公开(公告)号：US20220186372A1

公开(公告)日：2022-06-16

申请号：US17590614

申请日：2022-02-01

Applicant: Applied Materials, Inc.

Inventor： Kaushal Gangakhedkar ,  Jonathan Frankel ,  Colin C. Neikirk ,  Pravin K. Narwankar

IPC: C23C16/455 ,  A61K9/16 ,  C23C16/44

Abstract: A reactor for coating particles includes a vacuum chamber configured to hold particles to be coated, a vacuum port to exhaust gas from the vacuum chamber via the outlet of the vacuum chamber, a chemical delivery system configured to flow a process gas into the particles via a gas inlet on the vacuum chamber, one or more vibrational actuators located on a first mounting surface of the vacuum chamber, and a controller configured to cause the one or more vibrational actuators to generate a vibrational motion in the vacuum chamber sufficient to induce a vibrational motion in the particles held within the vacuum chamber.

公开(公告)号：US20220105048A1

公开(公告)日：2022-04-07

申请号：US17492363

申请日：2021-10-01

Applicant: Applied Materials, Inc.

Inventor： Fei Wang ,  Miaojun Wang ,  Colin C. Neikirk ,  Jonathan Frankel ,  Pravin K. Narwankar

IPC: A61K9/50

Abstract: A method of preparing a pharmaceutical composition having a drug-containing core enclosed by one or more silicon oxide materials is provided. The method entails alternating exposing the particles to gaseous or vaporous SiCl4 and gaseous or vaporous H2O at a reduced temperature and in the absence of a catalyst.

公开(公告)号：US20220064794A1

公开(公告)日：2022-03-03

申请号：US17522869

申请日：2021-11-09

Applicant: Applied Materials, Inc.

Inventor： Colin C. Neikirk ,  Pravin K. Narwankar ,  Kaushal Gangakhedkar ,  Visweswaren Sivaramakrishnan ,  Jonathan Frankel ,  David Masayuki Ishikawa ,  Quoc Truong ,  Joseph Yudovsky

IPC: C23C16/455 ,  C23C16/44 ,  C23C16/442

Abstract: A reactor for coating particles includes one or more motors, a rotary vacuum chamber configured to hold particles to be coated, wherein the rotary vacuum chamber is coupled to the motors, a controller configured to cause the motors to rotate the rotary vacuum chamber about an axial axis of the rotary vacuum chamber such that the particles undergo tumbling agitation, a vacuum port to exhaust gas from the rotary vacuum chamber, a paddle assembly including a rotatable drive shaft extending through the rotary vacuum chamber and coupled to the motors and at least one paddle extending radially from the drive shaft, such that rotation of the drive shaft by the motors orbits the paddle about the drive shaft in a second direction, and a chemical delivery system including a gas outlet on the paddle configured inject process gas into the particles.

公开(公告)号：US11015252B2

公开(公告)日：2021-05-25

申请号：US16283567

申请日：2019-02-22

Applicant: Applied Materials, Inc.

Inventor： David Britz ,  Pravin K. Narwankar ,  David Thompson ,  Yuriy Melnik ,  Sukti Chatterjee

IPC: F01D5/28 ,  F01D5/18 ,  C23C28/00 ,  C23C16/455 ,  C23C28/04 ,  C23C16/40 ,  C23C14/08

Abstract: Using the systems and methods discussed herein, CMAS corrosion is inhibited via CMAS interception in an engine environment and/or is prevented or reduced by the formation of a metal oxide protective coating on a hot engine section component. The CMAS interception can occur while the engine is in operation in flight or in a testing or quality control environment. The metal oxide protective coating can be applied over other coatings, including Gd-zirconates (GZO) or yttria-stabilized zirconia (YSZ). The metal oxide protective coating is applied at original equipment manufacturers (OEM) and can also be applied in-situ using a gas injection system during engine use in-flight or during maintenance or quality testing. The metal oxide protective coating contains a rare earth element, aluminum, zirconium, chromium, or combinations thereof, and is from 1 nm to 3 microns in thickness.

公开(公告)号：US20170365491A1

公开(公告)日：2017-12-21

申请号：US15689550

申请日：2017-08-29

Applicant: Applied Materials, Inc.

Inventor： Banqiu Wu ,  Nag B. Patibandla ,  Toshiaki Fujita ,  Ralf Hofmann ,  Pravin K. Narwankar ,  Jeonghoon Oh ,  Srinivas Satya ,  Li-Qun Xia

IPC: H01L21/673 ,  C23C16/54 ,  C23C16/458 ,  H01L21/677 ,  C23C16/455

CPC classification number: H01L21/673 ,  C23C16/45546 ,  C23C16/4558 ,  C23C16/4584 ,  C23C16/54 ,  H01L21/67346 ,  H01L21/677

Abstract: A processing chamber having a plurality of movable substrate carriers stacked therein for continuously processing a plurality of substrates is provided. The movable substrate carrier is capable of being transported from outside of the processing chamber, e.g., being transferred from a load luck chamber, into the processing chamber and out of the processing chamber, e.g., being transferred into another load luck chamber. Process gases delivered into the processing chamber are spatially separated into a plurality of processing slots, and/or temporally controlled. The processing chamber can be part of a multi-chamber substrate processing system.

公开(公告)号：US20240390286A1

公开(公告)日：2024-11-28

申请号：US18674730

申请日：2024-05-24

Applicant: Applied Materials, Inc.

Inventor： Miaojun Wang ,  Kai Zheng ,  Lance A. Scudder ,  Sukti Chatterjee ,  Fei Wang ,  Shrikant Swaminathan ,  Pravin K. Narwankar

IPC: A61K9/50

Abstract: This disclosure pertains to methods to prepare coated particles comprising a drug-containing core and a coating of inorganic oxides applied by vapor phase deposition (supercycles). The coated particles have a modified drug release profile comparing to the uncoated drug particles.

公开(公告)号：US20230347310A1

公开(公告)日：2023-11-02

申请号：US18212599

申请日：2023-06-21

Applicant: Applied Materials, Inc.

Inventor： Jonathan Frankel ,  Colin C. Neikirk ,  Pravin K. Narwankar ,  Quoc Truong ,  Govindraj Desai ,  Sekar Krishnasamy

IPC: B01J8/10 ,  C23C16/44 ,  B05D1/00 ,  B01F27/70 ,  B01F27/112

CPC classification number: B01J8/10 ,  C23C16/4417 ,  B05D1/60 ,  B01F27/70 ,  B01F27/112 ,  B01J2208/00867 ,  B01F2101/22

Abstract: A reactor for coating particles includes a stationary vacuum chamber to hold a bed of particles to be coated, a vacuum port in an upper portion of the chamber, a chemical delivery system configured to inject a reactant or precursor gas into a lower portion of the chamber, a paddle assembly, and a motor to rotate a drive shaft of the paddle assembly. The lower portion of the chamber forms a half-cylinder. The paddle assembly includes a rotatable drive shaft extending through the chamber along the axial axis of the half cylinder, and a plurality of paddles extending radially from the drive shaft such that rotation of the drive shaft by the motor orbits the plurality of paddles about the drive shaft.

公开(公告)号：US11753727B2

公开(公告)日：2023-09-12

申请号：US17313863

申请日：2021-05-06

Applicant: Applied Materials, Inc.

Inventor： David Britz ,  Pravin K. Narwankar ,  David Thompson ,  Yuriy Melnik ,  Sukti Chatterjee

IPC: C23C16/40 ,  C23C28/00 ,  F01D5/28 ,  F01D5/18 ,  C23C16/455 ,  C23C16/52 ,  C23C28/04 ,  C23C14/08

CPC classification number: C23C28/3455 ,  C23C16/45525 ,  C23C16/52 ,  C23C28/3215 ,  C23C28/345 ,  F01D5/186 ,  F01D5/288 ,  C23C14/083 ,  C23C16/40 ,  C23C28/042 ,  F05D2230/31 ,  F05D2240/24 ,  F05D2260/95 ,  F05D2300/121 ,  F05D2300/132 ,  F05D2300/134 ,  Y10T428/2462

Abstract: Using the systems and methods discussed herein, CMAS corrosion is inhibited via CMAS interception in an engine environment and/or is prevented or reduced by the formation of a metal oxide protective coating on a hot engine section component. The CMAS interception can occur while the engine is in operation in flight or in a testing or quality control environment. The metal oxide protective coating can be applied over other coatings, including Gd-zirconates (GZO) or yttria-stabilized zirconia (YSZ). The metal oxide protective coating is applied at original equipment manufacturers (OEM) and can also be applied in-situ using a gas injection system during engine use in-flight or during maintenance or quality testing. The metal oxide protective coating contains a rare earth element, aluminum, zirconium, chromium, or combinations thereof.

公开(公告)号：US11753726B2

公开(公告)日：2023-09-12

申请号：US17313858

申请日：2021-05-06

Applicant: Applied Materials, Inc.

Inventor： David Britz ,  Pravin K. Narwankar ,  David Thompson ,  Yuriy Melnik ,  Sukti Chatterjee

IPC: F01D5/28 ,  C23C28/00 ,  F01D5/18 ,  C23C16/455 ,  C23C16/52 ,  C23C28/04 ,  C23C16/40 ,  C23C14/08

CPC classification number: C23C28/3455 ,  C23C16/45525 ,  C23C16/52 ,  C23C28/3215 ,  C23C28/345 ,  F01D5/186 ,  F01D5/288 ,  C23C14/083 ,  C23C16/40 ,  C23C28/042 ,  F05D2230/31 ,  F05D2240/24 ,  F05D2260/95 ,  F05D2300/121 ,  F05D2300/132 ,  F05D2300/134 ,  Y10T428/2462

Abstract: Using the systems and methods discussed herein, CMAS corrosion is inhibited via CMAS interception in an engine environment and/or is prevented or reduced by the formation of a metal oxide protective coating on a hot engine section component. The CMAS interception can occur while the engine is in operation in flight or in a testing or quality control environment. The metal oxide protective coating can be applied over other coatings, including Gd-zirconates (GZO) or yttria-stabilized zirconia (YSZ). The metal oxide protective coating is applied at original equipment manufacturers (OEM) and can also be applied in-situ using a gas injection system during engine use in-flight or during maintenance or quality testing. The metal oxide protective coating contains a rare earth element, aluminum, zirconium, chromium, or combinations thereof.

公开(公告)号：US11732353B2

公开(公告)日：2023-08-22

申请号：US16850856

申请日：2020-04-16

Applicant: Applied Materials, Inc.

Inventor： Sukti Chatterjee ,  Lance A. Scudder ,  Yuriy Melnik ,  David A. Britz ,  Thomas Knisley ,  Kenichi Ohno ,  Pravin K. Narwankar

IPC: C23C16/40 ,  C23C16/455 ,  C23C28/02 ,  C23C16/56 ,  B64F5/40

CPC classification number: C23C16/403 ,  C23C16/405 ,  C23C16/45525 ,  C23C16/56 ,  C23C28/02 ,  B64F5/40

Abstract: Embodiments of the present disclosure generally relate to protective coatings on an aerospace component and methods for depositing the protective coatings. In one or more embodiments, a method for depositing a coating on an aerospace component includes depositing one or more layers on a surface of the aerospace component using an atomic layer deposition or chemical vapor deposition process, and performing a partial oxidation and annealing process to convert the one or more layers to a coalesced layer having a preferred phase crystalline assembly. During oxidation cycles, an aluminum depleted region is formed at the surface of the aerospace component, and an aluminum oxide region is formed between the aluminum depleted region and the coalesced layer. The coalesced layer forms a protective coating, which decreases the rate of aluminum depletion from the aerospace component and the rate of new aluminum oxide scale formation.