公开(公告)号：US20150030443A1

公开(公告)日：2015-01-29

申请号：US14286510

申请日：2014-05-23

Applicant: United Technologies Corporation

Inventor： Carl S. Richardson ,  Mark J. Rogers ,  Jonathan J. Earl ,  Kenneth E. Carman ,  Richard K. Hayford

IPC: F01D9/04 ,  F01D25/04

CPC classification number: F01D5/22 ,  F01D9/041 ,  F01D25/06 ,  F01D25/246 ,  Y02T50/672 ,  Y10T29/49236

Abstract: A vane cluster includes a split damped outer shroud and an inner shroud spaced from the split damped outer shroud with a multiple of stator vane airfoils that extend between the split damped outer shroud and the inner shroud.

Abstract translation: 叶片组包括分离的阻尼外护罩和与分开的阻尼外护罩间隔开的内护罩，其具有多个定子叶片翼型件，其在分离的阻尼外护罩和内护罩之间延伸。

公开(公告)号：US10781716B2

公开(公告)日：2020-09-22

申请号：US16253038

申请日：2019-01-21

Applicant: United Technologies Corporation

Inventor： Susan M. Tholen ,  Dominic J. Mongillo ,  Paul M. Lutjen ,  James N. Knapp ,  Virginia L. Ross ,  Jonathan J. Earl ,  Eric A. Hudson

IPC: F01D25/12 ,  F01D11/08 ,  B22C9/10

Abstract: A cooling scheme for a blade outer air seal includes a perimeter cooling arrangement configured to convectively cool a perimeter of the blade outer air seal, and a core cooling arrangement configured to cool a central portion of the blade outer air seal through impingement cooling and to provide film cooling to an inner diameter face of the blade outer air seal.

公开(公告)号：US10119410B2

公开(公告)日：2018-11-06

申请号：US15026011

申请日：2014-09-23

Applicant: United Technologies Corporation

Inventor： Mark J. Rogers ,  Carl S. Richardson ,  Richard K. Hayford ,  Kenneth E. Carman ,  Jonathan J. Earl

IPC: F01D11/00

Abstract: A vane seal system includes a non-rotatable vane segment that has an airfoil with a pocket at one end thereof. The pocket spans in an axial direction between forward and trailing sides, with respect to the airfoil, and in a lateral direction between open lateral sides. A seal member extends in the pocket. The seal member includes a seal element and at least one spring portion that is configured to positively locate the seal member in the axial direction in the pocket. A method for positioning the seal member in a vane seal system includes positively locating the seal member in the axial direction in the pocket using the spring portion.

公开(公告)号：US09988915B2

公开(公告)日：2018-06-05

申请号：US14776181

申请日：2014-03-11

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jonathan J. Earl ,  Carl S. Richardson

IPC: F01D9/04 ,  F01D11/00 ,  F01D25/24

CPC classification number: F01D9/04 ,  F01D9/041 ,  F01D11/005 ,  F01D25/246 ,  F05D2230/51 ,  F05D2240/12 ,  F05D2240/129 ,  F05D2240/57 ,  F05D2250/314 ,  Y02T50/671

Abstract: One exemplary embodiment of this disclosure relates to a stator segment. The stator segment includes a first circumferential end face, and a second circumferential end face. Further, the first and second circumferential end faces are misaligned relative to one another.

公开(公告)号：US20150300205A1

公开(公告)日：2015-10-22

申请号：US14665780

申请日：2015-03-23

Applicant: United Technologies Corporation

Inventor： Matthew R. Willett ,  Charles H. Warner ,  Gerald D. Cassella ,  Jonathan J. Earl ,  Christopher B. Lyons

IPC: F01D25/24 ,  F01D9/04

CPC classification number: F01D25/246 ,  F01D9/041 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/30 ,  F05D2230/60 ,  F05D2240/12 ,  F05D2240/14 ,  F05D2240/80

Abstract: Systems and methods are disclosed for anti-rotation lugs. A stator for a gas turbine engine may comprise an outer shroud, an inner shroud, and a plurality of vanes located between the outer shroud and the inner shroud. A plurality of anti-rotation lugs may be coupled to the inner shroud. The anti-rotation lugs may be configured to contact a diffuser case in order to prevent rotation of the stator. The anti-rotation lugs may comprise a body and a tapered shoulder. The tapered shoulder may distribute stress concentrations in the anti-rotation lugs.

Abstract translation: 公开了用于防旋转凸耳的系统和方法。 用于燃气涡轮发动机的定子可以包括外护罩，内护罩和位于外护罩和内护罩之间的多个叶片。 多个防旋转凸耳可以联接到内护罩。 防旋转凸耳可以被配置为接触扩散器壳体以防止定子旋转。 防旋转凸耳可以包括主体和锥形肩部。 锥形肩部可以在抗旋转凸耳中分布应力集中。