公开(公告)号：US20160084103A1

公开(公告)日：2016-03-24

申请号：US14495319

申请日：2014-09-24

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Michael Kahrs ,  Timothy Vander Hoek ,  Loris Bedrosyan ,  Jason Smoke ,  Ardeshir Riahi ,  Daniel C. Crites

IPC: F01D11/12 ,  F01D5/22 ,  B23P15/04

CPC classification number: B23P15/04 ,  B23K20/02 ,  B23K20/233 ,  B23K2101/001 ,  B23K2103/18 ,  B23K2103/26 ,  B23P15/006 ,  F01D5/3061 ,  F01D5/34 ,  F05D2230/232

Abstract: Methods are provided for manufacturing a shrouded bonded turbine rotor. A shrouded blade ring is formed. The shrouded blade ring is formed by bonding a unitary shroud ring to an assembled blade ring or assembling a plurality of shrouded turbine blade segments. The shrouded blade ring is bonded to a hub. The shrouded bonded turbine rotors are also provided. The shrouded bonded turbine rotor comprises a shrouded blade ring and a shroud. The shrouded blade ring comprises a plurality of turbine blade segments and a shroud. Each turbine blade segment comprises an airfoil portion including an airfoil having a root and a tip. The shroud covers the tip of each airfoil in the shrouded blade ring. A hub is bonded with the shrouded blade ring.

Abstract translation: 提供了用于制造被覆盖的粘结涡轮转子的方法。 形成有盖的叶片环。 被覆盖的叶片环通过将整体护罩环结合到组装的叶片环或组装多个带盖的涡轮叶片段而形成。 被覆盖的叶片环结合到轮毂。 还提供了带盖的粘合涡轮转子。 被覆盖的粘合涡轮转子包括被覆盖的叶片环和护罩。 被覆盖的叶片环包括多个涡轮叶片段和护罩。 每个涡轮机叶片段包括翼型部分，其包括具有根部和尖端的翼型件。 护罩覆盖被覆盖的叶片环中每个翼型的末端。 轮毂与被覆盖的叶片环结合。

公开(公告)号：US09027392B2

公开(公告)日：2015-05-12

申请号：US13888955

申请日：2013-05-07

Applicant: Honeywell International Inc.

Inventor： Timothy Vander Hoek

IPC: G01M15/14 ,  G01L13/00 ,  G01P5/14 ,  G01P13/02 ,  G01F1/42 ,  G01M9/06

CPC classification number: G01M15/14 ,  G01F1/34 ,  G01F1/42 ,  G01L13/00 ,  G01L15/00 ,  G01M9/06 ,  G01P5/14 ,  G01P13/025 ,  Y10T29/49826

Abstract: A multi-hole probe has a kernel that includes a forward surface that includes at least a first, second, and third pressure sensing ports. The multi-hole probe kernel further includes an upper surface, generally orthogonal to the forward surface, and including at least a first, second, and third stem ports. Still further, the multi-hole probe kernel includes first, second, and third tubes running between and providing a fluid connection with the first, second, and third pressure sensing ports and the first, second, and third stem ports, respectively.

Abstract translation: 多孔探针具有包括至少包括第一，第二和第三压力感测端口的前表面的内核。 多孔探针核还包括大致垂直于前表面的上表面，并且至少包括第一，第二和第三阀杆端口。 此外，多孔探针核包括分别在第一，第二和第三压力传感端口以及第一，第二和第三阀杆端口之间运行并提供流体连接的第一，第二和第三管。

公开(公告)号：US20140331750A1

公开(公告)日：2014-11-13

申请号：US13888955

申请日：2013-05-07

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Timothy Vander Hoek

IPC: G01M15/14

CPC classification number: G01M15/14 ,  G01F1/34 ,  G01F1/42 ,  G01L13/00 ,  G01L15/00 ,  G01M9/06 ,  G01P5/14 ,  G01P13/025 ,  Y10T29/49826

Abstract: A multi-hole probe has a kernel that includes a forward surface that includes at least a first, second, and third pressure sensing ports. The multi-hole probe kernel further includes an upper surface, generally orthogonal to the forward surface, and including at least a first, second, and third stem ports. Still further, the multi-hole probe kernel includes first, second, and third tubes running between and providing a fluid connection with the first, second, and third pressure sensing ports and the first, second, and third stem ports, respectively.

Abstract translation: 多孔探针具有包括至少包括第一，第二和第三压力感测端口的前表面的内核。 多孔探针核还包括大致垂直于前表面的上表面，并且至少包括第一，第二和第三阀杆端口。 此外，多孔探针核包括分别在第一，第二和第三压力传感端口以及第一，第二和第三阀杆端口之间运行并提供流体连接的第一，第二和第三管。