Exhaust guide member of nozzle vane-type turbocharger
In a turbocharger equipped with a nozzle vane for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, the member to constitute the nozzle vane and to constitute an exhaust guide for guiding exhaust gas to the turbine is characterized in that the exhaust guide member of a nozzle vane-type turbocharge is formed of an austenite stainless steel containing, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N and containing these ingredients in such a manner that they satisfy a DE value of the specified formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities.
1. An exhaust guide member of a nozzle vane-type turbocharger equipped with at least a nozzle vane and drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
2. The exhaust guide member of a nozzle vane-type turbocharger according to claim 1 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
3. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of Nb and Ti in an amount of from 0.05 to 1.0% by mass in total and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
4. The exhaust guide member of a nozzle vane-type turbocharger according to claim 3 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
5. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of Mo and Cu in an amount of from 0.50 to 5.0% by mass in total and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
6. The exhaust guide member of a nozzle vane-type turbocharger according to claim 5 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
7. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of REM (rare earth element including Y) and Ca in an amount of from 0.01 to 0.20% by mass in total and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
8. The exhaust guide member of a nozzle vane-type turbocharger according to claim 7 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
9. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of Nb and Ti in an amount of from 0.05 to 1.0% by mass in total, one or two of Mo and Cu in an amount of from 0.50 to 5.0% by mass in total and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
10. The exhaust guide member of a nozzle vane-type turbocharger according to claim 9 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
11. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of Nb and Ti in an amount of from 0.05 to 1.0% by mass in total, one or two of REM (rare earth element including Y) and Ca in an amount of from 0.01 to 0.20% by mass in total and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
12. The exhaust guide member of a nozzle vane-type turbocharger according to claim 11 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
13. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of Mo and Cu in an amount of from 0.50 to 5.0% by mass in total, one or two of REM (rare earth element including Y) and Ca in an amount of from 0.01 to 0.20% by mass in total and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
14. The exhaust guide member of a nozzle vane-type turbocharger according to claim 13 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.
15. An exhaust guide member of a nozzle vane-type turbocharger equipped with a nozzle vane and a drive ring for changing the speed of exhaust gas running through a turbine in accordance with the speed of engine revolution, wherein the member to constitute the nozzle vane and the drive ring and to constitute an exhaust guide for guiding exhaust gas to the turbine is formed of an austenite stainless steel consisting of, in terms of % by mass, at most 0.08% of C, from 2.0 to 4.0% of Si, at most 2.0% of Mn, from 8.0 to 16.0% of Ni, from 18.0 to 20.0% of Cr and at most 0.04% of N, one or two of Nb and Ti in an amount of from 0.05 to 1.0% by mass in total, one or two of Mo and Cu in an amount of from 0.50 to 5.0% by mass in total, one or two of REM (rare earth element including Y) and Ca in an amount of from 0.01 to 0.20% by mass in total, and containing these ingredients in such a manner that they satisfy a DE value of the following formula to be from 5.0 to 12.0, with a balance of Fe and inevitable impurities:
DE value=Cr+1.5Si+0.5Nb+Mo—Ni−0.3Cu−0.5Mn−30(C+N).
16. The exhaust guide member of a nozzle vane-type turbocharger according to claim 15 , wherein the exhaust guide member comprises the drive ring, a drive lever, a nozzle ring, and the vane and a shaft of the nozzle vane.