公开(公告)号：US20090051120A1

公开(公告)日：2009-02-26

申请号：US11843850

申请日：2007-08-23

Applicant: Peter M. Munsell ,  Ioannis Alvanos

Inventor： Peter M. Munsell ,  Ioannis Alvanos

IPC: F16J15/34

CPC classification number: F16J15/3464 ,  F01D11/001 ,  F01D11/02

Abstract: Gas turbine engine systems involving hydrostatic face seals are provided. In this regard, representative turbine assembly for a gas turbine engine includes a turbine having a hydrostatic seal formed by a seal face and a seal runner.

Abstract translation: 提供涉及静水面密封的燃气涡轮发动机系统。 在这方面，用于燃气涡轮发动机的代表性涡轮机组件包括具有由密封面和密封转轮形成的静压密封的涡轮机。

公开(公告)号：US20060275107A1

公开(公告)日：2006-12-07

申请号：US11146798

申请日：2005-06-07

Applicant: Ioannis Alvanos ,  Rajendra Agrawal ,  John Virtue ,  James Hill ,  Hector Pinero

Inventor： Ioannis Alvanos ,  Rajendra Agrawal ,  John Virtue ,  James Hill ,  Hector Pinero

IPC: F03B11/00

CPC classification number: F01D5/3007 ,  F01D5/085 ,  F01D11/001 ,  F02C7/28

Abstract: Disclosed are assemblies and articles for restricting leakage of a pressurized fluid from a cavity. In accordance with an embodiment of the invention, a vane support defines at least one land, and an interrupted rim region of a bladed rotor assembly defines at least one segmented ring. The at least one segmented ring protruding outward from the bladed rotor assembly in the interrupted rim region, spans across the cavity and cooperates with the at least one land to define a seal.

Abstract translation: 公开了用于限制加压流体从空腔泄漏的组件和制品。 根据本发明的实施例，叶片支撑件限定至少一个平台，并且叶片转子组件的中断的边缘区域限定至少一个分段环。 在中断的边缘区域中从叶片转子组件向外突出的至少一个分段环跨越空腔并与至少一个平台配合以限定密封。