A method and system of depositing a coating on a substrate and/or simulating depositing a coating on a substrate.

A heating device for heating the surface of a substrate. The heating device comprises a gas source comprising an inert material supply inert under the operating conditions of the heating device, the gas source being adapted for supplying a hot jet of a gas comprising at least elements of said inert material on the substrate. The gas source is adapted for heating the hot jet of the gas to a temperature above 1500° C.

An apparatus may comprise a plasma deposition unit, a movement system, and a mesh system. The plasma deposition unit may be configured to generate a plasma. The movement system may be configured to move a substrate under the plasma deposition unit. The mesh system may be located between the plasma deposition unit and the substrate in which a mesh may comprise a number of materials for deposition onto the substrate and in which the plasma passing through the mesh may cause a portion of the number of materials from the mesh to be deposited onto the substrate.

The process for producing an orthopedic implant having an integrated ceramic surface layer includes steps for positioning the orthopedic implant inside a vacuum chamber, emitting a relatively high energy beam into the at least two different vaporized metalloid or transition metal atoms in the vacuum chamber to cause a collision therein to form ceramic molecules, and driving the ceramic molecules with the ion beam into an outer surface of the orthopedic implant at a relatively high energy such that the ceramic molecules implant therein and form at least a part of the molecular structure of the outer surface of the orthopedic implant, thereby forming the integrated ceramic surface layer.

A gas flow system is provided, including a gas flow source, one or more gas inlets, one or more gas outlets, a gas flow region, a low pressure region, wherein the low pressure region is fluidly coupled to the one or more gas outlets, a high pressure region, and a gap. The one or more gas inlets are fluidly coupleable to the gas flow source. The gas flow region is fluidly coupled to the one or more gas inlets and the one or more gas outlets. The gap fluidly couples the gas flow region to the high pressure region. The high pressure region near the targets allows for process gas interactions with the target to sputter onto the substrate below. The low pressure region near the substrate prevents unwanted chemical interactions between the process gas and the substrate.

OVJP depositors and techniques for using the same are provided, in which the in-substrate plane velocity of the delivery and confinement flows are both nonzero and parallel to each other across the boundary between the two. These configurations provide improved material utilization efficiency and relaxed fly height tolerances, while achieving acceptable printing resolution and feature uniformity.

A deposition apparatus (20) comprising: a chamber (22); a process gas source (62) coupled to the chamber; a vacuum pump (52) coupled to the chamber; at least two electron guns (26); one or more power supplies (30) coupled to the electron guns; a plurality of crucibles (32,33,34) positioned or positionable in an operative position within a field of view of at least one said electron gun; and a part holder (170) having at least one operative position for holding parts spaced above the crucibles by a standoff height H. The standoff height H is adjustable in a range including at least 22 inches.

Systems and methods for depositing materials on a substrate via OVJP are provided. A float table and grippers are used to move and position the substrate relative to one or more OVJP print bars to reduce the chance of damaging or compromising the substrate or prior depositions.

A device (1) for coating a substrate (4) with nanometric sized particles, wherein the device comprises: a plurality of aerodynamic lenses able to product a jet (3) of nanometric sized particles, each of the aerodynamic lenses having a longitudinal axis, the aerodynamic lenses being arranged so that the various longitudinal axes are parallel and oriented in a first direction (X) defining the direction of propagation of the jet and in the form of at least two columns (9, 10) offset from each other in a second direction (Y) orthogonal to the first direction, where the first and the second column each comprise at least one of the aerodynamic lenses, the at least one of the aerodynamic lenses of the first column also being offset relative to the at least one of the aerodynamic lenses of the second column in a third direction (Z) that is both orthogonal to the first direction and to the second direction.

The present disclosure provides a holding arrangement. The holding arrangement for holding a substrate includes: a body portion having a first side; a dry adhesive material provided on the first side of the body portion; a seal surrounding the dry adhesive material and configured to provide a vacuum region on the first side, wherein the dry adhesive material is provided in the vacuum region; and a conduit to evacuate the vacuum region.