Structural component including a tempered transition zone

Abstract

The invention provides a hot stamped structural component (20) for an automotive vehicle, such as a B-pillar, including a first part (22) formed of a high strength steel material joined to a second part (24) formed of a high ductility steel material. The structural component (20) also includes a locally tempered transition zone (26) along the joint (28) to reduce the potential for failure along the joint (28). The transition zone (26) has strength and ductility levels between the strength and ductility levels of the remaining portions of the first and second parts (22, 24). The tempering step can be incorporated into a laser trimming cell or assembly cell, and thus the transition zone (26) can be created without adding an additional process step or increasing cycle time.

Claims

1. A structural component, comprising: a first part formed of a first steel material having a first ductility; a second part formed of a second steel material having a second ductility being greater than said first ductility; said first part being welded directly to said second part to present a joint therebetween; and a transition zone disposed adjacent said welded joint, said transition zone consisting of a portion of said first part adjacent said joint and/or a portion of said second part adjacent said welded joint, and said transition zone having a third ductility between said first ductility and said second ductility.

2. The structural component of claim 1, wherein said first steel material has a first strength, said second steel material has a second strength being less than said first strength, and said transition zone has a third strength between said first strength and said second strength.

3. The structural component of claim 1, wherein said third strength of said transition zone includes an ultimate tensile strength (UTS) from 700 MPa to 1,400 MPa and a yield strength (YS) from 470 MPa to 1,000 MPa.

4. The structural component of claim 1, wherein said transition zone includes a mixture of ferrite and martensite, said first part includes more martensite than said transition zone, and said second part includes less martensite than said transition zone.

5. The structural component of claim 1, wherein the transition zone consists of a portion of said first part adjacent said welded joint and a portion of said second part adjacent said welded joint.

6. The structural component of claim 1, wherein said third ductility varies along said transition zone.

7. The structural component of claim 1, wherein said first part has a first volume and said second part has a second volume; at least 50% of said first volume has said first ductility being less than said third ductility; and at least 50% of said second volume has said second ductility being greater than said third ductility.

8. The structural component of claim 1, wherein said third ductility of said transition zone is provided by an elongation (e.sub.f) of at least 6%.

9. The structural component of claim 1, wherein said first part is laser welded to said second part to form said welded joint and said transition zone is tempered.

10. The structural component of claim 1, wherein said steel material of said first part includes carbon in an amount not greater than 0.25 weight percent (wt. %), manganese in an amount not greater than 1.4 wt. %, silicon in an amount not greater than 0.35 wt. %, chromium in an amount not greater than 0.3 wt. %, boron in an amount not greater than 0.005 wt. %, and a balance of iron, based on the total weight of said steel material.

11. The structural component of claim 1, wherein said structural component is a B-pillar for an automotive vehicle, said B-pillar extends longitudinally from a first end to a second end, said first part extends from said first end to said joint, and said second part extends from said joint to said second end.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other advantages of the present invention will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:

(2) FIG. 1 illustrates an exemplary hot stamped structural component including a first part formed of a high strength material welded to a second part formed of a high ductility material and including a transition zone adjacent the welded joint; and

(3) FIG. 2 illustrates a first blank welded to a second blank which are used to form the structural component of FIG. 1.

DESCRIPTION OF THE ENABLING EMBODIMENT

(4) The invention provides a hot formed structural component 20, such as a B-pillar for an automotive vehicle, including a first part 22 having a high strength joined to a second part 24 having a high ductility, and a method of manufacturing the structural component 20, as shown in FIG. 1. A locally tempered transition zone 26 extends along a region of the structural component 20 adjacent the joint 28. The transition zone 26 typically comprises a portion of the first part 22 adjacent the joint 28, for example less than 50% of the volume of the first part 22. The transition zone 26 can also comprise a portion of the second part 24 adjacent the joint 28, for example less than 50% of the volume of the second part 24. The transition zone 26 has a ductility level between the ductility levels of the adjacent portions of the first part 22 and the second part 24. The transition zone 26 can also have a strength different from the strength of the adjacent portions of the first part 22 and the second part 24. In an exemplary embodiment, the structural component 20 is efficiently manufactured by hot stamping sheet steel blanks, for example Usibor and Ductibor blanks 30, 32, which are shown in FIG. 2, and then tempering a portion of the hot stamped parts 22, 24 adjacent the joint 28 to provide the transition zone 26, as shown in FIG. 1. The transition zone 26 provides controlled tempered properties in an automotive vehicle component. For example, the ductility of the transition zone 26 assists in energy absorption during impact and reduces the potential for fracture or separation along the joint 28.

(5) The first blank 30 used to form the high strength first part 22 of the structural component 20 comprises a steel material, referred to as the first steel material. Various different steel alloys can be used, however, in the exemplary embodiment, the first blank 30 comprises a coated, press hardened steel alloy, such as Usibor 1500P. This steel alloy includes carbon in an amount not greater than 0.25 weight percent (wt. %), manganese in an amount not greater than 1.4 wt. %, silicon in an amount not greater than 0.35 wt. %, chromium in an amount not greater than 0.3 wt. %, boron in an amount not greater than 0.005 wt. %, and a balance of iron. Prior to hot forming, the first blank 30 of the exemplary embodiment has a microstructure comprising ferrite and perlite. The first blank 30 also has an ultimate tensile strength (UTS) ranging from 500 MPa to 700 MPa; a yield strength (YS) ranging from 350 MPa to 550 MPa; and an elongation (e.sub.f) of at least 10% (L.sub.0=80 mm and th<3 mm).

(6) The geometry of the first blank 30 can vary depending on the type of structural component 20 to be formed. Typically, the first blank 30 includes a first end 34 extending longitudinally to a second end 36. In the exemplary embodiment, the first blank 30 is designed for use as a B-pillar of an automotive vehicle and thus includes a foot portion at the first end 34 and a longitudinal section extending from the foot portion to the second end 36, as shown in FIG. 2. However, the geometry of the first blank 30 could alternatively be designed to provide another type of pillar, rail, beam, reinforcement, ring, frame, or body component for an automotive vehicle. The first blank 30 could also be designed for non-automotive applications. The thickness of the first blank 30 can be uniform or vary along its length. The thickness typically ranges from 1 mm to 2 mm for automotive applications, and in the exemplary embodiment, the thickness of the first blank 30 is about 1.5 mm.

(7) The first blank 30 is preferably coated to prevent corrosion, increase heating rate, and prevent cracks in the steel material during the hot forming process. In the exemplary embodiment, the coating includes aluminum in an amount of 90 wt. % and silicon in an amount of 10 wt. %. However, other types of coatings could be used, such as a zinc coating. The coating typically has an average thickness of 25 m when applied to the first blank 30 having a thickness ranging from 1 mm to 2 mm.

(8) The second blank 32 used to form the high ductility second part 24 of the structural component 20 is also formed of a steel material, referred to as the second steel material. The second steel material can also comprise various different types of steel material. In the exemplary embodiment, the second blank 32 comprises a non-coated, press hardened steel alloy, such as Ductibor500P.

(9) The geometry of the second blank 32 can vary depending on the type of structural component 20 to be formed. However, the second blank 32 typically includes a first end 35 extending longitudinally to a second end 37. In the exemplary embodiment, wherein the second blank 32 is designed for use in a B-pillar, the second blank 32 includes a longitudinal section extending from the first end 35 to the second end 37, with a foot portion at the second end 37, as shown in FIG. 2. In this embodiment, the width of the first end 35 of the second part 24 is approximately equal to the width of the second end 36 of the first part 22. Alternatively, the geometry of the second blank 32 could be designed to provide another type of pillar, rail, beam, reinforcement, ring, frame, or body component for an automotive vehicle. The second blank 32 could also be designed for non-automotive applications. The thickness of the second blank 32 can be uniform or vary along its length. However, the thickness typically ranges from 1 mm to 2 mm for automotive applications. In the exemplary embodiment, the second blank 32 has a thickness of 1.5 mm.

(10) The method of manufacturing the structural component 20 typically includes joining the first blank 30 to the second blank 32 to form the joint 28. In the exemplary embodiment, the second end 36 of the first blank 30 is laser welded to the first end 35 of the second blank 32 to form the joint 28 (i.e., weld), as shown in FIG. 2. However, various other types of joining techniques could be used, such as resistance spot welding, arc welding, metal inert gas (MIG) welding, metal active gas (MAG) welding, and brazing.

(11) Once the first blank 30 and the second blank 32 are joined together, the blanks 30, 32 are hot formed to provide the structural component 20 with a desired shape. Various different hot forming processes could be used. In the exemplary embodiment, the hot forming process includes hot stamping the first blank 30 and the second blank 32 after the blanks 30, 32 are joined together. The exemplary hot stamping process first includes heating the welded blanks 30, 32 in a furnace to a temperature of 900 C. to 950 C. for 5 to 10 minutes. During this step, the steel material of the first and second blanks 30, 32 transforms to an austenitic microstructure. Next, the exemplary process includes transferring the heated blanks 30, 32 to a forming die, wherein the transfer time from the furnace to the forming die is preferably less than 7 seconds. The method next includes stamping the heated blanks 30, 32 in the die while the blanks 30, 32 are still at a temperature of 600 C. to 800 C. The die forms the heated blanks 30, 32 into the first and second parts 22, 24 having a predetermined shape. After the stamping step, but while the die is still closed and the parts 22, 24 are still in the die, the exemplary method includes quenching the first part 22 at a speed greater than 50 C. per second and the second part 24 at a speed greater than 30 C. per second. The quenching step could alternatively include water quenching at greater speeds. During the quenching step, the microstructure of the first part 22 transforms from austenite to martensite, and the microstructure of the second part 24 transforms from austenite to a mixture of ferrite and martensite. As stated above, this hot stamping process is provided only as an example, and various other hot stamping or hot forming processes could be used.

(12) After the hot forming process, the strength of the first part 22 is still greater than the strength of the second part 24, and the ductility of the second part 24 is still greater than the ductility of the first part 22. At this point during the process, the strength and ductility are typically uniform throughout the first part 22 and uniform throughout the second part 24. In the exemplary embodiment, wherein the first part 22 is formed from Usibor1500P, the first part 22 has an ultimate tensile strength (UTS) ranging from 1,400 MPa to 1,600 MPa; a yield strength (YS) ranging from 1,000 MPa to 1,200 MPa; an elongation (e.sub.f) of at least 5 to 6% (L.sub.0=80 mm and th<3 mm); and a hardness less than 490. The second part 24 of the exemplary embodiment, which is formed from Ductibor500P, has an ultimate tensile strength (UTS) ranging from 550 MPa to 700 MPa; a yield strength (YS) ranging from 370 MPa to 470 MPa; and an elongation (e.sub.f) of at least 17% (L.sub.0=80 mm and th<3 mm). However, the properties of the first part 22 and the second part 24 can vary from this example.

(13) The method of manufacturing the structural component 20 further includes heating at least one region of the first part 22 and/or at least one region of the second part 24 along and adjacent the joint to form the transition zone 26. For example, the transition zone 26 can be located in the first part 22 alone, the second part 24 alone, or in a portion of both the first part 22 and the second part 24. This heating step is conducted outside the forming die after the hot stamping step, and it is preferably conducted in a laser trimming cell or assembly cell. Alternatively, the heating step can be provided as a secondary process. The heating step used to form the transition zone 26 can include tempering, annealing, or any other type of heat treatment. The transition zone 26 introduced into the structural component 20 has a ductility level between the ductility levels of the adjacent portions of the first part 22 and the second part 24 to absorb energy during a crash. The transition zone 26 can also have a strength level between or different from the strength levels of the adjacent portions of the first part 22 and the second part 24. The ductility of the transition zone 26 can be determined by the elongation (e.sub.f), and the strength of the transition zone 26 can be determined by the ultimate tensile strength (UTS) or yield strength (YS). The time and temperature of the heating step will vary depending on the steel material and thickness of the blanks 30, 32. In addition, the time and temperature can be adjusted to meet the desired tempered properties for each particular application.

(14) In the exemplary embodiment, the step of introducing the transition zone 26 includes locally tempering a portion of the first part 22 and locally tempering a portion of the second part 24 adjacent the laser weld joint 28. The tempered portion of the first part 22 is located adjacent the second end 36 of the first part 22, and the tempered portion of the second part 24 is located adjacent the first end 35 of the second part 24, as shown in FIG. 1. This tempering step is conducted after the blanks 30, 32 are hot stamped, using an induction heating system incorporated into the laser trimming cell or the assembly cell. The induction heating system includes at least one heating coil which heats a portion of the structural component 20 along and adjacent the laser weld joint 28 to a certain temperature. A form control mechanism can also be used to control the geometry of the transition zone 26 during the heating step. In addition, a monitoring or thermal imaging system for controlling the temperature of the transition zone 26 during the heating step is provided. However, another technique or other equipment could be used to heat the structural component 20 adjacent the joint 28 and form the transition zone 26, for example, by a laser.

(15) After the tempering step, the ductility of the transition zone 26 is greater than the ductility of the first part 22 outside of the transition zone 26 and less than the ductility of the second part 24 outside of the transition zone 26. The strength of the transition zone 26 can also be different from the strength of the first part 22 and the second part 24 outside of the transition zone 26. For example, the strength of the transition zone 26 could be greater than the strength of the second part 24 outside of the transition zone 26 and less than the strength of the first part 22 outside of the transition zone 26. The strength and ductility can be constant or can vary along the length of the first part 22 and the second part 24. The strength and ductility of the transition zone 26 can also be constant or vary continuously along the length of the transition zone 26. For example, the strength of the transition zone 26 can decrease continuously in a direction moving from the first part 22 to the second part 24, and the ductility can increase continuously in a direction moving from the first part 22 to the second part 24.

(16) The method of the present invention requires tempering or heating only the transition zone 26, which is small relative to the tempered regions of comparative hot stamped components, and therefore less capital investment is required. The dimensions of the transition zone 26 can also vary. In one embodiment, at least 50% of the volume of the first part 22 has the first ductility and at least 50% of the volume of the second part 24 has the second ductility. Typically, the transition zone 26 typically comprises a minority of the volume of the first part 22 and/or a minority of the volume of the second part 24.

(17) The area of the transition zone 26 can also be easily adjusted. For example, the area can be adjusted by simply changing the induction coil of the heating system, rather than making major die modifications as in the tempering methods of the prior art. The thickness of the transition zone 26 can also vary, but typically the thickness of the transition zone 26 is approximately equal to the thickness of the adjacent portions of the first and second parts 22, 24.

(18) In the exemplary embodiment, the microstructure of the transition zone 26 includes a mixture of ferrite and martensite. The portion of the transition zone 26 located in the first part 22 includes more martensite than the portion of the transition zone 26 located in the second part 24. Thus, the strength of the transition zone 26 decreases continuously along its length and the ductility increases continuously along its length, moving from the first part 22 to the second part 24. In the exemplary embodiment, when the Usibor and Ductibor blanks 30, 32 are used, the ultimate tensile strength (UTS) of the transition zone 26 could range from 700 MPa to 1,400 MPa; the yield strength (YS) could range from 470 MPa to 1,000 MPa; and the elongation (e.sub.f) could range from at least 6% to at least 17% (L.sub.0=80 mm and th<3 mm). However, the transition zone 26 introduced can have other properties, depending on the particular material and heating step employed.

(19) Many modifications and variations of the present invention are possible in light of the above teachings and may be practiced otherwise than as specifically described while within the scope of the following claims.