公开(公告)号：WO2014196987A3

公开(公告)日：2015-02-26

申请号：PCT/US2013046819

申请日：2013-06-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DEAL JAMES L ,  SCHIRRA JOHN J ,  DROZDENKO LEE ,  GRAVES WILLIAM R ,  HANSEN JAMES O ,  WEISSE MICHAEL A ,  WATSON THOMAS J

IPC: F01D5/14 ,  F01D5/28 ,  F04D29/38

CPC classification number: F01D5/288 ,  F01D5/147 ,  F04D29/023 ,  F04D29/324 ,  F05D2220/36 ,  F05D2230/23 ,  F05D2240/303 ,  F05D2300/121 ,  F05D2300/124 ,  F05D2300/174 ,  Y02T50/672

Abstract: A fan blade comprises an airfoil portion and a sheath portion. The sheath portion has a sheath head section, a first sheath flank, and a second sheath flank, both flanks extending chordwise from the forward sheath section. The sheath portion is bonded to the airfoil portion such that the sheath head section covers the forward airfoil edge, defining a blade leading edge. The first sheath flank covers a portion of the first airfoil surface proximate the airfoil forward edge, jointly defining a blade suction surface. The second sheath flank covers a portion of the second airfoil surface proximate the airfoil forward edge, jointly defining a blade pressure surface. The first metallic material is an aluminum alloy containing between about 0.5 wt% and about 3.0 wt% of lithium.

Abstract translation: 风扇叶片包括翼型部分和鞘部分。 护套部分具有鞘头部分，第一护套侧面和第二护套侧面，两个侧面从前鞘部分向翼伸出。 护套部分结合到翼型部分，使得鞘头部分覆盖前翼型边缘，限定叶片前缘。 第一护套侧面覆盖靠近翼型件前缘的第一翼型件表面的一部分，共同限定叶片抽吸表面。 第二护套侧面覆盖靠近翼型件前缘的第二翼型件表面的一部分，共同限定叶片压力表面。 第一种金属材料是含有约0.5wt％至约3.0wt％的锂的铝合金。

公开(公告)号：WO2014204542A2

公开(公告)日：2014-12-24

申请号：PCT/US2014031818

申请日：2014-03-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： COSBY JAMES ,  HUI KWAN ,  WEISSE MICHAEL A

CPC classification number: F01D5/3007 ,  F01D5/12 ,  F01D5/141 ,  F01D5/28 ,  F01D5/30 ,  F01D5/3023 ,  F01D5/303 ,  F01D5/3038 ,  F01D5/3053 ,  Y02T50/671 ,  Y02T50/673

Abstract: A blade for use in a gas turbine engine has an airfoil and a dovetail. The airfoil extends radially outwardly of the dovetail. An inner surface of the dovetail includes a slot extending along a length of the dovetail between a leading edge and a trailing edge. A rotor and a gas turbine engine are also disclose

Abstract translation: 用于燃气涡轮发动机的叶片具有翼型件和燕尾形件。 翼型件沿燕尾径向向外延伸。 燕尾榫的内表面包括沿着燕尾榫的长度在前缘和后缘之间延伸的槽。 还公开了一种转子和燃气涡轮发动机

公开(公告)号：WO2015102715A3

公开(公告)日：2015-11-12

申请号：PCT/US2014059897

申请日：2014-10-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WEISSE MICHAEL A ,  HUI KWAN

IPC: F01D5/18

CPC classification number: F04D29/388 ,  F01D5/147 ,  F01D5/282 ,  F04D29/023 ,  F04D29/325 ,  F05D2220/36 ,  F05D2250/75 ,  Y02T50/672

Abstract: A fan blade has a blade body, a composite rib and a cover. The blade body extends from a blade root to an opposed blade tip along a longitudinal axis. The blade body defines a leading edge and a trailing edge. A first airfoil surface extends from the leading edge to the trailing edge A pocket is defined between the leading edge, the trailing edge, the blade root, and the blade tip. The pocket has a bottom surface that opposes the first airfoil surface across the blade body. The composite rib is disposed in the pocket. The cover is mounted to the composite rib and the blade body to form a second airfoil surface opposed to the first airfoil surface.

Abstract translation: 风扇叶片具有叶片体，复合肋和盖。 叶片主体沿着纵向轴线从叶片根部延伸到相对的叶片尖端。 刀片主体限定前缘和后缘。 第一翼型表面从前缘延伸到后缘。凹口限定在前缘，后缘，刀根和刀尖之间。 口袋具有与刀片体上的第一翼型表面相对的底面。 复合肋设置在口袋中。 盖子安装到复合肋和刀片体上以形成与第一翼型件表面相对的第二翼型件表面。

公开(公告)号：DE602005008119D1

公开(公告)日：2008-08-28

申请号：DE602005008119

申请日：2005-01-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WHITESELL DANIEL J ,  PALAZZINI CHRISTOPHER M ,  WEISSE MICHAEL A

IPC: B23P15/04 ,  F01D5/14 ,  F01D5/18 ,  F02C3/06 ,  F02C7/16 ,  F04D29/32 ,  F04D29/38

Abstract: A method for making a hollow fan blade includes the steps of: forming a plurality of ribs (42) on a first substrate (31), the first substrate (31) including cavities (40) on either side of each of the plurality of ribs; abutting the plurality of ribs (42) on the first substrate (31) with a second substrate (31) to form a hollow fan blade (30); and forming the hollow fan blade (30) into an airfoil shape while pressure inside the cavities (40) is substantially ambient pressure.

公开(公告)号：WO2015099861A3

公开(公告)日：2015-11-12

申请号：PCT/US2014059895

申请日：2014-10-09

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HUI KWAN ,  WEISSE MICHAEL A

IPC: F01D5/14 ,  F01D5/18

CPC classification number: F04D29/388 ,  F01D5/147 ,  F01D5/282 ,  F02K3/06 ,  F04D29/023 ,  F04D29/325 ,  F05D2220/36 ,  F05D2300/133 ,  F05D2300/603 ,  Y02T50/672

Abstract: A fan blade includes a blade body, a composite segment and a cover. The blade body extends from a blade root to an opposed blade tip along a longitudinal axis. The blade body defines a leading edge and a trailing edge. A first airfoil surface extends from the leading edge to the trailing edge. A pocket is defined between the leading edge, the trailing edge, the blade root and the blade tip. The pocket has a bottom surface that opposes the first airfoil surface across the blade body. The composite segment is disposed in the pocket. The cover is mounted to the composite segment and to the blade body to form a second airfoil surface opposed to the first airfoil surface.

Abstract translation: 风扇叶片包括叶片主体，复合段和盖。 叶片主体沿着纵向轴线从叶片根部延伸到相对的叶片尖端。 刀身限定前缘和后缘。 第一翼型表面从前缘延伸到后缘。 在前缘，后缘，叶根和叶尖之间形成一个口袋。 该袋具有横跨叶片主体与第一翼型表面相对的底表面。 复合段被放置在口袋中。 盖被安装到复合段和叶片体以形成与第一翼型表面相对的第二翼型表面。

公开(公告)号：WO2014099634A3

公开(公告)日：2014-11-27

申请号：PCT/US2013074847

申请日：2013-12-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  WEISSE MICHAEL A ,  ZYSMAN STEVEN H

IPC: F01D5/12 ,  F01D5/22 ,  F01D7/02 ,  F04D29/34 ,  F04D29/38

CPC classification number: F01D5/225 ,  F04D25/028 ,  F04D29/324 ,  F04D29/666 ,  F04D29/668 ,  F05D2220/36 ,  F05D2250/14 ,  Y02T50/671 ,  Y02T50/673

Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a fan section including a fan with a plurality of fan blades rotatable about an axis. Each of the plurality of fan blades includes a mid-span shroud and a speed change device in communication with the fan.

Abstract translation: 除了别的之外，根据本公开的示例性方面的燃气涡轮发动机包括风扇部分，该风扇部分包括具有多个绕轴线可旋转的风扇叶片的风扇。 多个风扇叶片中的每一个包括中跨度护罩和与风扇连通的变速装置。

公开(公告)号：WO2014031203A3

公开(公告)日：2014-05-01

申请号：PCT/US2013042884

申请日：2013-05-28

Applicant: UNITED TECHNOLOGIES CORP

Inventor： HUI KWAN ,  WEISSE MICHAEL A

IPC: F01D5/14 ,  F02C3/04

CPC classification number: F01D5/141 ,  B23P15/04 ,  F01D5/147 ,  F01D5/282 ,  F04D29/023 ,  F04D29/324 ,  F05D2220/36 ,  F05D2230/23 ,  F05D2260/941 ,  F05D2300/50212 ,  F05D2300/603 ,  F05D2300/615 ,  Y02T50/672 ,  Y02T50/673 ,  Y10T29/49236

Abstract: An example airfoil for a gas turbine engine includes a body having a first surface extending from a first edge to a second edge and a cavity disposed in the body. A first cover is at least partially disposed within the cavity. The first cover includes a first portion cooperates with a corresponding second portion. A second cover covers the first cover and forms at least a portion of the first surface with the body. The first cover is disposed between the body and the second cover. The first cover and the second cover have a different coefficient of thermal expansion than the body.

Abstract translation: 用于燃气涡轮发动机的示例性翼型件包括具有从第一边缘延伸到第二边缘的第一表面的主体和设置在主体中的空腔。 第一盖至少部分地设置在腔内。 第一盖包括与对应的第二部分配合的第一部分。 第二盖覆盖第一盖并且与主体形成第一表面的至少一部分。 第一盖设置在主体和第二盖之间。 第一盖和第二盖具有与身体不同的热膨胀系数。

公开(公告)号：DE602005003973D1

公开(公告)日：2008-02-07

申请号：DE602005003973

申请日：2005-01-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PALAZZINI CHRISTOPHER M ,  WEISSE MICHAEL A ,  SENECAL DOUGLAS A

IPC: B23P15/04 ,  F01D5/14 ,  F01D5/18 ,  F02C7/00 ,  F04D29/32 ,  F04D29/38

Abstract: Hollow fan blades (30) for turbo fan gas turbine engines are formed of two separate detail halves (30a;30b). Each detail half (30a;30b) has a plurality of cavities (40) and ribs (42) machined out to reduce weight. The floor (48) and opposite interior walls (50) of each cavity (40) are machined simultaneously. The configuration minimizes the number of cutter plunge cuts for the internal cavities, and maximizes cutter size, in order to minimize the time required to machine them. These detail halves (30a;30b) are subsequently bonded and given an airfoil shape in the forming operation.

公开(公告)号：DE3917937A1

公开(公告)日：1989-12-07

申请号：DE3917937

申请日：1989-06-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CHAPLIN GARY F ,  PANNONE JOHN L ,  WEISSE MICHAEL A

IPC: F01D9/02 ,  F01D5/22 ,  F01D11/00 ,  F01D11/02

Abstract: A stator vane assembly 30 for a rotary machine is disclosed. The stator vane assembly includes an array of stator vanes 44 and an inner air seal 46. Various construction details which damp vibrational stresses in the vanes are developed. In one embodiment, the stator vanes slidably engage the inner air seal. The inner air seal is urged radially into sliding contact with the vanes at the inner ends 52 of the vanes by a resilient device such as a radial spring member 70. In one detailed embodiment, the stator vane has at least two airfoils 55b,c which are circumferentially spaced at their inner ends leaving a circumferential gap therebetween.

公开(公告)号：SG173949A1

公开(公告)日：2011-09-29

申请号：SG2010093862

申请日：2010-12-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DEAL JAMES L ,  GRAVES WILLIAM R ,  WEISSE MICHAEL A

Abstract: A blade includes a hollow metal airfoil having an opening to an internal cavity in a first major surface. A metal cover is adhesively bonded to a socket formed around the opening. The cover encloses the cavity and provides a continuous first major surface.(Figure 3B)