公开(公告)号：US20090148614A1

公开(公告)日：2009-06-11

申请号：US12343852

申请日：2008-12-24

Applicant: Matthew B. BUCZEK ,  Andrew J. SKOOG ,  Mark RECHTSTEINER ,  Jane Ann MURPHY

Inventor： Matthew B. BUCZEK ,  Andrew J. SKOOG ,  Mark RECHTSTEINER ,  Jane Ann MURPHY

IPC: B05D1/06

CPC classification number: C23C24/00 ,  B05B5/032 ,  B05B5/1683 ,  B05B14/48 ,  C23C4/12 ,  C23C4/18 ,  Y02T50/67

Abstract: Electrostatic deposition of high performance powdered materials onto gas turbine surfaces. The process also includes post-deposition thermal staging of the deposited powder to provide a durable coating that will satisfy the demands of turbine engine operation. The process envisions application of organic-based powdered materials, glass/ceramic powdered materials and metal-based powdered materials and combinations thereof using electrostatic techniques to components exposed to low temperature operations, such as may be found in the front section of a gas turbine engine or to the exterior portions of an aircraft engine, and metal-containing glass ceramics, glass-ceramic materials, or materials that can be transformed into glass ceramic materials, when applied to components exposed to high temperature operations, such as may be found in the turbine and exhaust sections of a gas turbine engine or the flaps of an aircraft.

Abstract translation: 将高性能粉末材料静电沉积到燃气轮机表面上。 该方法还包括沉积粉末的沉积后分级，以提供将满足涡轮发动机运行需求的耐用涂层。 该方法设想使用静电技术将有机基粉末材料，玻璃/陶瓷粉末材料和金属基粉末材料及其组合应用于暴露于低温操作的部件，例如可以在燃气涡轮发动机的前部 或飞机发动机的外部部分，以及金属玻璃陶瓷，玻璃陶瓷材料或可转化成玻璃陶瓷材料的材料，当应用于暴露于高温操作的部件时，例如可以在 燃气涡轮发动机的涡轮机和排气段或飞行器的翼片。

公开(公告)号：US20080118719A1

公开(公告)日：2008-05-22

申请号：US11698546

申请日：2007-01-25

Applicant: Andrew Jay Skoog ,  Matthew Buczek ,  Mark Rechtsteiner

Inventor： Andrew Jay Skoog ,  Matthew Buczek ,  Mark Rechtsteiner

IPC: B32B5/00

CPC classification number: C23D5/04 ,  C23C24/08 ,  C23C24/082 ,  Y10T428/12611 ,  Y10T428/24893

Abstract: In accordance with one embodiment of the invention, there is provided a method of coating a gas turbine engine component using a powder coating process. The method comprises providing a gas turbine engine component; and applying a powder coating to the gas turbine engine component using the powder coating process. The powder coating is applied in a dry form without an organic solvent. The method further comprises heating the applied powder coating to melt and fuse particles of the powder coating to the gas turbine engine component and cure the powder coating.

Abstract translation: 根据本发明的一个实施例，提供了一种使用粉末涂覆工艺涂覆燃气涡轮发动机部件的方法。 该方法包括提供燃气轮机发动机部件; 以及使用所述粉末涂覆法将粉末涂料施加到所述燃气涡轮发动机部件。 粉末涂料以干燥形式施用而无有机溶剂。 该方法还包括加热所施加的粉末涂层以熔化并将粉末涂料的颗粒熔合到燃气涡轮发动机部件并固化粉末涂层。

公开(公告)号：US20050202270A1

公开(公告)日：2005-09-15

申请号：US10798134

申请日：2004-03-10

Applicant: Andrew Skoog ,  Matthew Buczek ,  Mark Rechtsteiner

Inventor： Andrew Skoog ,  Matthew Buczek ,  Mark Rechtsteiner

IPC: C23C4/12 ,  B05D1/04

CPC classification number: C23D5/04 ,  C23C24/08 ,  C23C24/082 ,  Y10T428/12611 ,  Y10T428/24893

Abstract: In accordance with one embodiment of the invention, there is provided a method of coating a gas turbine engine component using a powder coating process. The method comprises providing a gas turbine engine component; and applying a powder coating to the gas turbine engine component using the powder coating process. The powder coating is applied in a dry form without an organic solvent. The method further comprises heating the applied powder coating to melt and fuse particles of the powder coating to the gas turbine engine component and cure the powder coating.

Abstract translation: 根据本发明的一个实施例，提供了一种使用粉末涂覆工艺涂覆燃气涡轮发动机部件的方法。 该方法包括提供燃气轮机发动机部件; 以及使用所述粉末涂覆法将粉末涂料施加到所述燃气涡轮发动机部件。 粉末涂料以干燥形式施用而无有机溶剂。 该方法还包括加热所施加的粉末涂层以熔化并将粉末涂料的颗粒熔合到燃气涡轮发动机部件并固化粉末涂层。

公开(公告)号：US08420180B2

公开(公告)日：2013-04-16

申请号：US12343852

申请日：2008-12-24

Applicant: Matthew B. Buczek ,  Andrew J. Skoog ,  Mark Rechtsteiner ,  Jane Ann Murphy

Inventor： Matthew B. Buczek ,  Andrew J. Skoog ,  Mark Rechtsteiner ,  Jane Ann Murphy

IPC: B05D1/06

CPC classification number: C23C24/00 ,  B05B5/032 ,  B05B5/1683 ,  B05B14/48 ,  C23C4/12 ,  C23C4/18 ,  Y02T50/67

Abstract: Electrostatic deposition of high performance powdered materials onto gas turbine surfaces. The process also includes post-deposition thermal staging of the deposited powder to provide a durable coating that will satisfy the demands of turbine engine operation. The process envisions application of organic-based powdered materials, glass/ceramic powdered materials and metal-based powdered materials and combinations thereof using electrostatic techniques to components exposed to low temperature operations, such as may be found in the front section of a gas turbine engine or to the exterior portions of an aircraft engine, and metal-containing glass ceramics, glass-ceramic materials, or materials that can be transformed into glass ceramic materials, when applied to components exposed to high temperature operations, such as may be found in the turbine and exhaust sections of a gas turbine engine or the flaps of an aircraft.

Abstract translation: 将高性能粉末材料静电沉积到燃气轮机表面上。 该方法还包括沉积粉末的沉积后分级，以提供将满足涡轮发动机运行需求的耐用涂层。 该方法设想使用静电技术将有机基粉末材料，玻璃/陶瓷粉末材料和金属基粉末材料及其组合应用于暴露于低温操作的部件，例如可以在燃气涡轮发动机的前部 或飞机发动机的外部部分，以及金属玻璃陶瓷，玻璃陶瓷材料或可转化成玻璃陶瓷材料的材料，当应用于暴露于高温操作的部件时，例如可以在 燃气涡轮发动机的涡轮机和排气段或飞行器的翼片。

公开(公告)号：US20070104886A1

公开(公告)日：2007-05-10

申请号：US11272167

申请日：2005-11-10

Applicant: Matthew Buczek ,  Andrew Skoog ,  Mark Rechtsteiner ,  Jane Murphy

Inventor： Matthew Buczek ,  Andrew Skoog ,  Mark Rechtsteiner ,  Jane Murphy

IPC: H05C1/00 ,  B05D1/04

CPC classification number: C23C24/00 ,  B05B5/032 ,  B05B5/1683 ,  B05B14/48 ,  C23C4/12 ,  C23C4/18 ,  Y02T50/67 ,  Y02T50/6765

Abstract: Electrostatic deposition of high performance powdered materials onto gas turbine surfaces. The process also includes post-deposition thermal staging of the deposited powder to provide a durable coating that will satisfy the demands of turbine engine operation. The process envisions application of organic-based powdered materials, glass/ceramic powdered materials and metal-based powdered materials and combinations thereof using electrostatic techniques to components exposed to low temperature operations, such as may be found in the front section of a gas turbine engine or to the exterior portions of an aircraft engine, and metal-containing glass ceramics, glass-ceramic materials, or materials that can be transformed into glass ceramic materials, when applied to components exposed to high temperature operations, such as may be found in the turbine and exhaust sections of a gas turbine engine or the flaps of an aircraft.

Abstract translation: 将高性能粉末材料静电沉积到燃气轮机表面上。 该方法还包括沉积粉末的沉积后分级，以提供将满足涡轮发动机运行需求的耐用涂层。 该方法设想使用静电技术将有机基粉末材料，玻璃/陶瓷粉末材料和金属基粉末材料及其组合应用于暴露于低温操作的部件，例如可以在燃气涡轮发动机的前部 或飞机发动机的外部部分，以及金属玻璃陶瓷，玻璃陶瓷材料或可转化成玻璃陶瓷材料的材料，当应用于暴露于高温操作的部件时，例如可以在 燃气涡轮发动机的涡轮机和排气段或飞行器的翼片。