Abstract: The problem of addressing vibrational disturbances in mechanical positioning systems is addressed by systems and methods that use a combination of active vibration dampening and passive vibration dampening. A system described herein generally comprises a mechanical positioning system; a payload; and a vibration dampening module coupled to the mechanical position system and to the payload. The vibration dampening module generally comprises an active vibration dampener and/or a passive vibration dampener.

Abstract: The problem of addressing vibrational disturbances in mechanical positioning systems is addressed by systems and methods that use a combination of active vibration dampening and passive vibration dampening. A system described herein generally comprises a mechanical positioning system; a payload; and a vibration dampening module coupled to the mechanical position system and to the payload. The vibration dampening module generally comprises an active vibration dampener and/or a passive vibration dampener.

Abstract: A machine (10) for positioning an object (12) includes a movable part (16C) and a vibration reduction assembly (24) that couples the object (12) to the movable part (16C). Further, the vibration reduction assembly (24) reduces a magnitude of a vibration being transferred from the movable part (16C) to the object (12). The vibration reduction assembly (24) can include an actively controlled support system (30) and an actively controlled actuator system (32).

Abstract: 3D metrology techniques are disclosed for determining a changing topography of a substrate processed in an additive manufacturing system. Techniques include fringe scanning, simultaneous fringe projections, interferometry, and x-ray imaging. The techniques can be applied to 3D printing systems to enable rapid topographical measurements of a 3D printer powder bed, or other rapidly moving, nearly continuous surface to be tested. The techniques act in parallel to the system being measured to provide information about system operation and the topography of the product being processed. A tool is provided for achieving higher precision, increasing throughput, and reducing the cost of operation through early detection and diagnosis of operating problems and printing defects. These techniques work well with any powder bed 3D printing system, providing real-time metrology of the powder bed, the most recently printed layer, or both without reducing throughput.

Abstract: To improve the operation of 3D printing systems, techniques are disclosed for a rotary 3D printer comprising: a main rotating support table rotating about a first axis and one or more secondary support tables rotating around a non-coaxial secondary axis; a powder supply assembly for distributing powder onto the tables; and an energy system for directing an energy beam at the powder to form a part. The main support table and secondary support tables can rotate in the same or opposite directions. Disclosed techniques include: grooved support table surfaces for improving stability of applied powder; reciprocating bellows for controlling a differential load on actuators that move the support tables; high temperature bearings or bushings for supporting rotary motion at high temperatures; and a mechanism for counterbalancing a weight of the part being built.

Abstract: Apparatus include a reaction mass and an actuator coupled to the reaction mass. The actuator is configured to couple to a payload and to move the reaction mass in response to a movement error of the payload to reduce the movement error of the payload. Robotic systems using actuated reaction masses, as well as related methods of reducing movement errors, are also disclosed.

Abstract: The problem of addressing vibrational disturbances in mechanical positioning systems is addressed by systems and methods that use a combination of active vibration dampening and passive vibration dampening. A system described herein generally comprises a mechanical positioning system; a payload; and a vibration dampening module coupled to the mechanical position system and to the payload. The vibration dampening module generally comprises an active vibration dampener and/or a passive vibration dampener.

Abstract: Positioning assemblies for use with a robot include a gimbal assembly having a gimbal's rotational center is positioned directly above a center of gravity of a payload. One or more linear counter masses and/or one or more rotating masses (flywheels) can be provided, and each can include an actuator or brake to control forces acting between the counter masses and/or flywheels and the payload and stabilize the payload during and after movement of the payload with the robot.

Abstract: A vibration reduction assembly (24) for reducing a magnitude of a vibration being transferred from a first component (14) (e.g. a robot assembly) to a second component (12) (e.g. a payload) includes a first vibration reduction system (30) and a second vibration reduction system (32). The first vibration reduction system (30) reducing vibration along a first axis that is oriented parallel with gravity. The second vibration reduction system (32) reducing vibration along a second axis that is orthogonal to the first axis. The first vibration reduction system (30) and the second vibration reduction system (32) are connected in series between the first component (14) and the second component (12).

Abstract: A processing machine (10) for building a part (11) includes: a support device (26) including a support surface (26B); a drive device (28) which moves the support device (26) so as a specific position on the support surface (26B) is moved along a moving direction (25); a powder supply device (18) which supplies a powder (12) to the moving support device (26) to form a powder layer (13); an irradiation device (22) which irradiates at least a portion of the powder layer (13) with an energy beam (22D) to form at least a portion of the part (11) from the powder layer (13) during a first period of time; and a measurement device (20) which measures at least portion of the part (11) during a second period of time. The first period in which the irradiation device (22) irradiates the powder layer (13) with the energy beam (22D) and the second period in which the measurement device (22) measures are overlapped.

Abstract: A stage apparatus includes at least one tube having a first section and a second section, the first section being coupled to a point of reference. The apparatus also includes at least one magnet, a precision stage, and a tube carrier. The precision stage is positioned at least partially over the at least one magnet, and has a first set of coils. The first set of coils cooperates with the at least one magnet to drive the precision stage. The tube carrier is at least partially positioned over the at least one magnet, and includes an end effector portion arranged to carry the second section, wherein the tube carrier further includes a second set of coils, the second set of coils being supported by the end effector portion and arranged to cooperate with the at least one magnet to control motion of the end effector portion.