Title:
軸流排気タービンの案内翼装置
Document Type and Number:
Japanese Patent JP4526055
Kind Code:
B2
Abstract:
The conducting apparatus is for the position alteration of conducting blades (6) in a turbocharger exhaust gas turbine flowed through axially. The blades are arranged axially symmetrically to the turbine axis (1) in an exhaust gas flow channel (14) and can be pivoted by a pivot device around a radially fitted axis (8). To each blade is fitted a shaft (18) which extends through a housing wall radially outwards from the flow channel. This shaft with its outwardly extending part is rotatably located around a pivot axis (8). The pivot device contains a positioning ring (19) rotatable around the turbine axis and positioning levers (20) transmit torque from the positioning ring to the shaft of each blade.
Inventors:
Berent Datingref
Bets joseph
Sailer Martin
Bets joseph
Sailer Martin
Application Number:
JP2001567904A
Publication Date:
August 18, 2010
Filing Date:
March 06, 2001
Export Citation:
Assignee:
Arbor turbo systems acti genzel shaft
International Classes:
F01D17/16; F02B37/24; F01D25/24; F02B39/00
Domestic Patent References:
| JP63069736U | ||||
| JP61128342U | ||||
| JP61065202U |
Attorney, Agent or Firm:
Mitsufumi Esaki
Tsuneo Mihara
Blacksmith
Tsuneo Mihara
Blacksmith