公开(公告)号：US20160160673A1

公开(公告)日：2016-06-09

申请号：US14732905

申请日：2015-06-08

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Dmitri Novikov ,  David Ulrich Furrer ,  Sergei F Burlatsky

IPC: F01D11/12 ,  F01D5/12 ,  F01D5/02 ,  F01D11/00 ,  F01D25/18

CPC classification number: F01D11/122 ,  F01D11/003 ,  F05D2240/307 ,  F05D2240/55 ,  F05D2300/226 ,  F05D2300/228 ,  F05D2300/50 ,  F05D2300/509 ,  Y02T50/672

Abstract: A stiffness controlled abradable seal system for a gas turbine engine includes a cantilevered arm that supports one of a rotating seal surface and a static seal surface, a stiffness of the cantilevered arm controlled to achieve a desired operational temperature at a seal interface, and an optimally matched abradeable seal material with required thermo-physical and friction properties to enable desired wear mechanisms and maximized sealing and durability.

Abstract translation: 用于燃气涡轮发动机的刚性控制的可磨损密封系统包括支撑旋转密封表面和静态密封表面中的一个的悬臂，控制悬臂的刚度以在密封界面处实现期望的操作温度，并且最佳地 匹配的可磨损密封材料具有所需的热物理和摩擦性能，以实现所需的磨损机制，并实现最大的密封和耐用性。

公开(公告)号：US20160115278A1

公开(公告)日：2016-04-28

申请号：US14921177

申请日：2015-10-23

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Dmitri Novikov ,  David Ulrich Furrer ,  Sergei F. Burlatsky ,  Hillary Anne Huttenhower ,  Vadim Atrazhev ,  Vadim Sultanov ,  Dmitry Dmitriev ,  John D. Riehl ,  Charles R. Watson

IPC: C08G73/10 ,  C08K5/00 ,  C08K3/00

CPC classification number: C08G73/1085 ,  C08J3/18 ,  C08J3/24 ,  C08J3/28 ,  C08J2379/08 ,  C08K3/01 ,  C08K3/013 ,  C08K5/0016 ,  C08L79/08

Abstract: A polymeric material process includes increasing a mobility within a polymer to enables specific alignment of polymer chains.

Abstract translation: 聚合物材料方法包括增加聚合物内的迁移率，以实现聚合物链的特异性排列。

公开(公告)号：US20160040284A1

公开(公告)日：2016-02-11

申请号：US14810767

申请日：2015-07-28

Applicant: United Technologies Corporation

Inventor： Dmitri Novikov ,  Sergei F. Burlatsky ,  David Ulrich Fuller ,  David A. Litton

IPC: C23C14/54 ,  F01D25/00 ,  C23C14/24

CPC classification number: C23C14/54 ,  C23C14/228 ,  C23C14/243 ,  F01D25/005

Abstract: A method or control strategy in a coating apparatus for use in a coating process can include controlling differential gas pressures among multiple selected localized zones in a coating chamber with respect to each other. The controlled differential gas pressure of the multiple selected localized zones is used to influence how a coating deposits on at least one component. The localized zones can be selected from a first localized zone around the component, a second localized zone adjacent the source of coating material, a third localized zone that diverges from the second localized zone toward the first localized zone, and a fourth localized zone that circumscribes at least the third localized zone

Abstract translation: 在涂覆工艺中使用的涂覆装置中的方法或控制策略可以包括控制涂覆室中相对于彼此的多个选定局部区域中的差分气体压力。 多个选定的局部区域的受控差压气体压力用于影响涂层如何沉积在至少一个部件上。 局部区域可以从组件周围的第一局部区域，与涂层材料源相邻的第二局部区域，从第二局部区域向第一局部区域分叉的第三局部区域以及第四局部区域选择， 至少第三个本地化区域

公开(公告)号：US20160024955A1

公开(公告)日：2016-01-28

申请号：US14775927

申请日：2013-12-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Shahram Amini ,  Christopher W Strock ,  Sergei F Burlatsky ,  Dmitri Novikov ,  David Ulrich Fuller

IPC: F01D11/12 ,  F01D9/04 ,  B23K1/00 ,  B23K1/19 ,  C23C24/04 ,  B23K20/22 ,  B23K26/34 ,  B23K26/00 ,  C23C4/12 ,  F01D5/28 ,  B23K20/02

CPC classification number: F01D11/122 ,  B23K1/0006 ,  B23K1/19 ,  B23K20/02 ,  B23K20/22 ,  B23K26/0006 ,  B23K26/34 ,  B23K2103/16 ,  C23C4/04 ,  C23C4/134 ,  C23C24/04 ,  F01D5/288 ,  F01D9/041 ,  F01D11/12 ,  F01D11/20 ,  F05D2220/30 ,  F05D2230/236 ,  F05D2230/237 ,  F05D2230/312 ,  F05D2230/60 ,  F05D2230/90 ,  F05D2240/125 ,  F05D2240/307 ,  F05D2300/6032

Abstract: A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix.

Abstract translation: 涡轮发动机系统包括具有翼型部分和尖端的涡轮发动机部件，该涡轮发动机部件具有结合到尖端的MAXMET复合材料。 MAXMET复合材料在金属基体中具有MAX相。

公开(公告)号：US20150354397A1

公开(公告)日：2015-12-10

申请号：US14731743

申请日：2015-06-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Dmitri Novikov ,  David Ulrich Furrer ,  Sergei F. Burlatsky

IPC: F01D11/12 ,  C10M109/00

CPC classification number: F01D11/001 ,  C04B35/5607 ,  C04B35/5611 ,  C04B35/5618 ,  C04B35/5622 ,  C04B35/58 ,  C04B35/58007 ,  C04B35/58014 ,  C04B35/58021 ,  C04B35/58028 ,  C04B2235/5212 ,  C10M109/00 ,  F01D11/122 ,  F05D2240/55 ,  F05D2300/226 ,  F05D2300/228 ,  F05D2300/509 ,  Y02T50/672

Abstract: A stiffness controlled abradeable seal system for a gas turbine engine includes a cantilevered arm that supports one of a rotating seal surface and a static seal surface, a stiffness of the cantilevered arm controlled to achieve a desired operational temperature at a seal interface.

Abstract translation: 用于燃气涡轮发动机的刚性控制的可磨蚀密封系统包括支撑旋转密封表面和静态密封表面中的一个的悬臂，所述悬臂的刚度被控制以在密封界面处实现期望的操作温度。