Global Patent Index - EP 1999343 A1

EP 1999343 A1 20081210 - TURBOCHARGER

Title (en)

TURBOCHARGER

Title (de)

TURBOLADER

Title (fr)

TURBOCOMPRESSEUR

Publication

EP 1999343 A1 20081210 (DE)

Application

EP 07723702 A 20070328

Priority

  • EP 2007002757 W 20070328
  • DE 102006014896 A 20060330

Abstract (en)

[origin: WO2007112910A1] The invention relates to a turbocharger (1) with variable turbine geomtry (VTG), comprising a multiplicity of guide blades (7). Each guide blade (7) has a blade lever (19, 19'), wherein the centre plane (Em2) of an intermediate region (24; 24') of the blade lever (19, 19') is arranged so as to be offset axially along a blade shaft longitudinal axis (L) at a distance (a) from the centre plane (Em1) of a first end region (20; 20') of the blade lever (19, 19') and of a second end region (23; 23') of the blade lever (19, 19'), and wherein a recess (26; 26') is arranged adjacent to the intermediate region (24; 24') between the first end region (20; 20') and the second end region (23; 23').

IPC 8 full level

F01D 17/16 (2006.01)

CPC (source: EP KR US)

F01D 17/16 (2013.01 - KR); F01D 17/165 (2013.01 - EP US); F02B 37/22 (2013.01 - KR); F05D 2220/40 (2013.01 - EP US); F05D 2230/64 (2013.01 - EP US); F05D 2250/182 (2013.01 - EP US); F05D 2250/312 (2013.01 - EP US); F05D 2260/50 (2013.01 - EP US); F05D 2260/79 (2013.01 - EP US)

Citation (search report)

See references of WO 2007112910A1

Designated contracting state (EPC)

DE FR GB IT NL

DOCDB simple family (publication)

WO 2007112910 A1 20071011; CN 101405479 A 20090408; EP 1999343 A1 20081210; JP 2009531587 A 20090903; KR 20090007728 A 20090120; US 2011182717 A1 20110728

DOCDB simple family (application)

EP 2007002757 W 20070328; CN 200780010170 A 20070328; EP 07723702 A 20070328; JP 2009501941 A 20070328; KR 20087026096 A 20081024; US 29501307 A 20070328