公开(公告)号：GB2418955A

公开(公告)日：2006-04-12

申请号：GB0513290

申请日：2005-06-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PENDA ALLAN R ,  BURGE JOSEPH C

IPC: F04D29/16 ,  F01D11/08 ,  F01D11/16 ,  F01D11/18 ,  F01D11/22 ,  F04D29/08 ,  F04D29/54

Abstract: A turbine engine has a circumferentially segmented shroud 62 within a case structure 70. Each shroud segment (66) is mounted for movement between an inboard position and an outboard position. One or more springs 130 bias the shroud segments (66) toward their inboard positions. One or more valves 144 are positioned to vent one or more volumes 150 so as to counter the spring bias to shift the shroud segments (66) to their outboard positions.

公开(公告)号：DE69627915T2

公开(公告)日：2003-11-13

申请号：DE69627915

申请日：1996-02-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： EL-AINI YEHIA M ,  BURGE JOSEPH C ,  MEECE CARL E

IPC: F01D5/16

Abstract: A rotor blade (14) for a turbine engine rotor assembly (10) is provided with apparatus for damping vibrations in the blade. The blade includes a pocket (26) formed in a surface. The apparatus for damping vibrations in the blade includes a damper (34) and a pocket lid (36). The damper (34) is received within the pocket (26) between an inner surface (32) of the pocket (26) and the pocket lid (36). The pocket lid is attached to the airfoil and contoured to match the curvature of the airfoil. The damper may be of a sinusoidal shape, or may comprise a plurality of strands (39) formed in a mesh (38).

公开(公告)号：GB2418955B

公开(公告)日：2009-07-08

申请号：GB0513290

申请日：2005-06-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PENDA ALLAN R ,  BURGE JOSEPH C

IPC: F04D29/16 ,  F01D11/08 ,  F01D11/16 ,  F01D11/18 ,  F01D11/22 ,  F04D29/08 ,  F04D29/54

公开(公告)号：CA2511635A1

公开(公告)日：2006-01-09

申请号：CA2511635

申请日：2005-07-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PENDA ALLAN R ,  BURGE JOSEPH C

IPC: F01D11/22 ,  F01D11/16

Abstract: A turbine engine has a circumferentially segmented shroud within a case structure. Each shroud segment is mounted for movement between an inboard position and an outboard position. One or more springs bias the shroud segments toward their inboard positions. One or more valves are positioned to vent one or more volumes so as to counter the spring bias to shift the shroud segments to their outboard positions.

公开(公告)号：DE102005032068A1

公开(公告)日：2006-02-02

申请号：DE102005032068

申请日：2005-07-08

Applicant: UNITED TECHNOLOGIES CORP HARTF

Inventor： PENDA ALLAN R ,  BURGE JOSEPH C

IPC: F01D11/04 ,  F01D11/16 ,  F01D11/22

公开(公告)号：FR2872870A1

公开(公告)日：2006-01-13

申请号：FR0507202

申请日：2005-07-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： PENDA ALLAN R ,  BURGE JOSEPH C

IPC: F04D29/52 ,  F01D11/16 ,  F01D11/22

Abstract: Un moteur à turbine (20) comprend un flasque (62, 64) segmenté dans le sens circonférentiel dans une structure de carter. Chaque segment de flasque (66, 68) est monté pour un mouvement entre une position intérieure et une position extérieure. Un ou plusieurs ressorts (130, 132, 134) sollicitent les segments de flasque (66, 68) vers leurs positions intérieures. Une ou plusieurs soupapes (144, 146) sont positionnées pour dégazer un ou plusieurs volumes de manière à contrer la sollicitation du ressort pour décaler les segments de flasque (66, 68) vers leurs positions extérieures.

公开(公告)号：DE69627915D1

公开(公告)日：2003-06-12

申请号：DE69627915

申请日：1996-02-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： EL-AINI YEHIA M ,  BURGE JOSEPH C ,  MEECE CARL E

IPC: F01D5/16

Abstract: A rotor blade (14) for a turbine engine rotor assembly (10) is provided with apparatus for damping vibrations in the blade. The blade includes a pocket (26) formed in a surface. The apparatus for damping vibrations in the blade includes a damper (34) and a pocket lid (36). The damper (34) is received within the pocket (26) between an inner surface (32) of the pocket (26) and the pocket lid (36). The pocket lid is attached to the airfoil and contoured to match the curvature of the airfoil. The damper may be of a sinusoidal shape, or may comprise a plurality of strands (39) formed in a mesh (38).

公开(公告)号：EP0727563A3

公开(公告)日：1998-11-04

申请号：EP96301044

申请日：1996-02-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： EL-AINI YEHIA M ,  BURGE JOSEPH C ,  MEECE CARL E

IPC: F01D5/16

CPC classification number: F01D5/16 ,  Y10S416/50

Abstract: A rotor blade (14) for a turbine engine rotor assembly (10) is provided with apparatus for damping vibrations in the blade. The blade includes a pocket (26) formed in a surface. The apparatus for damping vibrations in the blade includes a damper (34) and a pocket lid (36). The damper (34) is received within the pocket (26) between an inner surface (32) of the pocket (26) and the pocket lid (36). The pocket lid is attached to the airfoil and contoured to match the curvature of the airfoil. The damper may be of a sinusoidal shape, or may comprise a plurality of strands (39) formed in a mesh (38).

Abstract translation: 提供了一种用于涡轮发动机转子组件的转子叶片，其包括根部，翼型件，平台以及用于阻尼翼型件中的振动的装置。 翼型件包括形成在弦向表面中的口袋。 用于阻尼叶片中的振动的装置包括阻尼器和袋盖。 阻尼器容纳在口袋的内表面和口袋盖之间的口袋内。 口袋盖通过传统的附接装置附接到翼型，并且轮廓以匹配翼型的曲率。