US2013045082A1PendingUtilityA1

Compressor of an exhaust-gas turbocharger

Assignee: BORGWARNER INCPriority: Apr 27, 2010Filed: Apr 20, 2011Published: Feb 21, 2013
Est. expiryApr 27, 2030(~3.7 yrs left)· nominal 20-yr term from priority
Inventors:Udo Dellmann
F01D 25/24F02B 39/00F02B 37/00F01D 9/06F02B 37/16F02B 2037/125F02C 6/12Y02T10/12F01N 1/165
32
PatentIndex Score
0
Cited by
0
References
0
Claims

Abstract

A compressor ( 8 ) of an exhaust-gas turbocharger ( 1 ), having a compressor wheel ( 11 ) which can be driven in a compressor wheel direction of rotation (VR); having a compressor housing ( 10 ) in which the compressor wheel ( 11 ) is arranged, as viewed in the flow direction of the inducted air, between a preferably tubular compressor inlet ( 12 ) and a compressor outlet ( 13 ), and having an overrun air recirculation valve inflow duct ( 14, 15 ) which runs in the compressor housing ( 10 ) from the compressor outlet ( 13 ) to the compressor inlet ( 12 ), wherein the inflow duct ( 14, 15 ) opens into the compressor inlet ( 12 ) substantially in the circumferential direction with respect to the inner diameter (D I ) of said compressor inlet ( 12 ).

Claims

exact text as granted — not AI-modified
1 . A compressor ( 8 ) of an exhaust-gas turbocharger ( 1 ),
 having a compressor wheel ( 11 ) which can be driven in a compressor wheel direction of rotation (VR);   having a compressor housing ( 10 ) in which the compressor wheel ( 11 ) is arranged, as viewed in the flow direction of the inducted air, between a compressor inlet ( 12 ) and a compressor outlet ( 13 ), and   having an overrun air recirculation valve inflow duct ( 14 ,  15 ) which runs in the compressor housing ( 10 ) from the compressor outlet ( 13 ) to the compressor inlet ( 12 ), wherein   the inflow duct ( 14 ,  15 ) opens into the compressor inlet ( 12 ) substantially in the circumferential direction with respect to the inner diameter (D I ) of said compressor inlet ( 12 ).   
     
     
         2 . The compressor as claimed in  claim 1 , wherein the inflow duct ( 15 ) opens into the compressor inlet ( 12 ) in such a way that the inflow of air takes place in the direction of rotation (VR) of the compressor wheel ( 11 ). 
     
     
         3 . The compressor as claimed in  claim 1 , wherein the inflow duct ( 14 ) opens into the compressor inlet ( 12 ) in such a way that the inflow of air takes place counter to the direction of rotation (VR) of the compressor wheel ( 11 ). 
     
     
         4 . The compressor as claimed in  claim 1 , wherein the inflow duct ( 14 ) opens into the compressor inlet ( 12 ) in such a way that the inflow of air has an axial component in the flow direction. 
     
     
         5 . The compressor as claimed in  claim 1 , wherein compressor inlet ( 12 ) is tubular.

Join the waitlist — get patent alerts

Track US2013045082A1 — get alerts on status changes and closely related new filings.

We store only your email — no account needed. See our privacy policy.