Claims
- 1. An exhaust manifold which is made of a steel which exhibits improved formability as well as thermal fatigue resistance properties, the steel composition thereof consisting essentially of, on the basis of weight:
- C: 0.02% or less, Si: 1.0% or less,
- Mn: 0.5% or less, P: 0.04% or less,
- S: 0.005% or less, Cu: 0.1-1.0%,
- Cr: 18.0-25.0%, Mo: 1.0 (exclusive)-3.0%,
- Nb: 0.1-1.0%, Al: 0.20% or less,
- N: 0.02% or less, B: 0-0.01%,
- Fe and incidental impurities: balance
- wherein the content of C and N satisfies the following equation (i) and the content of Cr, Mo and Nb satisfies the following equation (ii):
- C+N.ltoreq.0.03% - - - (i)
- 21%.ltoreq.Cr+Mo+Nb.ltoreq.25% - - - (ii), and
- the steel having thermal fatigue resistance enabling the steel to withstand 700 cycles or more before rupturing at 1000.degree. C., high temperature strength of at least 1.3 kgf/mm.sup.2 at 1000.degree. C., and elongation of at least 30%.
- 2. An exhaust manifold as set forth in claim 1 in which Cr: 19-21%.
- 3. An exhaust manifold as set forth in claim 1 in which Cr: 19-23%.
- 4. An exhaust manifold as set forth in claim 1 in which C+N.ltoreq.0.02%.
- 5. An exhaust manifold as set forth in claim 1 in which Cu: 0.4-0.6%.
- 6. An exhaust manifold as set forth in claim 1 in which Mo: 1.5-2.5%.
- 7. An exhaust manifold which is made of a steel which exhibits improved formability as well as thermal fatigue resistance properties, the steel composition thereof consisting essentially of, on the basis of weight:
- C: 0.02% or less, Si: 1.0% or less,
- Mn: 0.5% or less, P: 0.04% or less,
- S: 0.005% or less, Cu: 0.1-1.0%,
- Cr: 18.0-22.0%, Mo: 1.0 (exclusive)-2.0%,
- Nb: 0.1-1.0%, Al: 0.20% or less,
- N: 0.02% or less, B:0.001 (exclusive)-0.01%,
- Fe and incidental impurities: balance
- wherein the content of C and N satisfies the following equation (i) and the content of Cr, Mo and Nb satisfies the following equation (ii):
- C+N.ltoreq.0.03% - - - (i)
- 21%.ltoreq.Cr+Mo+Nb.ltoreq.25% - - - (ii), and
- the steel having thermal fatigue resistance enabling the steel to withstand 700 cycles or more before rupturing at 1000.degree. C., high temperature strength of at least 1.3 kgf/mm.sup.2 at 1000.degree. C., and elongation of at least 30%.
- 8. An exhaust manifold as set forth in claim 7 in which Cr: 19-21%.
- 9. An exhaust manifold as set forth in claim 7 in which C+N.ltoreq.0.02%.
- 10. An exhaust manifold as set forth in claim 7 in which Cu: 0.4-0.6%.
- 11. An exhaust manifold which is made of a steel which exhibits improved formability as well as thermal fatigue resistance properties, the steel composition thereof consisting essentially of, on the basis of weight:
- C: 0.02% or less, Si: 1.0% or less,
- Mn: 0.5% or less, P: 0.04% or less,
- S: 0.005% or less, Cu: 0.1-1.0%,
- Cr: 19.0-25.0%, Mo: 1.0 (exclusive)-3.0%,
- Nb: 0.1-1.0%, Al: 0.20% or less,
- N: 0.02% or less,
- Fe and incidental impurities: balance
- wherein the content of C and N satisfies the following equation (i) and the content of Cr, Mo and Nb satisfies the following equation (ii):
- C+N.ltoreq.0.03% - - - (i)
- 21%.ltoreq.Cr+Mo+Nb.ltoreq.25% - - - (ii), and
- the steel having thermal fatigue resistance enabling the steel to withstand 700 cycles or more before rupturing at 1000.degree. C., high temperature strength of at least 1.3 kgf/mm.sup.2 at 1000.degree. C., and elongation of at least 30%.
- 12. An exhaust manifold as set forth in claim 11 in which Cr: 19-23%.
- 13. An exhaust manifold as set forth in claim 11 in which C+N.ltoreq.0.02%.
- 14. An exhaust manifold as set forth in claim 11 in which Cu: 0.4-0.6%.
- 15. An exhaust manifold as set forth in claim 11 in which Mo: 1.5-2.5%.
- 16. An exhaust manifold as set forth in claim 1, having a strength of at least 2.2 kgf/mm.sup.2 at 950.degree. C.
- 17. An exhaust manifold as set forth in claim 7, having a strength of at least 2.2 kgf/mm.sup.2 at 950.degree. C.
- 18. An exhaust manifold as set forth in claim 11, having a strength of at least 2.2 kgf/mm.sup.2 at 950.degree. C.
- 19. An exhaust manifold as set forth in claim 1, having a weight gain of no more than 5 mg/cm.sup.2 after heating in air at 950.degree. C. for 100 hours.
- 20. An exhaust manifold as set forth in claim 7, having a weight gain of no more than 5 mg/cm.sup.2 after heating in air at 950.degree. C. for 100 hours.
- 21. An exhaust manifold as set forth in claim 11, having a weight gain of no more than 5 mg/cm.sup.2 after heating in air at 950.degree. C. for 100 hours.
Priority Claims (2)
Number |
Date |
Country |
Kind |
3-336634 |
Dec 1991 |
JPX |
|
3-250850 |
Sep 1992 |
JPX |
|
Parent Case Info
This application is a continuation, of application Ser. No. 08/299,795, filed Sep. 1, 1994 abandoned which is a continuation, of application Ser. No. 07/992,104, filed Dec. 17, 1992 abandoned.
US Referenced Citations (10)
Foreign Referenced Citations (8)
Number |
Date |
Country |
0435003A1 |
Jul 1991 |
EPX |
2158943 |
May 1973 |
FRX |
55-138057 |
Oct 1980 |
JPX |
63-118011 |
May 1988 |
JPX |
64-8254 |
Jan 1989 |
JPX |
3-274245 |
Dec 1991 |
JPX |
2075549A |
Nov 1981 |
GBX |
2084187A |
Apr 1982 |
GBX |
Continuations (2)
|
Number |
Date |
Country |
Parent |
299795 |
Sep 1994 |
|
Parent |
992104 |
Dec 1992 |
|