公开(公告)号：US09963989B2

公开(公告)日：2018-05-08

申请号：US14296657

申请日：2014-06-05

Applicant: United Technologies Corporation

Inventor： Anton G. Banks ,  Robert L. Hazzard

IPC: F01D11/00 ,  F01D25/24

CPC classification number: F01D11/005 ,  F01D25/246

Abstract: A vane seal assembly for a gas turbine engine comprises of a case including a first connector. A notch in the case adjoins the groove. A vane having a second connector mates with the first connector. A seal assembly is provided between the vane and the case to provide a sealed cavity adjoining the notch.

公开(公告)号：US20160047259A1

公开(公告)日：2016-02-18

申请号：US14783054

申请日：2014-04-11

Applicant: United Technologies Corporation

Inventor： Anton G. Banks ,  Anthony P. Cherolis ,  Donald Kastel

IPC: F01D11/00 ,  F01D9/04

CPC classification number: F01D11/005 ,  F01D9/02 ,  F01D9/04 ,  F01D9/041 ,  F01D9/047 ,  F01D11/00 ,  F01D11/003 ,  F01D25/24 ,  F01D25/246 ,  F05D2220/32 ,  F05D2240/128 ,  F05D2240/55 ,  F05D2240/57 ,  F05D2260/20 ,  F05D2260/97

Abstract: A nozzle segment for a gas turbine engine includes an arcuate outer vane platform segment. An arcuate inner vane platform segment spaced from the arcuate outer vane platform segment. A multiple of airfoils between the arcuate inner vane platform segment and the arcuate outer vane platform segment, the arcuate outer vane platform segment includes a scallop slot and a seal that seals the scallop slot.

Abstract translation: 用于燃气涡轮发动机的喷嘴段包括弓形外叶片平台段。 与弓形外叶片平台段间隔开的弧形内叶片平台段。 弧形内叶片平台段与弧形外叶片平台段之间的多个翼型，弓形外叶片平台段包括扇贝槽和密封扇贝槽的密封件。

公开(公告)号：US20150122031A1

公开(公告)日：2015-05-07

申请号：US14449813

申请日：2014-08-01

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Anton G. Banks ,  Steven Taffett ,  Christopher Laxton

IPC: G01N29/22 ,  G01N29/265 ,  G01N29/44

CPC classification number: G01N29/265 ,  G01N2291/044 ,  G01N2291/101 ,  G01N2291/2638 ,  G01N2291/2693

Abstract: The present disclosure relates generally to a transducer position guide. The transducer position guide may be attached to a component to be measured, such as an airfoil, and controls a path traversed by the transducer during a measurement process.

Abstract translation: 本公开总体上涉及换能器位置导向件。 换能器位置引导件可以附接到要测量的部件，例如翼型件，并且在测量过程期间控制由换能器穿过的路径。