Method of manufacturing fuel rail for gasoline direct injection
11015231 · 2021-05-25
Assignee
Inventors
Cpc classification
F02M55/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B23K1/0008
PERFORMING OPERATIONS; TRANSPORTING
F02M2200/9053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22C38/002
CHEMISTRY; METALLURGY
C22C38/12
CHEMISTRY; METALLURGY
F02M55/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B23K1/00
PERFORMING OPERATIONS; TRANSPORTING
F02M55/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M55/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22C38/12
CHEMISTRY; METALLURGY
Abstract
To obtain, at low cost, a fuel rail that maintains low hardness and good formability before being formed into a tube stock, can be made to form a welded pipe, and has high-strength properties with which the fuel rail can withstand a high fuel pressure even when formed so as to be relatively thin. A fuel rail for gasoline direct injection that is used at a fuel pressure of at least 30 MPa and is formed from an iron-alloy welded pipe. The fuel rail comprises an iron alloy that contains chemical components of C, Si, Mn, P, S, Nb, and Mo. The plate thickness t and the outer diameter D of the fuel rail have a ratio t/D of 0.2 or less. A bainitic structure can be precipitated by brazing the fuel rail in a furnace during manufacturing.
Claims
1. A method of manufacturing fuel rail for gasoline direct injection at a fuel pressure of at least 30 MPa, the method comprising: a step of forming a welded pipe from an iron alloy that contains chemical components of C, Si, Mn, P, S, Nb, and Mo, wherein the plate thickness t and the outer diameter D of the welded pipe have a ratio t/D of 0.2 or less, and a step of copper-brazing the welded pipe at a temperature of 1000° C. or more in a furnace so that a bainitic structure is precipitated.
Description
MODES FOR CARRYING OUT THE INVENTION
(1) A fuel rail for gasoline direct injection of the Examples of this invention is described below. First, among the iron alloy materials constituting this example, the chemical components excluding iron and impurities and the compounding ratio to all the components are shown in Table 1 below.
(2) TABLE-US-00001 TABLE 1 C(%) Si(%) Mn(%) P(%) S(%) Nb(%) Mo(%) Ni(%) Cr(%) Example 1 0.20 0.21 1.63 0.010 0.002 0.026 0.38 — — Example 2 0.18 0.20 1.25 0.015 0.002 0.025 0.25 — — Comparative 0.02 0.33 1.33 0.036 0.022 — — 9.89 18.35 Example 1
(3) Examples 1 and 2 of the invention include C, Si, Mn, P, S, Nb, and Mo, as shown above. The production method of Examples 1 and 2 is as follows. Examples 1 and 2 are iron alloys comprising the chemical components shown in Table 1 above, in addition to iron and the other impurities. This material was then formed into a welded pipe with its both ends closed by parts, and sockets and fixtures were installed in the pipe, respectively. Next, the completed assembly is subjected to copper-brazing in a furnace at temperature of 1000° C. or more, annealed, and then, shipped as a product after passing through the process of die matching, leak checking, or the like.
(4) The fuel rails of Examples 1 and 2 were copper-brazed in a furnace as mentioned above, and during this copper brazing process, the temperature in a furnace raised to 1000° C. or more, and after that, cooled down slowly. Physical properties of the iron alloy of Examples 1 and 2 made of the materials as described above change due to the copper-brazing in the furnace. In order to examine changes in physical properties before and after the copper-brazing in the furnace, physical property testing was conducted based on the JIS standard.
(5) Specifically, JIS5 test pieces (test piece thickness 1.6 mm, formed width 25 mm, and formed length 350 mm) of the materials of Examples 1 and 2 were formed at first and then tensile testing and structure observation were conducted by using these test pieces. The results of the tensile testing and structure observations are shown in Table 2 below. Note that, “Before” and “After” mean the state before the tube stock being formed, and the state after the tube stock being copper-brazed in a furnace, respectively.
(6) TABLE-US-00002 TABLE 2 Tensile Strength 0.2 Prof Stress Extension Coefficient Hardness (MPa) (MPa) (%) (HV) Structure Examples Before After Before After Before After Before After Before After 1 675 722 434 499 23.2 23.4 225 238 Ferrite Bainite Ferrite- Pearlit 2 568 628 361 434 26.6 16.0 190 211 Ferrite Bainite Ferrite- Pearlit
(7) As shown in Table 2, the values of tensile strength, 0.2% proof stress, and hardness after the copper-brazing in the furnace were larger than those values before being formed into the tube stock. Precipitation of bainite occurred in both Example 1 and Example 2 after copper-brazing in a furnace, according to structure observation of the tube. By contrast, the structure before being formed into a tube stock was either Ferrite or Ferrite-Pearlite only, and no bainite structure was found.
(8) It was confirmed from this result that the fuel rail of Examples 1 and 2 containing chemical components of C, Si, Mn, P, S, Nb, and Mo formed a bainite structure due to the process of copper-brazing in the furnace, and high strength and high hardness properties could be obtained compared with the state before being formed into a tube stock. Further, it was confirmed that as the state before being formed into a tube stock had the same ferrite or ferrite-pearlite structure as the conventional one have, and the quality of welding can be satisfactorily maintained and the material was superior in good formability.
(9) In addition, tensile testing and structure observation were conducted based on the JIS standard, about the materials used in Example 1 and 2, and the materials used in conventional fuel rails, for confirming the difference in the materials' physical properties between those of Examples 1 and 2 and the conventional fuel rail containing different chemical components compared to Examples 1 and 2. Among the iron alloy materials constituting Comparative Example 1, the chemical components excluding iron and impurities and the compounding ratio to all the components are shown in Table 1 below. As shown in Table 1, Comparative Example 1 does not include Nb and Mo, and its chemical components are different from that of Examples 1 and 2, and also include Ni and Cr which are not included in the materials of Examples 1 and 2. Note that, JIS5 test pieces (test piece thickness 1.6 mm, formed width 25 mm, and formed length 350 mm) are used in Comparative Example 1, just like Examples 1 and 2. The results are shown in Table 3 below.
(10) TABLE-US-00003 TABLE 3 Tensile Strength (MPa) Hardness (HV) Structure Example 1 722 238 Bainite Example 2 628 211 Bainite Comparative Example 1 520 150 Austenite
(11) As it turned out, Examples 1 and 2 exhibit higher values with regard to both tensile strength and hardness compared to Comparative Example 1. Also, when the structure observations were conducted, Examples 1 and 2 precipitated a bainitic structure while Comparative Example 1 exhibits an austenite structure, showing no precipitation of a bainitic structure. Thus, higher strength and higher hardness of Examples 1 and 2 were confirmed in comparison with the conventional materials.
(12) Further, as an example, the fuel rail made of a material of Examples 1 and 2 mentioned above can be formed into a product having the sizes shown in Table 4. Note that, D and t in Table 4 means outside diameters and thicknesses of the fuel rail, respectively. And a in Table 4 is mainly used under fuel pressure around 30 MPa, and when formed from the materials of Examples 1 and 2, its outer diameter D is 11 mm, the wall thickness t is 2.0 mm and it can be formed to be thin with t/D of 0.2 or less. On the other hand, in the case of a conventional product formed from the material of Comparative Example 1, since the outer diameter must be 15 mm and the wall thickness 4.0 mm in order to be usable under the fuel pressure around 30 MPa, t/D is higher than 0.2 and must be formed to be much thicker than that formed by the materials of Examples 1 and 2.
(13) In addition, b in Table 4 is mainly used under the fuel pressure of around 80 MPa, and when formed from the materials of Examples 1 and 2, its outer diameter is 13 mm and its wall thickness is 2.3 mm, T/D can be formed to be as thin as 0.2 or less. In contrast, in the case of using the material of Comparative Example 1, since the outer diameter is 20 mm and the wall thickness is 5.8 mm in order to be used under the fuel pressure around 80 MPa, t/D is higher than 0.2, In this case as well, it must be formed to be much thicker than that formed by the materials of Examples 1 and 2.
(14) TABLE-US-00004 TABLE 4 Examples 1 and 2 Comparative Example 1 a D = 11 mm, t = 2.0 mm t/D = 0.18 D = 15 m, t/D = 0.27 t = 4.0 mm b D = 13 mm, t = 2.3 mm t/D = 0.18 D = 20 mm, t/D = 0.29 t = 5.8 mm
(15) From the above results, it can be seen that a fuel rail made of a material of Examples 1 and 2 can be formed to have a thin wall and to be light-weighted compared with a conventional material, and it can be made to form a welded pipe by roll forming, gaining high strength and high pressure resistance. Thus, it is possible to obtain a product at a low price and in an easy manner that can cope with high a fuel pressure of 30 MPa˜80 MPa.