公开(公告)号：US07530782B2

公开(公告)日：2009-05-12

申请号：US11223129

申请日：2005-09-12

Applicant: Barry Barnett ,  Bruce Fielding

Inventor： Barry Barnett ,  Bruce Fielding

IPC: F01D9/00

CPC classification number: F01D9/042 ,  F02C7/05 ,  F05D2260/30

Abstract: A vane assembly for a gas turbine engine including a shroud with openings defined about a circumference of the shroud and vanes extending radially from the shroud with a vane tip in each opening. Isolating apparatus are disposed in each opening to isolate the vane tip from the shroud ring. Each vane tip is engaged with the shroud by retaining apparatus for restricting movement of the vane tip in an axial direction relative to the shroud.

Abstract translation: 一种用于燃气涡轮发动机的叶片组件，其包括具有围绕所述护罩的圆周限定的开口的护罩和在每个开口中具有从所述护罩径向延伸的叶片。 隔离装置设置在每个开口中以将叶片尖端与护罩环隔离。 每个叶片尖端通过保持装置与护罩接合，以限制叶片尖端在相对于护罩的轴向上的运动。

公开(公告)号：US07413400B2

公开(公告)日：2008-08-19

申请号：US11223148

申请日：2005-09-12

Applicant: Barry Barnett

Inventor： Barry Barnett

IPC: F01D9/00

CPC classification number: F01D9/042 ,  F02C7/05 ,  F05D2260/30

Abstract: A vane assembly for a gas turbine engine including a shroud ring with openings and isolating arrangement isolating a vane extremity within each opening, the isolating arrangement cooperating to form a continuous gas path surface completely covering at least an axial portion of a surface of the shroud ring.

Abstract translation: 一种用于燃气涡轮发动机的叶片组件，其包括具有开口的护罩环和将每个开口内的叶片末端隔离的隔离装置，所述隔离装置配合以形成完全覆盖所述护罩环的表面的至少轴向部分的连续气体路径表面 。

公开(公告)号：US20080086881A1

公开(公告)日：2008-04-17

申请号：US11537890

申请日：2006-10-02

Applicant: Andreas Eleftheriou ,  Steven Bokan ,  Barry Barnett ,  Steven Hunt ,  Czeslaw Wojtyczka ,  John Paterson

Inventor： Andreas Eleftheriou ,  Steven Bokan ,  Barry Barnett ,  Steven Hunt ,  Czeslaw Wojtyczka ,  John Paterson

IPC: B23P15/04

CPC classification number: F01D25/24 ,  F01D21/045 ,  F05D2230/20 ,  F05D2230/26 ,  F05D2230/50 ,  F05D2240/14 ,  Y02T50/671 ,  Y10T29/4932

Abstract: The method is used for making an annular gas turbine engine case, the method comprises flowforming a first area of the preform to provide a first annular case portion having a first thickness and a second area having a second thickness, the first and the second average thickness being different.

Abstract translation: 该方法用于制造环形燃气涡轮发动机壳体，该方法包括流动成形预成型件的第一区域以提供具有第一厚度的第一环形壳体部分和具有第二厚度的第二区域，第一和第二平均厚度 不同

公开(公告)号：US20080080971A1

公开(公告)日：2008-04-03

申请号：US11528648

申请日：2006-09-28

Applicant: Barry Barnett

Inventor： Barry Barnett

IPC: F03B11/00

CPC classification number: F01D11/02 ,  B23P6/005 ,  B23P11/025 ,  F05D2230/80 ,  Y10T29/49318 ,  Y10T29/49719 ,  Y10T29/4973

Abstract: A method and apparatus for repairing damaged fins in a labyrinth seal, the seal without the use of welding or metallurgical bonding. The method comprises the steps of removing a section of the shaft containing the damaged fins, and providing a sleeve with replacement fins.

Abstract translation: 用于修复迷宫式密封件中损坏的翅片的方法和装置，密封件不使用焊接或冶金结合。 该方法包括以下步骤：去除包含损坏的翅片的轴的一部分，并为套筒提供替换翅片。

公开(公告)号：US07306432B2

公开(公告)日：2007-12-11

申请号：US11224090

申请日：2005-09-13

Applicant: Sean André Rockarts ,  Barry Barnett

Inventor： Sean André Rockarts ,  Barry Barnett

IPC: F01D5/02

CPC classification number: F02K3/04 ,  F01D5/027 ,  F16F15/34 ,  G01M1/32 ,  Y02T50/671

Abstract: An apparatus for balancing a shaft of an aircraft engine preferably includes a nose cone and the use of standard fasteners. The nose cone is adapted to cooperate with at least one standard fastener to retain the standard fastener to the nose cone to rotationally balance the shaft.

Abstract translation: 用于平衡飞机发动机的轴的装置优选地包括鼻锥和使用标准紧固件。 鼻锥体适于与至少一个标准紧固件配合，以将标准紧固件保持在鼻锥体上以旋转平衡轴。

公开(公告)号：US20060188379A1

公开(公告)日：2006-08-24

申请号：US11224090

申请日：2005-09-13

Applicant: Sean Rockarts ,  Barry Barnett

Inventor： Sean Rockarts ,  Barry Barnett

IPC: F01D5/30

CPC classification number: F02K3/04 ,  F01D5/027 ,  F16F15/34 ,  G01M1/32 ,  Y02T50/671

Abstract: An apparatus for balancing a shaft of an aircraft engine preferably includes a nose cone and the use of standard fasteners. The nose cone is adapted to cooperate with at least one standard fastener to retain the standard fastener to the nose cone to rotationally balance the shaft.

Abstract translation: 用于平衡飞机发动机的轴的装置优选地包括鼻锥和使用标准紧固件。 鼻锥体适于与至少一个标准紧固件配合，以将标准紧固件保持在鼻锥体上以旋转平衡轴。