US2015050126A1PendingUtilityA1
Exhaust-gas turbocharger
Est. expiryMar 1, 2032(~5.6 yrs left)· nominal 20-yr term from priority
Inventors:Michael Loewenberg
F04D 29/054F01D 5/025F05D 2300/174F05D 2230/238F05D 2230/232F05D 2220/40
42
PatentIndex Score
0
Cited by
0
References
0
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-modified1 . 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.Join the waitlist — get patent alerts
Track US2015050126A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.