公开(公告)号：JPH10183378A

公开(公告)日：1998-07-14

申请号：JP32584397

申请日：1997-11-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZAJCHOWSKI PAUL H ,  FRELING MELVIN ,  MEIER SUSAN M ,  ROY R DONOVAN

IPC: F16J15/16 ,  C22C29/06 ,  C22C32/00 ,  C23C4/06 ,  C23C30/00 ,  F01D11/12 ,  F16J15/32

Abstract: PROBLEM TO BE SOLVED: To provide a thick coating which can be used for a brush seal, has a long life and is free from crack. SOLUTION: This coating for a brush seal, in which a brush bristle is formed with a super alloy, has a nickel - chromium matrix which has a standard particle size of abut 44-15μm and contains a hard carbide phase of about 40-60vol% essentially made of a chromium carbide, and the nickel - chromium matrix contains, by nominal composition, about 80% Cr and about 20% Ni. The chromium carbide phase preferably and further contains either one of a titanium carbide, a tungsten carbide, a vanadium carbide and an optional mixture thereof.

公开(公告)号：JPH11229109A

公开(公告)日：1999-08-24

申请号：JP34088998

申请日：1998-12-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRELING MELVIN ,  LAGUEUX KEN R ,  ZAJCHOWSKI PAUL H

IPC: F01D5/28 ,  C23C4/02 ,  C23C4/06 ,  C23C4/10 ,  F02C7/28

Abstract: PROBLEM TO BE SOLVED: To improve the compsn. of grindable coating to be subjected to a substrate in a gas turbine engine. SOLUTION: The grindable coating is formed by plasma-spraying a top coat on a bond coat medium. The grindable coating contains 11 to 14 wt.% yttria, and the balance substantial zirconia. By this compsn., the corrosion resistance of the coating can be improved, and further, its thermal conductivity is made low, and by using this coating, the efficiency of the engine and its ductility can be improved.

公开(公告)号：JPH11229108A

公开(公告)日：1999-08-24

申请号：JP33642198

申请日：1998-11-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZAJCHOWSKI PAUL H ,  DIAZ ALFONSO ,  FRELING MELVIN ,  LALLY JOHN F

IPC: F01D5/28 ,  C23C4/02 ,  C23C4/06 ,  C23C4/12 ,  F02C7/28

Abstract: PROBLEM TO BE SOLVED: To improve a method for applying sprayed coating on a substrate in a gas turbine engine. SOLUTION: The method for applying sprayed coating on a substrate contains the arrangement of a rotor blade 10 in a fixture 12 rotatable with a shaft as the center, the formation of a spray contg. coating medium particles softened in a device 14 for spraying a coating medium onto the tip part of the blade 10 and the passing the blade 10 through the spray. By changing the details as for various treatment including treating parameters, the sprayed coating can controllably be applied.

公开(公告)号：JPH11229810A

公开(公告)日：1999-08-24

申请号：JP33516798

申请日：1998-11-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRELING MELVIN ,  GUPTA DINESH K ,  LAGUEUX KEN ,  DEMASI-MARCIN JEANINE T

IPC: F01D5/20 ,  F01D11/00 ,  F01D11/12 ,  F02C7/28 ,  F16J15/16

Abstract: PROBLEM TO BE SOLVED: To achieve an abrasive end portion for a seal mechanism of a gas turbine engine that receives a high degree of wear which is more durable, and the production of which is less expensive. SOLUTION: An abrasive end portion 28 includes a zirconium oxide wear coating 44 which is harder than a abraded seal surface such that it is able to grind the abraded seal surface, and which directly covers the top which has substantially no macrogrit. The coating 44 has a pillar-like structure and contains a stabilizer of approximately 3 wt.% to approximately 25 wt.%. The stabilizer may be selected from yttrium oxide, magnesium oxide, calcium oxide, or a mixture of these materials.

公开(公告)号：WO2009002680A2

公开(公告)日：2008-12-31

申请号：PCT/US2008066027

申请日：2008-06-06

Applicant: UNITED TECHNOLOGIES CORP ,  FRELING MELVIN ,  SCHLICHTING KEVIN W

Inventor： FRELING MELVIN ,  SCHLICHTING KEVIN W

IPC: C22C19/00 ,  C23C28/00

CPC classification number: C23C4/02 ,  B22F2998/00 ,  C22C19/03 ,  C22C19/058 ,  C22C30/00 ,  C23C28/021 ,  C23C28/023 ,  C23C28/028 ,  C23C30/00 ,  F05B2230/311 ,  F05C2201/0418 ,  Y02T50/67 ,  Y10T428/12493 ,  Y10T428/12611 ,  Y10T428/1275 ,  Y10T428/12854 ,  Y10T428/12931 ,  B22F3/115

Abstract: A protective coating system includes a coating having a composition that includes about 5-40 wt% of chromium, of about 5-35 wt% of aluminum, about 0.1-9 wt% of at least one of silicon, hafnium, or magnesium, about 0.05-2 wt% of a Group IIIB Periodic Table element, a non-zero amount less than 13 wt% of at least one noble metal selected from platinum, palladium, and gold, and a balance including nickel, cobalt or iron.

Abstract translation: 保护性涂层系统包括具有组合物的涂层，该组合物包括约5-40wt％的铬，约5-35wt％的铝，约0.1-9wt％的硅，铪或镁中的至少一种，约为 0.05-2重量％的IIIB族周期表元素，非零量小于13重量％的至少一种选自铂，钯和金的贵金属，余量包括镍，钴或铁。

公开(公告)号：WO2015142411A3

公开(公告)日：2015-12-17

申请号：PCT/US2015010750

申请日：2015-01-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRELING MELVIN ,  SERRA JESSICA L ,  ZAJCHOWSKI PAUL H ,  OSTROUT CRAIG L ,  HAZEL BRIAN T ,  BOCHIECHIO MARIO P

IPC: F23R3/42 ,  F23M5/00 ,  F23R3/46

CPC classification number: F23R3/007 ,  C23C4/073 ,  C23C4/129 ,  F23M5/00 ,  F23M2900/05004 ,  F23R3/002 ,  F23R2900/00018

Abstract: An article such as a heat shield panel includes a substrate and a multi-layered coating supported on the substrate. The multi-layered coating can include alternating layers of different ceramic material compositions having individual thicknesses of less than 25 micrometers.

Abstract translation: 诸如遮光板的物品包括基底和支撑在基底上的多层涂层。 多层涂层可以包括具有小于25微米的单独厚度的不同陶瓷材料组合物的交替层。

公开(公告)号：SG134210A1

公开(公告)日：2007-08-29

申请号：SG2006085989

申请日：2006-12-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRELING MELVIN ,  SCHLICHTING KEVIN W ,  MALONEY MICHAEL J ,  LITTON DAVID A ,  SMEGGIL JOHN G ,  SNOW DAVID B

Abstract: A turbine engine component is provided which has a substrate and a thermal barrier coating applied over the substrate. The thermal barrier coating comprises alternating layers of yttria- stabilized zirconia and a molten silicate resistant material. The molten silicate resistant outer layer may be formed from at least one oxide of a material selected from the group consisting of lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, scandium, indium, zirconium, hafnium, and titanium or may be formed from a gadolinia-stabilized zirconia. If desired, a metallic bond coat may be present between the substrate and the thermal barrier coating system. A method for forming the thermal barrier coating system of the present invention is described.

公开(公告)号：DE69822108T2

公开(公告)日：2005-02-03

申请号：DE69822108

申请日：1998-12-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZAJCHOWSKI PAUL H ,  DIAZ ALFONSO ,  FRELING MELVIN ,  LALLY JOHN F

IPC: F01D5/28 ,  C23C4/02 ,  C23C4/06 ,  C23C4/12 ,  F02C7/28

Abstract: A process for controllably applying thermal spray coating onto substrates is described. The process includes positioning rotor blades (10) in a fixture (12) rotatable about an axis, forming a spray of particles of softened coating medium in an apparatus for propelling the coating medium towards the blade tips and coating the blade tips by passing the blades through the spray of particles of coating medium. Various process details, including process parameters, are developed.

公开(公告)号：DE69822108D1

公开(公告)日：2004-04-08

申请号：DE69822108

申请日：1998-12-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ZAJCHOWSKI PAUL H ,  DIAZ ALFONSO ,  FRELING MELVIN ,  LALLY JOHN F

IPC: F01D5/28 ,  C23C4/02 ,  C23C4/06 ,  C23C4/12 ,  F02C7/28

Abstract: A process for controllably applying thermal spray coating onto substrates is described. The process includes positioning rotor blades (10) in a fixture (12) rotatable about an axis, forming a spray of particles of softened coating medium in an apparatus for propelling the coating medium towards the blade tips and coating the blade tips by passing the blades through the spray of particles of coating medium. Various process details, including process parameters, are developed.

公开(公告)号：CA2252658C

公开(公告)日：2002-08-13

申请号：CA2252658

申请日：1998-11-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRELING MELVIN ,  GUPTA DINESH K ,  DEMASI-MARCIN JEANINE T ,  LAGUEUX KEN

IPC: F01D5/20 ,  F01D11/00 ,  F01D11/12 ,  F02C7/28 ,  F16J15/16 ,  F01D5/28 ,  F01D11/08 ,  F01D11/14 ,  C09K3/14 ,  C04B35/48

Abstract: A gas turbine engine seal system includes a rotating member having an abrasive tip disposed in rub relationship to a stationary, abradable seal su rface. The abrasive tip comprises a zirconium oxide abrasive coat having a columnar str ucture that is harder than the abradable seal surface such that the abrasive tip ca n cut the abradable seal surface.