US2015050126A1PendingUtilityA1

Exhaust-gas turbocharger

Assignee: BORGWARNER INCPriority: Mar 1, 2012Filed: Feb 21, 2013Published: Feb 19, 2015
Est. expiryMar 1, 2032(~5.6 yrs left)· nominal 20-yr term from priority
F04D 29/054F01D 5/025F05D 2300/174F05D 2230/238F05D 2230/232F05D 2220/40
42
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Claims

Abstract

An exhaust-gas turbocharger ( 1 ) having a shaft ( 2 ), which has a first centric bore ( 4 ) on an end face ( 3 ), a turbine wheel ( 5 ), which has a second centric bore ( 7 ) in the wheel rear side ( 6 ) thereof, a connection piece ( 8 ), which engages into the first and second bores ( 4, 7 ); and an integral connection device ( 9 ) for connecting the shaft ( 2 ) to the turbine wheel ( 5 ), wherein the connection piece ( 8 ) is hollow in form.

Claims

exact text as granted — not AI-modified
1 . An exhaust-gas turbocharger ( 1 ) having
 a shaft ( 2 ), which has a first centric bore ( 4 ) on an end face ( 3 );   a turbine wheel ( 5 ) having a wheel rear side ( 6 ), which has a second centric bore ( 7 ) in the wheel rear side ( 6 ) thereof;   a connection piece ( 8 ), which engages into the first and second bores ( 4 ,  7 ); and   an integral connection device ( 9 ) for connecting the shaft ( 2 ) to the turbine wheel ( 5 ),   
       wherein
 the connection piece ( 8 ) is hollow in form. 
 
     
     
         2 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the connection piece ( 8 ) is in the form of a bored-out sleeve. 
     
     
         3 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the connection piece ( 8 ) is in the form of a hollow clamping sleeve. 
     
     
         4 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the connection piece ( 8 ) has a circular-cylindrical cross section. 
     
     
         5 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the connection piece ( 8 ) has an angular cross section. 
     
     
         6 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the turbine wheel ( 5 ) is formed from TiAl material. 
     
     
         7 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the shaft ( 2 ) is formed from steel. 
     
     
         8 . The exhaust-gas turbocharger as claimed in  claim 1 , wherein the integral connection device ( 9 ) is a soldered, adhesively bonded or welded connection. 
     
     
         9 . A rotor of an exhaust-gas turbocharger ( 1 ), having
 a shaft ( 2 ), which has a first centric bore ( 4 ) on an end face ( 3 );   a turbine wheel ( 5 ) having a wheel rear side ( 6 ), which has a second centric bore ( 7 ) in the wheel rear side ( 6 ) thereof;   a connection piece ( 8 ), which engages into the first and second bores ( 4 ,  7 ); and   an integral connection device ( 9 ) for connecting the shaft ( 2 ) to the turbine wheel ( 5 ),   
       wherein
 the connection piece ( 8 ) is hollow in form. 
 
     
     
         10 . The rotor as claimed in  claim 9 , wherein the connection piece ( 8 ) is in the form of a bored-out sleeve. 
     
     
         11 . The rotor as claimed in  claim 9 , wherein the connection piece ( 8 ) is in the form of a hollow clamping sleeve. 
     
     
         12 . The rotor as claimed in  claim 9 , wherein the connection piece ( 8 ) has a circular-cylindrical cross section. 
     
     
         13 . The rotor as claimed in  claim 9 , wherein the connection piece ( 8 ) has an angular cross section. 
     
     
         14 . The rotor as claimed in  claim 9 , wherein the turbine wheel ( 5 ) is formed from TiAl material. 
     
     
         15 . The rotor as claimed in  claim 9 , wherein the shaft ( 2 ) is formed from steel. 
     
     
         16 . The rotor as claimed in  claim 9 , wherein the integral connection device ( 9 ) is a soldered, adhesively bonded or welded connection.

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