Title:
【発明の名称】排ガスターボ過給機の軸流タービン
Document Type and Number:
Japanese Patent JP2956834
Kind Code:
B2
Abstract:
The turbine has a gas intake casing (1), gas exit casing (2) with gas intake side wall (5), turbine disc (10) with scoops (11) and a burst prevention ring (8) outside the scoops at a small clearance from their running plane. The burst prevention ring is made as an integral, basically radially extending component of the wall on the gas intake side of the gas exit casing. The burst prevention ring is connected to the gas intake casing, either directly or via an axial elongation piece (6). The gas intake side wall may stem from the burst prevention ring and on which semi-radial extending gas outlet supports (7) may be set.
More Like This:
WO/1995/030076 | FAN BLADE CONTAINMENT ASSEMBLY |
Inventors:
YOOZEFU BETSUTEITSUHI
RUUDORUFU RIKANEKU
RUUDORUFU RIKANEKU
Application Number:
JP11681697A
Publication Date:
October 04, 1999
Filing Date:
May 07, 1997
Export Citation:
Assignee:
ASEA BURAUN BOERI AG
International Classes:
F01D21/04; F01D25/24; F02B39/16; F02C3/04; F02B39/00; F02C7/00; F02C7/05; F16P7/00; (IPC1-7): F01D25/24; F02B39/00; F02B39/16
Domestic Patent References:
JP59168221A | ||||
JP6039703U | ||||
JP5650736U | ||||
JP58564B2 |
Attorney, Agent or Firm:
Toshio Yano (2 outside)