Abstract: A method for saving a file stored on a third-party system to a cloud storage system includes receiving, at a cloud storage server of the cloud storage system, a save request from the third party system. The method further includes authenticating the save request, based at least in part on information identifying a user, creating a copy of the file at the cloud storage server, and associating the copy of the file with the user.

Abstract: A thermal management system is provided for incorporation into a gas turbine engine, wherein the gas turbine engine, the aircraft, or both define a vertical direction. The thermal management system including: a thermal transport bus having a thermal fluid flowing therethrough; a plurality of heat source exchangers in thermal communication with the thermal fluid in the thermal transport bus; and a pump assembly in flow communication with the thermal transport bus, the pump assembly including: a pump; and a pump protection device positioned below the pump along the vertical direction.

Abstract: A method includes receiving distributed sensing information on one or more characteristics associated with a subject from distributed sensors distributed between a starting location spaced from a resolution location and the resolution location. If the subject is sensed by the plurality of distributed sensors, in combination without any break in chain of custody (“COC”), the method does not adjust a reliability of the distributed sensing information caused by any break in COC. If there are one or more time gaps in the COC, the method determines one or more COC factors based on the time gaps and adjusts the reliability of the distributed sensing information based on the one or more COC factors. The method determines a trust score of the subject to assess security concern of the subject based on the distributed sensing information and the reliability thereof, and resolves the security concern based on the trust score.

Abstract: A fan assembly for a gas turbine engine includes a fan disk, a trunnion, an actuation device, a fan blade, and a counterweight assembly. The trunnion is mounted to the fan disk. The actuation device is operably coupled to the trunnion. The fan blade is rotatably attached to the fan disk. The counterweight assembly includes a link arm, a lever arm, a hinge, and a counterweight. The link arm is connected to the trunnion, to the actuation device, or to both. The link arm is configured to drive rotation of the trunnion relative to the fan disk. The hinge is pivotably connected to the lever arm. The lever arm is connected to the link arm and is disposed to rotate about a connection point of the lever arm and the hinge. The counterweight is mounted to the lever arm at a location spaced from the hinge.

Abstract: Systems and methods involve a case, adapter, and portable electronic device, the system includes at least one base; at least two walls positioned on either side of the at least one base; at least one slot defined at least in part by the at least two walls and the at least one base; at least one post extending from the at least one base; and at least one interface including at least one electrically conductive contact extending from the at least one base. In addition, other aspects are described in the claims, drawings, and text forming a part of the present disclosure.

Abstract: The adjustable helmet assembly disclosed within in comprises a front shell, a back shell and a locking mechanism. The locking mechanism allows sliding movement of the front shell relative to the back shell for adjustment to a desired length for a specific wearer. The locking mechanism is movable from an unlocked position allowing the front shell to move relative to the back shell, and a locked position prohibiting the front shell to move relative to the back shell. The locking mechanism may be a clamp or lever function, and/or a cam function. Accordingly, the adjustable helmet may further comprise crumple zones to further reduce and/or dissipate impact forces.

Abstract: An orthopedic brace is provided that includes one or more pad plates formed of a light-curable material and a hinge comprising one or more hinge framework elements connected to the one or more pad plates. The pad plates may include an elastomeric shell to contain the light-curable material. A rigid attachment member may be coupled to the elastomeric shell to couple to the hinge framework element.

Abstract: Described herein are examples of evaluating electromagnetic energy reflection data of security scans. In embodiments, a method to evaluate electromagnetic energy reflection data determines whether electronic information of a security scan contains an anomaly, and identifies an anomaly location in the electronic information corresponding to the anomaly. The method determines a subset of the electronic information corresponding to the anomaly location, determines anomaly attributes using the subset of the electronic information, and evaluates the anomaly attributes using a database of reference items by comparing anomaly attributes to respective reference characteristics of reference items or identity information. When a comparison meets the respective match criterion for the given reference item, the method assigns to the anomaly the respective identifier as an anomaly identifier.

Abstract: Described herein are compounds that inhibit ALK2 and its mutants, pharmaceutical compositions including such compounds, and methods of using such compounds and compositions.

Abstract: Systems and methods involve a portable electronic computing device, the system includes a case section including two apertures with a channel extending therebetween, and cover assembly including two plug portions with a mid portion extending therebetween, the two apertures, channel, two plug portions and mid portion sized and oriented, respectively, for coupling of the cover assembly with case section. In addition, other aspects are described in the claims, drawings, and text forming a part of the present disclosure.

Abstract: A turbofan engine is provided. The turbofan engine includes a fan comprising a plurality of fan blades; a turbomachine operably coupled to the fan for driving the fan, the turbomachine comprising a compressor section, a combustion section, and a turbine section in serial flow order and together defining a core air flowpath; a nacelle surrounding and at least partially enclosing the fan; an inlet pre-swirl feature located upstream of the plurality of fan blades, the inlet pre-swirl feature attached to or integrated into the nacelle; and a means for reducing ice buildup or ice formation on the inlet pre-swirl feature, the means in communication with the inlet pre-swirl feature.