公开(公告)号：US20160159488A1

公开(公告)日：2016-06-09

申请号：US14903987

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James T. Roach ,  Colin J. Kling ,  Grant O. Cook ,  James J. McPhail ,  Shari L. Bugaj ,  James F. O'Brien ,  Majidullah Dehlavi ,  Scott A. Smith ,  Matthew R. Rader ,  Matthew A. Turner ,  JinQuan Xu

IPC: B64D29/00 ,  F01D25/28 ,  F01D5/02

CPC classification number: B64D29/00 ,  B29D22/00 ,  F01D5/02 ,  F01D25/28 ,  F02K3/04 ,  F05D2220/32 ,  F05D2230/30 ,  F05D2230/90 ,  F05D2300/10 ,  F05D2300/43 ,  F05D2300/603 ,  Y02T50/672

Abstract: Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.

Abstract translation: 公开了用于制造轻质电镀聚合物燃气涡轮发动机部件的电镀聚合物燃气涡轮发动机部件和方法。 这些部件包括镀有一个或多个金属层的聚合物基材。 聚合物基材的聚合材料可以用可以包括碳，金属或玻璃的材料在结构上加强。 聚合物基底还可以包括多个层以形成复合铺层结构。

公开(公告)号：US20140255202A1

公开(公告)日：2014-09-11

申请号：US13725359

申请日：2012-12-21

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Colin J. Kling ,  James J. McPhail ,  Matthew R. Rader

IPC: B64C11/14

CPC classification number: F02C7/05 ,  B64C11/14

Abstract: An assembly for a turbine engine including a nosecone that extends along an axis between a tip end and a second end. The nosecone includes a base region and a deformation region configured integral with the base region. The base region is arranged axially between the deformation region and the second end. The deformation region is adapted to deform relative to the base region upon impact of an object, and includes a stress concentrator.

Abstract translation: 一种用于涡轮发动机的组件，其包括沿尖端和第二端之间的轴线延伸的鼻锥体。 鼻锥包括基部区域和与基部区域一体形成的变形区域。 基部区域轴向地布置在变形区域和第二端部之间。 变形区域适于在物体撞击时相对于基底区域变形，并且包括应力集中器。

公开(公告)号：US11267576B2

公开(公告)日：2022-03-08

申请号：US14903987

申请日：2014-07-09

Applicant: United Technologies Corporation

Inventor： James T. Roach ,  Colin J. Kling ,  Grant O. Cook, III ,  James J. McPhail ,  Shari L. Bugaj ,  James F. O'Brien ,  Majidullah Dehlavi ,  Scott A. Smith ,  Matthew R. Rader ,  Matthew A. Turner ,  JinQuan Xu

IPC: B64D29/00 ,  B29D22/00 ,  F02K3/04 ,  F01D5/02 ,  F01D25/28

Abstract: Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.

公开(公告)号：US09353685B2

公开(公告)日：2016-05-31

申请号：US13725359

申请日：2012-12-21

Applicant: United Technologies Corporation

Inventor： Colin J. Kling ,  James J. McPhail ,  Matthew R. Rader

IPC: B64C11/14 ,  F02C7/05

CPC classification number: F02C7/05 ,  B64C11/14

Abstract: An assembly for a turbine engine including a nosecone that extends along an axis between a tip end and a second end. The nosecone includes a base region and a deformation region configured integral with the base region. The base region is arranged axially between the deformation region and the second end. The deformation region is adapted to deform relative to the base region upon impact of an object, and includes a stress concentrator.

Abstract translation: 一种用于涡轮发动机的组件，其包括沿尖端和第二端之间的轴线延伸的鼻锥体。 鼻锥包括基部区域和与基部区域一体形成的变形区域。 基部区域轴向地布置在变形区域和第二端部之间。 变形区域适于在物体撞击时相对于基底区域变形，并且包括应力集中器。