108245results about How to "Reduce pollution" patented technology

A method, computer readable medium, and system for vapor deposition on a substrate that maintain a first assembly of the vapor deposition system at a first temperature, maintain a second assembly of the vapor deposition system at a reduced temperature lower than the first temperature, dispose the substrate in a process space of the first assembly that is vacuum isolated from a transfer space in the second assembly, and deposit a material on the substrate. As such, the system includes a first assembly having a process space configured to facilitate material deposition, a second assembly coupled to the first assembly and having a transfer space to facilitate transfer of the substrate into and out of the deposition system, a substrate stage connected to the second assembly and configured to support the substrate, and a sealing assembly configured to separate the process space from the transfer space. The first assembly is configured to be maintained at a first temperature and the second assembly is configured to be maintained at a reduced temperature lower than the first temperature.

A method, computer readable medium, and system for treating a substrate in a process space of a processing system that is vacuum isolated from a transfer space of the processing system is described. A sealing device is disposed between a first chamber assembly configured to define the process space and a second chamber assembly configured to define the transfer space. When the sealing device is engaged, vacuum isolation is provided between the process space and the transfer space. The sealing device comprises two or more contact ridges with one or more pockets formed therebetween. When the sealing device is engaged between the first chamber assembly and the second chamber assembly, gas is trapped in the one or more pockets. This trapped gas assists the release of the sealing device upon disengagement of the sealing device between the first chamber assembly and the second chamber assembly.

A method and system for vapor deposition on a substrate that disposes a substrate in a process space of a processing system that is isolated from a transfer space of the processing system, processes the substrate at either of a first position or a second position in the process space while maintaining isolation from the transfer space, and deposits a material on said substrate at either the first position or the second position. Furthermore, the system includes a high conductance exhaust apparatus configured to be coupled to the process space, whereby particle contamination of the substrate processed in the deposition system is minimized. The exhaust apparatus comprises a pumping system located above the substrate and an evacuation duct, wherein the evacuation duct has an inlet located below the substrate plane.

A plasma enhanced atomic layer deposition (PEALD) system is described, wherein the system comprises a processing space and a high vacuum, ultra-clean transfer space. During processing, the substrate to which the thin conformal film is formed is exposed to the processing space. During substrate transfer, the substrate is exposed to the high vacuum space. Processing gases are introduced sequentially and alternately to the process chamber and the pressures and gas flows within, to and from, and between the process chamber and the high vacuum transfer space are controlled to keep the transfer space ultra-clean.

A method, computer readable medium, and system for vapor deposition on a substrate that introduce a gaseous film precursor to a process space, increase the volume of the process space from a first size to a second size to form an enlarged process space, introduce a reduction gas to the enlarged process space, and form a reduction plasma from the reduction gas. The system for vapor deposition includes a process chamber including a first process space and further including a second process space that includes the first process space and that has a second volume that exceeds the first volume. The first process space is configured for atomic layer deposition, and the second process space is configured for plasma reduction of a layer deposited in the first process space.

A method and system for plasma-assisted thin film vapor deposition on a substrate is described. The system includes a process chamber including a first process space having a first volume, a substrate stage coupled to the process chamber and configured to support a substrate and expose the substrate to the first process space, a plasma generation system coupled to the process chamber and configured to generate plasma in at least a portion of the first process space, and a vacuum pumping system coupled to the process chamber and configured to evacuate at least a portion of the first process space. The system further includes a process volume adjustment mechanism coupled to the process chamber and configured to create a second process space that includes at least a part of the first process space and that has a second volume less than the first volume, the substrate being exposed to the second process space.

A method and system for vapor deposition on a substrate that disposes a substrate in a process space of a processing system that is isolated from a transfer space of the processing system, processes the substrate at either of a first position or a second position in the process space while maintaining isolation from the transfer space, and deposits a material on said substrate at either the first position or the second position. Furthermore, the system includes a high conductance exhaust apparatus configured to be coupled to the process space, whereby particle contamination of the substrate processed in the deposition system is minimized. The exhaust apparatus comprises a pumping system located above the substrate and an evacuation duct, wherein the evacuation duct has an inlet located below the substrate plane.

A method, computer readable medium, and system for treating a substrate in a process space of a processing system that is vacuum isolated from a transfer space of the processing system is described. A sealing device is disposed between a first chamber assembly configured to define the process space and a second chamber assembly configured to define the transfer space. When the sealing device is engaged, vacuum isolation is provided between the process space and the transfer space. The sealing device comprises two or more contact ridges with one or more pockets formed therebetween. When the sealing device is engaged between the first chamber assembly and the second chamber assembly, gas is trapped in the one or more pockets. This trapped gas assists the release of the sealing device upon disengagement of the sealing device between the first chamber assembly and the second chamber assembly.

Embodiments of the present invention generally provide an apparatus and method for forming an improved thin film single or multi-junction solar cell in a substrate processing device. One embodiment provides a system that contains at least one processing chamber that is adapted to deposit one or more layers that form a portion of a solar cell device. In one embodiment, a method is employed to reduce the contamination of a substrate processed in the processing chamber by performing a cleaning process on the inner surfaces of the processing chamber prior to depositing the one or more layers on a substrate. The cleaning process may include depositing a layer, such as a seasoning layer or passivation layer, that tends to trap contaminants found in the processing chamber. Other embodiments of the invention may provide scheduling and / or positioning the cleaning processing steps at desirable times within a substrate processing sequence to improve the overall system substrate throughput.

A method, computer readable medium, and system for vapor deposition on a substrate that maintain a first assembly of the vapor deposition system at a first temperature, maintain a second assembly of the vapor deposition system at a reduced temperature lower than the first temperature, dispose the substrate in a process space of the first assembly that is vacuum isolated from a transfer space in the second assembly, and deposit a material on the substrate. As such, the system includes a first assembly having a process space configured to facilitate material deposition, a second assembly coupled to the first assembly and having a transfer space to facilitate transfer of the substrate into and out of the deposition system, a substrate stage connected to the second assembly and configured to support the substrate, and a sealing assembly configured to separate the process space from the transfer space. The first assembly is configured to be maintained at a first temperature and the second assembly is configured to be maintained at a reduced temperature lower than the first temperature.

A method, computer readable medium, and system for treating a substrate in a process space of a vacuum processing system is described. A vacuum pump in fluid communication with the vacuum processing system and configured to evacuate the process space, while a process material supply system is pneumatically coupled to the vacuum processing system and configured to supply a process gas to the process space. Additionally, the vacuum pump is pneumatically coupled to the process supply system and configured to, at times, evacuate the process gas supply system.

A method for vapor deposition on a substrate in a vapor deposition system having a process space separated from a transfer space. The method disposes a substrate in a process space of a processing system that is vacuum isolated from a transfer space of the processing system, processes the substrate at either of a first position or a second position in the process space while maintaining vacuum isolation from the transfer space by way of a movement accommodating sealing material, and deposits a material on the substrate at either the first position or the second position.

A powered nose aircraft wheel system (130) for an aircraft (12) includes landing gear (104) that extends from the aircraft (12). A wheel axel (136) is coupled to the landing gear (104). A wheel (134) is coupled to the wheel axel (136). A wheel motor (106) is coupled to the wheel axel (136) and the wheel (134). A controller (120) is coupled to the wheel motor (106) and rotates the wheel (134). A method of taxiing an aircraft (12) includes permitting the wheel (134) of the aircraft (12) to freely spin during the landing of the aircraft (12). Power is transferred from an auxiliary power unit (73) of the aircraft (12) to the wheel motor (106). The wheel (134) is rotated via the wheel motor (106). The aircraft (12) is steered and the speed of the wheel (134) is controlled via one or more controllers selected from an onboard controller (18, 118, 120) and an offboard controller (45, 58, 59).