Abstract: A kit of parts for forming a foreline for coupling a process chamber to a vacuum pumping and/or abatement system, the kit comprising: a plurality of foreline segments; wherein each foreline segment is a pipe that comprises: a first substantially straight end portion; a second substantially straight end portion opposite to the first end portion; and an intermediate portion disposed between the first and second end portions and connected to the first and second end portions by respective bends; the first and second end portions are substantially parallel to each other; the intermediate portion is oblique to the first and second end portions; and the foreline segments are configured to be attached together so as to form a continuous foreline.

Abstract: A system comprising a pumping system configured to pump respective exhaust gases from each of a plurality of chemical etching process chambers and to combine the exhaust gases to provide a combined exhaust gas, and a noble gas recovery system configured to process the combined exhaust gas to remove one or more noble gases therefrom.

Abstract: Vehicle control using map-based braking includes receiving, while a driver is operating the vehicle to traverse a vehicle transportation network, vehicle operation information including at least a current speed of the vehicle, retrieving, from a planned path of an in-vehicle navigation system, an upcoming turn in a current road when the driver is using the in-vehicle navigation system, and retrieving from map data, the upcoming turn in the current road when the driver is not using tin-vehicle navigation system. Thereafter, it is determined whether, during the upcoming turn, wheels of the vehicle will maintain contact with a road surface at the current speed. A braking instruction is issued to a control system of the vehicle responsive to whether the wheels of the vehicle will maintain contact with the road surface at the current speed.

Abstract: Road feel is created in a vehicle that has a steer-by-wire system using image data obtained from one or more cameras on the vehicle and image data obtained from a light detection and ranging (LIDAR) sensor. A generative adversarial network (GAN) machine learning (ML) model is used to determine a road surface based on the image data from the one or more cameras and the image data from the LIDAR sensor. Haptic vibrations are generated based on the determined road surface to create the road feel using one or more motors on various vehicle components.

Abstract: A system comprising: a semiconductor processing tool (102) comprising a process chamber (108); a valve module (104) configured to receive a fluid from the process chamber (108) and to selectably direct a flow of said fluid; and a cooling apparatus (402) configured to supply a flow of a cooling fluid to the process chamber (108); wherein the valve module (104) and the cooling apparatus (402) are arranged in a stacked configuration.

Abstract: A method of delivering data to a vehicle including transmitting a request for the data from a vehicle to a database. The data stored in the database is tagged with location information. A location of the vehicle is determined. The data in the database tagged with location information within a predetermined distance of the determined location of the vehicle is determined. The data is delivered to the vehicle based on the determined location of the vehicle. The delivered data is displayed on a display disposed in the vehicle.

Abstract: A system may detect a sound associated with a vehicle. The sound may be detected using a set of one or more microphones. The system may use a machine learning model to detect at least one of a squeak or a rattle based on the sound. The machine learning model may be trained using a plurality of sounds emitted in relation to one or more vehicles. The system may determine, based on detecting at least one of the squeak or the rattle, a location of the vehicle associated with at least one of the squeak or the rattle. In some implementations, the location may be determined based on detecting different sound levels between a first microphone and a second microphone, or detecting a time difference between the first and the second microphone, or by correlating the sound to a sound signature associated with a part of the vehicle.

Abstract: Illustrative embodiments disclose systems for sharing, among a group of consumers, data provided by a contributor. Some embodiments are well-suited for real-time distribution of data developing from ongoing incidents, and may be useful, for example, for emergency management. Illustrative embodiments provide a cloud-based system having tenants that are data contributors and data consumers. The system receives, from each contributor, both data and sharing rules that dictate whether and how that data may be shared, and with whom (which consumer or consumers), and then provide data to such consumer or consumers according to the sharing rules.

Abstract: A vacuum exhaust system includes a plurality of turbo pumps that evacuate a plurality of vacuum chambers. A plurality of chamber valves are positioned between the turbo pumps and the plurality of vacuum chambers. A plurality of branch channels are each connected to a corresponding exhaust of the plurality of turbo pumps and a main channel is formed from a confluence of the branch channels. A booster vacuum pump is connected to the main channel. A backing vacuum pump is connected to an exhaust of the booster vacuum pump. A plurality of bypass channels, each having a valve, provide a fluid communication path between at least some of the plurality of vacuum chambers and the booster vacuum pump.

Abstract: A deployable antenna system for deployment in an extraterrestrial environment is provided, the deployable antenna system comprising a deployment mechanism including one or more extendable support structures comprising at least one axial support structure adapted to extend in a z-direction parallel to a z-axis in the deployable antenna system and a deployable antenna attached to the one or more extendable support structures and adapted to be stowed in an undeployed state and to be unfurled into a deployed state by the deployment mechanism, the deployable antenna being further adapted to extend and unfurl during deployment from the deployment mechanism in the z-direction responsive to extension of the at least one axial support structure, the deployable antenna including one or more flexible membranes coupled to the at least one axial support structure and extending from the z-axis in the deployed state.

Abstract: A vacuum pumping system which comprises a plurality of vacuum pumping arrangements for evacuating a flammable gas stream and exhausting the gas stream through an exhaust outlet. A housing houses the vacuum pumping arrangements and forms an air flow duct for an air flow for mixing with the exhaust gas stream output from the exhaust outlet in a mixing region in the housing. An airflow generator generates an air flow through the air flow duct to cause mixing of air with the flammable gas stream to a percentage of the flammable gas in the air flow lower than the lower flammability limit of the flammable gas. An airflow sensor senses the flow of air for determining if the air flow is sufficient to dilute the flammable gas to lower than said percentage.

Abstract: A lifting devices can include a tube with a first slot and a second slot. The devices also include an insert with a first insert projection connected to a second insert projection by a central portion. The first insert projection extends through the first slot and the second insert projection extends through the second slot. A first plate and a second plate are each connected to the central portion of the insert. The lifting devices can be used in a method of lifting a tanker truck or other structures.

Abstract: A kit of parts for forming a foreline for coupling a process chamber to a vacuum pumping and/or abatement system, the kit comprising: a plurality of foreline segments; wherein each foreline segment is a pipe that comprises: a first substantially straight end portion; a second substantially straight end portion opposite to the first end portion; and an intermediate portion disposed between the first and second end portions and connected to the first and second end portions by respective bends; the first and second end portions are substantially parallel to each other; the intermediate portion is oblique to the first and second end portions; and the foreline segments are configured to be attached together so as to form a continuous foreline.

Abstract: A deployable antenna system for deployment in an extraterrestrial environment is provided, the deployable antenna system comprising a deployment mechanism including one or more extendable support structures comprising at least one axial support structure adapted to extend in a z-direction parallel to a z-axis in the deployable antenna system and a deployable antenna attached to the one or more extendable support structures and adapted to be stowed in an undeployed state and to be unfurled into a deployed state by the deployment mechanism, the deployable antenna being further adapted to extend and unfurl during deployment from the deployment mechanism in the z-direction responsive to extension of the at least one axial support structure, the deployable antenna including one or more flexible membranes coupled to the at least one axial support structure and extending from the z-axis in the deployed state.

Abstract: A deployable structure for use in establishing a reflectarray antenna is provided that includes a flexible reflectarray and a deployment structure that includes an endless pantograph for deploying the flexible reflectarray from a folded, undeployed state towards a deployed state in which the flexible reflectarray is substantially planar. In a particular embodiment, the deployment structure includes a plurality of tapes that engage the endless pantograph and are used to establish a positional relationship between the deployed reflectarray and another component of the reflectarray antenna.

Abstract: A vacuum pumping and/or abatement system for evacuating and/or abating fluid from an entity, the system comprising: a first module comprising a vacuum pumping apparatus for pumping the fluid from the entity and/or an abatement apparatus for abating the fluid evacuated from the entity; and a second module arranged adjacent to the first module in a first system dimension; wherein the first and second modules each have a maximum size in the first system dimension that is a respective integer multiple of a common fixed system value.

Abstract: A deployable antenna system for deployment in an extraterrestrial environment is provided, the deployable antenna system comprising a deployment mechanism including one or more extendable support structures comprising at least one axial support structure adapted to extend in a z-direction parallel to a z-axis in the deployable antenna system and a deployable antenna attached to the one or more extendable support structures and adapted to be stowed in an undeployed state and to be unfurled into a deployed state by the deployment mechanism, the deployable antenna being further adapted to extend and unfurl during deployment from the deployment mechanism in the z-direction responsive to extension of the at least one axial support structure, the deployable antenna including one or more flexible membranes coupled to the at least one axial support structure and extending from the z-axis in the deployed state.

Abstract: A vacuum pump and vacuum assembly. The vacuum pump comprises: an inlet for receiving gas; and an exhaust for exhausting the gas; a hollow shaft defining an axial passage extending through the pump from an opening in a base of the pump to an opening axially beyond the pump inlet. The shaft comprises an end remote from the base of the pump, the end being configured to attach to a cathode plate within a vacuum chamber evacuated by the vacuum pump. The shaft is configured for axial movement of the end between at least one open position in which the end is remote from the inlet of the vacuum pump and a sealing position in which the end is closer to the inlet.

Abstract: A vacuum pump, vacuum pump arrangement and method are disclosed. The vacuum pump includes at least one rotor; and a stator, an inlet for receiving gas during operation; and an exhaust for exhausting the gas. The vacuum pump includes a shaft extending through a centre of said pump and comprising a plate mounted on an end of the shaft towards the inlet. The vacuum pump includes control circuitry configured to control an axial position of the plate, a change in axial position of the plate providing a change in inlet conductance of gas to the vacuum pump. The plate is mounted such that it extends beyond the inlet in at least some axial positions of the rotor such that the plate is not on the same side of the inlet as the stator.

Abstract: Process for forming a multi-layer electrochromic structure, the process comprising depositing a film of a liquid mixture onto a surface of a substrate, and treating the deposited film to form an anodic electrochromic layer, the liquid mixture comprising a continuous phase and a dispersed phase, the dispersed phase comprising metal oxide particles, metal alkoxide particles, metal alkoxide oligomers, gels or particles, or a combination thereof having a number average size of at least 5 nm.