particular application.

Abstract: A lighting receptacle assembly includes a receptacle assembly housing having a base and a head with a cavity. The head has an upper surface defining a mating interface for mating with a sensor connector and a seal configured to be sealed against the fixture housing. An index mounting ring is coupled to the fixture housing from an interior of the fixture housing and includes indexing features interfacing with housing indexing features. A spring holder plate is coupled to the head and holds a spring biasing the receptacle assembly housing in a holding direction toward the index mounting ring to engage the housing indexing features and the indexing features.

Abstract: Various embodiments provide for alert generation based on alert dependency. For some embodiments, the alert dependency checking facilitates alert noise reduction. Various embodiments described herein dynamically find or discover alert dependencies based on one or more alerts currently active, one or more active alerts generated in the past, or some combination of both. Various embodiments described herein provide alert monitoring that adapts based on an alert state of a machine. Various embodiments described herein generate a health score for a machine based on an alert state of the machine. Various embodiments described herein provide a tool for managing definitions of one or more alerts that can be identified as an active alert for a machine.

Abstract: A method for an aircraft may include determining a transition from an airplane mode to a helicopter mode for a propulsion system of the aircraft, wherein the propulsion system comprises a plurality of rotor blades; determining whether a descent rate condition is satisfied, wherein the descent rate condition is associated with a maximum allowable descent rate for the aircraft; and controlling a collective pitch angle for the plurality of rotor blades based on the descent rate condition.