Abstract: A device for contactlessly determining the straightness of at least one long product, where punctiform or linear measuring radiation is moved by a radiation source module over the long product at least transversely to the longitudinal direction of the long product during a measuring cycle. The intensity of detection radiation coming from an area of incidence of the measuring radiation is recorded by a radiation detection module in a time-resolved manner and is supplied to a control and evaluation unit. The spatial position of the areas of incidence and thus the straightness of a long product can be determined from location information regarding the areas of incidence in the longitudinal direction and from characteristic intensity values of the detection radiation. For a calibration, a reference straightness can be determined by carrying out multiple measuring cycles by rotating a long product of unknown straightness.

Abstract: Spacecraft servicing devices or pods and related methods may include a body configured to be deployed from a host spacecraft at a location adjacent a target spacecraft and at least one spacecraft servicing component configured to perform at least one servicing operation on the target spacecraft.

Abstract: Spacecraft servicing systems include a spacecraft servicing device and at least one mission extension pod comprising at least one spacecraft servicing component. The spacecraft servicing device is configured to transfer the at least pod to a target spacecraft in order to service the target spacecraft with the at least one spacecraft servicing component of the at least one pod. Spacecraft servicing pods configured to be supplied to a spacecraft with a spacecraft servicing device include at least one spacecraft servicing component.

Abstract: A crane barrier access warning system suspended by four or more pinned adjustable telescoping supports, which extend outward from a cranes lower car body between the tracks. One of the telescoping members end inserts into a mounting frame, which comprises of other pinned adjustable telescoping components, so that it can be fitted to the frame or track beams. This entire safety barrier system is erected without tools. The components that form the actual safety barrier surrounds the whole crane and are suspended from it so that the safely barrier moves with the crane. Suspension components are adjustable through their pinned telescoping members so that the invention can fit different sized cranes. All the parts can be separated and fully retracted for shipping or storage.

Abstract: A device for contactlessly determining the straightness of at least one long product, where punctiform or linear measuring radiation is moved by a radiation source module over the long product at least transversely to the longitudinal direction of the long product during a measuring cycle. The intensity of detection radiation coming from an area of incidence of the measuring radiation is recorded by a radiation detection module in a time-resolved manner and is supplied to a control and evaluation unit. The spatial position of the areas of incidence and thus the straightness of a long product can be determined from location information regarding the areas of incidence in the longitudinal direction and from characteristic intensity values of the detection radiation. For a calibration, a reference straightness can be determined by carrying out multiple measuring cycles by rotating a long product of unknown straightness.

Abstract: System and methods are provided for identifying, searching, collecting, locking, executing deleting, comparing and/or analyzing data from a plurality of computer devices and environments from a centralized interface. The endpoint computer devices utilize an agent to index data contained on each device and that allows for a distributed action model using simple or advanced analytics by authenticated users. The agent can be embedded in an integrated circuit of the endpoint computing device or otherwise stored in permanent read only memory (i.e., firmware). The system allows for one or more users to conduct actions via device indexes utilizing a centralized computing device for comparison and analyzation purposes.

Abstract: Spacecraft servicing systems include a spacecraft servicing device and at least one pod comprising at least one spacecraft servicing component. The spacecraft servicing device is configured to transfer the at least one pod to a target spacecraft in order to service the target spacecraft with the at least one spacecraft servicing component of the at least one pod. Spacecraft servicing pods configured to be supplied to a spacecraft with a spacecraft servicing device include at least one spacecraft servicing component.

Abstract: System and methods are provided for identifying, searching, collecting, locking, executing deleting, comparing and/or analyzing data from a plurality of computer devices and environments from a centralized interface. The endpoint computer devices utilize an agent to index data contained on each device and that allows for a distributed action model using simple or advanced analytics by authenticated users. The agent can be embedded in an integrated circuit of the endpoint computing device or otherwise stored in permanent read only memory (i.e., firmware). The system allows for one or more users to conduct actions via device indexes utilizing a centralized computing device for comparison and analyzation purposes.

Abstract: Spacecraft servicing devices or pods and related methods may include a body configured to be deployed from a host spacecraft at a location adjacent a target spacecraft and at least one spacecraft servicing component configured to perform at least one servicing operation on the target spacecraft. The servicing device may include a communication device configured to receive data relating to the target spacecraft from a location remote from the spacecraft servicing device. The servicing device may include a coupling mechanism comprising at least one movable coupling configured to rotate the body relative to the target spacecraft when the spacecraft servicing pod is coupled to the target spacecraft. The at least one spacecraft servicing component may include at least one propulsion device positioned on a boom arm extending away from the body.

Abstract: Spacecraft servicing devices or pods and related methods may be configured to be deployed from a carrier spacecraft and include at least one spacecraft servicing component configured to perform at least one servicing operation on the target spacecraft. The spacecraft servicing devices may be configured to be transported from an initial orbit to another orbit after the spacecraft servicing device is deployed from the carrier spacecraft.

Abstract: A locking device is provided for a motor vehicle door. The locking device includes a body having a base, a stake, a lever, a gusset and a rotational axis. A method of locking a motor vehicle door closed in response to a side impact is also provided.

Abstract: Removable goggle lens system including a sequentially-stacked set of lenses each of the lenses having a front-face, a back-face, a thickness, and a finger-tab. Each of the lenses are defined by the front-face, the back-face, the front-face, and the back-face separated by the thickness; and the finger-tab formed as an extension of the thickness such that a wearer-user can remove each of the lenses sequentially as desired approaching a main lens of a host goggle as sequentially removed.

Abstract: A computer implemented method and apparatus for integrating e-commerce providers with third-party vendors. The method comprises receiving an order from one vendor of a plurality of vendors, wherein the order comprises a vendor identification, a fulfillment identification, and a vendor stock keeping unit (SKU), and wherein a plurality of the vendors each has a unique communication protocol; mapping the fulfillment identification to a user identification (userID) known to a provider; mapping the vendor SKU to a provider SKU; generating a provisioning call responsive to the mapping; and provisioning the SKU for the userID in a database of the provider in response to the provisioning call.

Abstract: Disclosed herein are compounds and methods for antagonizing GPRC6a for the treatment of proteinopathies.

Abstract: In one embodiment, a method includes providing, to a client system of a user, a user interface for display. The user interface may include a first set of options for selecting an artificial intelligence (AI) task for integrating into a user application, a second set of options for selecting one or more devices on which the user wants to deploy the selected AI task, and a third set of options for selecting one or more performance constraints specific to the selected devices. User specifications may be received based on user selections in the first, second, and third sets of options. A custom AI model may be generated based on the user specifications and sent to the client system of the user for integrating into the user application. The custom AI model once integrated may enable the user application to perform the selected AI task on the selected devices.

Abstract: Spacecraft servicing systems include a spacecraft servicing device and at least one pod comprising at least one spacecraft servicing component. The spacecraft servicing device is configured to transfer the at least one pod to a target spacecraft in order to service the target spacecraft with the at least one spacecraft servicing component of the at least one pod. Spacecraft servicing pods configured to be supplied to a spacecraft with a spacecraft servicing device include at least one spacecraft servicing component.

Abstract: Spacecraft servicing devices or pods and related methods may include a body configured to be deployed from a host spacecraft at a location adjacent a target spacecraft and at least one spacecraft servicing component configured to perform at least one servicing operation on the target spacecraft.

Abstract: A latch system for vehicle doors includes a powered latch including a powered actuator that is configured to unlatch the powered latch. An interior unlatch input feature such as an unlatch switch can be actuated by a user to provide an unlatch request. The system may include a controller that is operably connected to the powered actuator of the powered latch. The controller is configured such that it does not unlatch the powered latch if a vehicle speed is greater than a predefined value unless the interior latch feature is actuated at least two times according to predefined criteria.

Abstract: A latch system for vehicle doors includes a powered latch including a powered actuator that is configured to unlatch the powered latch. An interior unlatch input feature such as an unlatch switch can be actuated by a user to provide an unlatch request. The system may include a controller that is operably connected to the powered actuator of the powered latch. The controller is configured such that it does not unlatch the powered latch if a vehicle speed is greater than a predefined value unless the interior latch feature is actuated at least two times according to predefined criteria.

Abstract: Removable goggle lens system including a sequentially-stacked set of lenses each of the lenses having a front-face, a back-face, a thickness, and a finger-tab. Each of the lenses are defined by the front-face, the back-face, the front-face, and the back-face separated by the thickness; and the finger-tab formed as an extension of the thickness such that a wearer-user can remove each of the lenses sequentially as desired approaching a main lens of a host goggle as sequentially removed.