公开(公告)号：EP2895283A4

公开(公告)日：2015-10-21

申请号：EP13837198

申请日：2013-09-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BULLIED STEVEN J ,  VERNER CARL R ,  PORTER STEVEN D ,  PARK JAMES B

IPC: B22C9/10 ,  B22C7/02 ,  B22C9/04

CPC classification number: F01D9/041 ,  B22C7/02 ,  B22C9/04 ,  B22C9/10 ,  B22C9/108 ,  B22C9/24 ,  B22D25/02 ,  B22D29/001 ,  F01D5/187 ,  F05D2230/21 ,  F05D2230/211 ,  Y02T50/671 ,  Y02T50/673 ,  Y02T50/676

Abstract: A casting mold assembly includes an airfoil defining section and a casting core. The airfoil defining section includes an outer mold wall and a direct-shelled inner mold wall. The direct-shelled inner mold wall is disposed within a forward chordwise portion of the airfoil defining section. The direct-shelled inner mold wall includes an aft end having an external radius measuring more than about 0.075 in. (1.9 mm). The casting core is secured within an aft chordwise portion of the airfoil defining section, and includes an aft end with an external radius measuring less than about 0.075 in. (1.9 mm). A cast component and a method for making the casting mold assembly are also disclosed.

公开(公告)号：EP3052764A4

公开(公告)日：2016-11-16

申请号：EP14850260

申请日：2014-09-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OLS JOHN T ,  ALLEN RICHARD N ,  PORTER STEVEN D ,  SANCHEZ PAUL K

IPC: F01D9/04

CPC classification number: F01D9/041 ,  F05D2220/32 ,  F05D2240/122 ,  F05D2240/80 ,  F05D2260/941 ,  Y02T50/671

公开(公告)号：EP3008291A4

公开(公告)日：2016-08-31

申请号：EP14836398

申请日：2014-05-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OLS JOHN T ,  ALLEN RICHARD N ,  PORTER STEVEN D

IPC: F01D9/00 ,  F01D5/14 ,  F01D9/02 ,  F01D9/04 ,  F01D25/24

CPC classification number: F01D9/041 ,  F01D5/143 ,  F01D9/042 ,  F01D9/047 ,  F01D25/24 ,  F05D2240/121 ,  F05D2240/122 ,  F05D2240/80 ,  Y02T50/673

Abstract: A vane for use in a gas turbine engine has an airfoil extending between a leading edge and a trailing edge, and is generally hollow. The vane has a radially outer platform and a radially inner platform. At least one of the radially inner and radially outer platforms has thicker portions circumferentially located beyond one of the leading edge and the trailing edge, and thinner portions circumferentially beyond circumferential edges of the airfoil. A mid-turbine frame and a gas turbine engine are also disclosed.

公开(公告)号：EP3022400A4

公开(公告)日：2016-07-20

申请号：EP14825846

申请日：2014-06-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OLS JOHN T ,  MENTZ KARL A ,  ALLEN RICHARD N ,  PORTER STEVEN D ,  JUREK RENEE J ,  SANCHEZ PAUL K ,  PINERO SANDRA S

IPC: F01D9/04 ,  F01D5/02 ,  F01D5/14 ,  F01D25/24

CPC classification number: F01D9/041 ,  F01D5/02 ,  F01D5/143 ,  F01D9/04 ,  F01D25/246 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/303 ,  F05D2240/304 ,  F05D2240/80 ,  F05D2250/71 ,  F05D2250/90 ,  Y02T50/673

Abstract: An airfoil extends between radially inner and radially outer platforms. The airfoil extends between a leading edge and a trailing edge, and merges into facing surfaces of the radially inner and outer platforms. A variable fillet merges a facing surface of one of the radially inner and outer platforms into a wall of the airfoil. The variable fillet has a length extending away from a surface of the airfoil and a height extending away from the facing surface of at least one of the radially inner and outer platforms outwardly on to the airfoil. The variable fillet has a greater length at one of the leading edge and the trailing edge. A spaced portion has a shorter length at locations spaced from at least one of the leading and trailing edges. A mid-turbine frame and a gas turbine engine are also disclosed.

Abstract translation: 翼型件在径向内部和径向外部平台之间延伸。 翼型件在前缘和后缘之间延伸，并且合并到径向内外平台的相对表面中。 可变圆角将径向内平台和外平台之一的面对面融合到翼型的壁中。 可变圆角具有远离翼型件的表面延伸的长度，并且从径向内部和外部平台中的至少一个的相对表面向外延伸到翼型的高度。 可变圆角在前缘和后缘之一处具有更大的长度。 间隔部分在与前缘和后缘中的至少一个间隔开的位置处具有较短的长度。 还公开了中涡轮机架和燃气涡轮发动机。

公开(公告)号：EP2951404A4

公开(公告)日：2016-06-15

申请号：EP14786006

申请日：2014-01-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PORTER STEVEN D ,  FEINDEL DAVID T ,  BUDNICK MATTHEW ,  CHUONG CONWAY

IPC: F01D25/00 ,  F01D11/00 ,  F01D21/00

CPC classification number: F01D21/003 ,  F05D2260/80 ,  F05D2260/83 ,  G02B23/2476

Abstract: A borescope plug assembly includes a borescope plug having a shaft section and a tip section, a bushing engageable with the shaft section and a seal engageable with the tip section.

Abstract translation: 管道插头组件包括具有轴部分和尖端部分的管道插塞，可与轴部分接合的衬套和可与尖端部分接合的密封件。

公开(公告)号：EP2855889A4

公开(公告)日：2016-01-13

申请号：EP13801167

申请日：2013-05-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GORDON AMY M ,  JAKIEL JONATHAN J ,  BURT JONATHAN P ,  PORTER STEVEN D

IPC: F02C7/28 ,  F01D11/00 ,  F01D25/16 ,  F02C3/00

CPC classification number: F04D29/083 ,  F01D11/005 ,  F01D25/162 ,  F02C7/28 ,  F04D29/542

Abstract: A seal land for a gas turbine engine can include a seal body that can extend between a leading edge portion, a trailing edge portion, a radially outer surface and a radially inner surface. A notch can extend at least partially through the seal body between the radially outer surface and the radially inner surface.