公开(公告)号：US10794191B1

公开(公告)日：2020-10-06

申请号：US15869122

申请日：2018-01-12

Applicant: United Technologies Corporation

Inventor： Charles H. Warner ,  Carl S. Richardson ,  Jeff M. Carrico ,  Robert W. Fessenden

IPC: F01D5/14 ,  F01D5/16 ,  F01D5/30

Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 0.78-0.91 inch (19.7-23.1 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 0.49-0.62 inch (12.5-15.6 mm). The airfoil element includes at least two of a first mode with a frequency of 3533±15% Hz, a second mode with a frequency of 8291±15% Hz, a third mode with a frequency of 17362±15% Hz and a fourth mode with a frequency of 23365±15% Hz.

公开(公告)号：US20160333890A1

公开(公告)日：2016-11-17

申请号：US15110856

申请日：2014-12-26

Applicant: UNITED TECHNOLOGIES CORPORATION

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

IPC: F04D29/54 ,  F04D29/52 ,  F04D29/64

CPC classification number: F04D29/542 ,  F01D9/042 ,  F04D29/023 ,  F04D29/522 ,  F04D29/644 ,  F05B2220/302 ,  F05B2240/124 ,  F05B2280/10743 ,  F05B2280/50032 ,  F05D2220/3219 ,  F05D2230/642 ,  F05D2240/129 ,  F05D2300/177 ,  F05D2300/50212

Abstract: A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.

Abstract translation: 燃气涡轮发动机包括可滑动地支撑在内壳体护罩段中的周向阵列的叶片。 多个段彼此固定以提供环形发动机静态结构部分。 内壳护罩段和叶片具有彼此不同的材料性质。

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。