The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 20, 2018

Filed:

Sep. 24, 2015
Applicant:

Abb Turbo Systems Ag, Baden, CH;

Inventors:

Fabrizio Lanni, Pfaffikon, CH;

Matthias Jarusel, Albbruck, DE;

Reiner Probst, Noeggenschwiel, DE;

Rudolf Roder, Thun, CH;

Hans Baumgartner, Munchenbuchsee, CH;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/24 (2006.01); F01D 25/28 (2006.01); F01D 5/02 (2006.01); F02B 33/40 (2006.01); F04D 17/10 (2006.01); F02B 37/00 (2006.01); F04D 25/02 (2006.01); F04D 29/62 (2006.01); F16M 1/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/28 (2013.01); F01D 5/02 (2013.01); F01D 25/24 (2013.01); F01D 25/285 (2013.01); F02B 33/40 (2013.01); F02B 37/00 (2013.01); F04D 17/10 (2013.01); F04D 25/024 (2013.01); F04D 29/624 (2013.01); F16M 1/04 (2013.01); F05D 2220/40 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2230/72 (2013.01); F05D 2240/20 (2013.01); F05D 2250/41 (2013.01); Y10T 29/49009 (2015.01); Y10T 29/49012 (2015.01); Y10T 29/49318 (2015.01); Y10T 29/49321 (2015.01); Y10T 29/53143 (2015.01); Y10T 29/53961 (2015.01);
Abstract

A lifting apparatus for assembly of exhaust turbocharger allows the removal of the rotor block from the housing in a horizontal direction. The lifting apparatus includes a cantilever, which is fastened on a vertical stop, i.e. on an axial end, of the housing, and on which there is arranged a structure which can be moved along the cantilever and which is likewise fastened on a vertical stop, i.e. an axial end of the rotor block.


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