FRONT STRUCTURE FOR AN ELECTRIC VEHICLE
20220315111 · 2022-10-06
Inventors
- Alexandre SOTTY (Compiegne, FR)
- Nicolas SCHNEIDER (Saint Martin Longueau, FR)
- Yves Drouadaine (Pontoise, FR)
- Elie GIBEAU (Pont-Sainte-Maxence, FR)
Cpc classification
B62D25/2018
PERFORMING OPERATIONS; TRANSPORTING
B62D21/15
PERFORMING OPERATIONS; TRANSPORTING
B60K1/04
PERFORMING OPERATIONS; TRANSPORTING
B62D25/2045
PERFORMING OPERATIONS; TRANSPORTING
B62D25/14
PERFORMING OPERATIONS; TRANSPORTING
International classification
B62D21/15
PERFORMING OPERATIONS; TRANSPORTING
B60K1/04
PERFORMING OPERATIONS; TRANSPORTING
B62D25/14
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Front structure for an electric vehicle including a lower dash panel, a seat cross-member and a tunnel nose, such that the tunnel nose is designed to absorb energy in its front portion while resisting intrusion in its rear portion, optimizing the energy absorption in the part during a front crash and protecting the battery pack from being breached by the downward pushing effect of the lower dash panel.
Claims
1-11. (canceled)
12: A front structure for an electric vehicle, the front structure comprising: a lower dash panel separating a passenger cabin and a front engine compartment, a seat cross-member extending in a transverse direction and being attached at either ends to a lateral reinforcement structure; and a tunnel nose including: a front portion at least attached to the lower dash panel, and a rear portion at least attached to the seat cross-member; wherein a product of the ultimate tensile strength by an average thickness of the rear portion is greater than or equal to a further product of the ultimate tensile strength by the average thickness of the front portion and wherein the front portion is made from a material having a fracture strain of at least 0.6 and a critical bending angle of at least 75°.
13: The front structure as recited in claim 12 wherein the material from which the tunnel nose is manufactured has at least an ultimate tensile strength of 700 MPa.
14: The front structure as recited in claim 12 wherein the front portion has at least one geometrical alteration locally altering a cross section.
15: The front structure as recited in claim 12 wherein at least part of the tunnel nose is made by hot stamping a material having a tensile strength of at least 1000 MPa after hot stamping.
16: The front structure as recited in claim 15 wherein the material is a press-hardened steel having a composition comprising in % weight: −0.20%≤C≤0.25%, 1.1%≤Mn≤1.4%, 0.15%≤Si≤0.35%, ≤Cr≤0.30%, 0.020%≤Ti≤0.060%, 0.020%≤Al≤0.060%, S≤0.005%, P≤0.025%, 0.002%≤B≤0.004%, a remainder being iron and unavoidable impurities resulting from the elaboration.
17: The front structure as recited in claim 12 wherein at least part of the tunnel nose is made by cold stamping a material having a tensile strength of at least 950 MPa.
18: The front structure as recited in claim 17 wherein a chemical composition of the material of the at least part of the tunnel nose comprises in weight %: 0.13%<C<0.25%, 2.0%<Mn<3.0%, 1.2%<Si<2.5%, 0.02%<Al<1.0%, with 1.22%<Si+Al<2.5%, Nb<0.05%, Cr<0.5%, Mo<0.5%, Ti<0.05%, a remainder being Fe and unavoidable impurities, the at least part of the tunnel nose having a microstructure comprising between 8% and 15% of retained austenite, a microstructure remainder being ferrite, martensite and bainite, wherein a sum of martensite and bainite fractions is between 70% and 92%.
19: The front structure as recited in claim 17 wherein a chemical composition of the material of the at least part of the tunnel nose comprises in weight %: 0.15%<C<0.25%, 1.4%<Mn<2.6%, 0.6%<Si<1.5%, 0.02%<Al<1.0%, with 1.0%<Si+Al<2.4%, Nb<0.05%, Cr<0.5%, Mo<0.5%, a remainder being Fe and unavoidable impurities, the at least part of the tunnel nose having a microstructure comprising between 10% and 20% of retained austenite, the remainder being ferrite, martensite and bainite.
20: The front structure as recited in claim 12 wherein the tunnel nose is formed by stamping a tailor welded blank.
21: The front structure as recited in claim 12 wherein the tunnel nose is formed by stamping a tailor rolled blank.
22: A method to produce the front structure as recited in claim 12 comprising the steps of: providing a blank; stamping the blank into the shape of the tunnel nose; attaching the tunnel nose to the lower dash panel; and attaching the tunnel nose to the seat cross-member.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0030] Other aspects and advantages of the invention will appear upon reading the following description, given by way of example, and made in reference to the appended drawings, wherein:
[0031]
[0032]
[0033]
[0034]
DETAILED DESCRIPTION
[0035] In the following description, the terms “upper”, “lower”, “front”, “rear”, “transverse” and “longitudinal” are defined according to the usual directions of a mounted vehicle. More particularly, the terms “upper” and “lower”, are defined according to the elevation direction of the vehicle, the terms “front”, “rear” and “longitudinal” are defined according to the front/rear direction of the vehicle and the term “transverse” is defined according to the width of the vehicle. By “substantially parallel” or “substantially perpendicular” it is meant a direction which can deviate from the parallel or perpendicular direction by no more than 15°.
[0036] More particularly, the term “fracture strain” and “critical bending angle” refer to the fracture strain criterion and the critical bending angle criterion defined by Pascal Dietsch et al. in “Methodology to assess fracture during crash simulation: fracture strain criteria and their calibration”, in Metallurgical Research Technology Volume 114, Number 6, 2017. The critical bending angle defines the angle at which the first cracks are detected on the extrados of a sample which has been deformed according to the standardized VDA-238-100 Standard. The fracture strain is the associated equivalent strain within the material at the point of the deformation when the critical bending angle has been reached.
[0037] The yield strength, the ultimate tensile strength and the uniform and total elongation are measured according to ISO standard ISO 6892-1, published in October 2009.
[0038] The average thickness of a part or a portion of a part is the thickness of the corresponding area of the sheet which is used to produce said part.
[0039] The term “controlled buckling” refers to the mode of deformation of a part subjected to a compressive load, where the part progressively absorbs the mechanical energy of the compressive load by forming a series of successive waves resulting from successive local buckling deformations of the part. As a result, the length of the part as measured in the direction of the compressive load is smaller after the deformation than the initial length of the part in said direction. In other words, when a part reacts to a compressive load by controlled buckling, it folds onto itself in the same way as a plastic bottle on which a compressive load is applied between the top and the bottom of the bottle.
[0040] Referring to
[0044] The front structure 1 is connected to the lateral reinforcement structure 17 on either side of the vehicle. The lateral reinforcement structure 17, comprises for example the following elements: a side sill 8 running longitudinally along the bottom of the body of the vehicle, a front pillar or A pillar 10 located at the front of the front door with a lower part connected to the side sill 8 and an upper part going up to the roof of the vehicle, a center pillar or B pillar 12, located between the front and back doors and a rear pillar or C pillar 14, located behind the back door.
[0045] The lower dash panel 3 is a large panel closing the passenger cabin 5 at its lower front end. It is connected to the lateral reinforcement structure 17 on its sides and to the front end of the floor panel 4 at its bottom end. It generally features several apertures 6 intended for the steering column or pedals for the driver. Its main function is to separate the passenger cabin 5 from the engine compartment 7 and as such does not have a major structural role in case of a front crash. It is generally made of a soft material, able to be deformed in the complex shape that the vehicle designer will require of this part and with a low average thickness, so as not to penalize the overall weight of the vehicle. For example, the lower dash panel 3 is made of steel designed for deep drawing having an average thickness comprised between 0.5 mm and 0.9 mm and an ultimate tensile strength below 350 MPa.
[0046] The lower dash panel 3 is generally slanted compared to a vertical plane, the bottom part of the lower dash panel 3 being further back than the top part of the lower dash panel 3. This is due to the general shape of the engine compartment 7 and to the need for mechanical elements of the chassis in the lower front part of the vehicle.
[0047] The seat cross member 9 is a structural part designed to reinforce the overall rigidity of the vehicle and to provide support for the lateral reinforcement structure 17. In a particular embodiment, depicted in
[0048] In a particular embodiment, the seat cross member 9 is attached to the floor panel 4. For example, the seat cross member 9 is attached by welding it on top of the floor panel 4 as depicted in
[0049] In the event of a lateral collision, the seat cross member 9 acts as an anti-intrusion part, protecting the driver and passenger from intrusion of the impactor. As such, it is usually manufactured using very high strength steel, which does not need to exhibit a high ductility when mounted on the vehicle, because it is not expected to absorb energy by deforming under the effect of the impact, but rather it is expected to keep its shape and length as much as possible. For example, the seat cross member is made of a material having an ultimate tensile strength higher than 1800 MPa and having a material average thickness before forming comprised between 1.3 mm and 2.0 mm.
[0050] The seat cross member 9 is attached to the lateral reinforcement structure 17 on either side of the vehicle. For example, the seat cross member 9 is attached to the lateral reinforcement structure 17 by spot welding. For example, the seat cross member 9 is attached to the lateral reinforcement structure 17 by welding it onto the side sill 8.
[0051] Referring to
[0052] The tunnel nose 15 is designed in such a way that the product of the ultimate tensile strength by the average thickness of the rear portion 23 is greater than or equal to the product of the ultimate tensile strength by the average thickness of the front portion 21. This product is a reflection of the deformability under loading. Because it is greater or equal on the rear portion 23 than on the front portion 21, when the part is submitted to a load, for example a compressive loading applied on both ends, the front portion 21 will have a tendency to deform before the rear portion 23. The tunnel nose 15 is also designed such that the front portion 21 is made from a material having a fracture strain of at least 0.6 and a critical bending angle of at least 75°. This allows the front portion 21 to deform without breaking during a front crash, as will be further detailed below.
[0053] In a particular embodiment, the tunnel nose 15 is further attached to the floor panel 4 on part of the front portion 21 and/or the rear portion 23. For example, the tunnel nose 15 is attached by spot welding the flange 25 to the floor panel 4.
[0054] In the event of a front collision, for example simulated by the standardized crash test FMVSS 208 described previously, the impact force will first have the effect of compressing the engine compartment 7, as depicted in
[0055] Furthermore, by folding onto itself, the front portion 21 prevents the rear portion 23 from moving under the effect of the transmitted impact force F, which prevents the rear portion 23 from breaching into the battery pack 2, located beneath the tunnel nose 15.
[0056] In a particular embodiment, depicted in
[0057] In a particular embodiment, depicted in
[0058] In a particular embodiment, the material from which the tunnel nose 15 is made has an ultimate tensile strength of at least 700 MPa. Advantageously, this guarantees a structural stability to the tunnel nose 15 and also ensures that the tunnel nose 15 will absorb an important amount of energy when deforming during a collision.
[0059] In a particular embodiment, at least part of the tunnel nose 15 is made by hot stamping a material having a tensile strength of at least 1000 MPa after hot stamping. Advantageously, the use of hot stamping technology enables to produce complex shapes with high resistance and no springback issues after forming. Furthermore, using high strength material with more than 1000 MPa mechanical resistance on the final part ensures a high energy absorption during a collision.
[0060] For example, the above mentioned press-hardened steel comprises in % weight: 0.20%≤C≤0.25%, 1.1%≤Mn≤1.4%, 0.15%≤Si≤0.35%, ≤Cr≤0.30%, 0.020%≤Ti≤0.060%, 0.020%≤Al≤0.060%, S≤0.005%, P≤0.025%, 0.002%≤B≤0.004%, the remainder being iron and unavoidable impurities resulting from the elaboration.
[0061] In a particular embodiment, at least part of the tunnel nose 15 is made by cold stamping a material having a tensile strength of at least 950 MPa. Advantageously, the use of high strength material with more than 950 MPa mechanical resistance on the final part ensures a high energy absorption during a collision. Furthermore, using cold stamping rather than hot stamping as mentioned in the previous embodiment, can reduce manufacturing costs.
[0062] For example, the tunnel nose 15 is made by cold stamping a material having a chemical composition comprising in weight %: 0.13%<C<0.25%, 2.0%<Mn<3.0%, 1.2%<Si<2.5%, 0.02%<Al<1.0%, with 1.22%<Si+Al<2.5%, Nb<0.05%, Cr<0.5%, Mo<0.5%, Ti<0.05%, the remainder being Fe and unavoidable impurities and having a microstructure comprising between 8% and 15% of retained austenite, the remainder being ferrite, martensite and bainite, wherein the sum of martensite and bainite fractions is comprised between 70% and 92%.
[0063] In another example, the tunnel nose 15 is made by cold stamping a material having a chemical composition comprising in weight %: %: 0.15%<C<0.25%, 1.4%<Mn<2.6%, 0.6%<Si<1.5%, 0.02%<Al<1.0%, with 1.0%<Si+Al<2.4%, Nb<0.05%, Cr<0.5%, Mo<0.5%, the remainder being Fe and unavoidable impurities and having a microstructure comprising between 10% and 20% of retained austenite, the remainder being ferrite, martensite and bainite.
[0064] According to a particular embodiment, the tunnel nose 15 is made by stamping a tailor welded blank. The tailor welded blank can be made of materials of different average thicknesses and strength levels for cold stamping. Alternatively, it can be made of materials of different average thicknesses and strength levels for hot stamping. Advantageously, using different grades and average thicknesses allows more flexibility to the designer to optimize the performance and weight of the part. For example, the front portion 21 is made of a material having a lower average thickness and/or a lower ultimate tensile strength than the rear portion 23.
[0065] According to a particular embodiment, the tunnel nose 15 is made by stamping a tailor rolled blank. This provides similar advantages as in the case of a tailor welded blank, explained previously. For example, the front portion 21 will be made of a material having a lower average thickness than the rear portion 23.
[0066] In a particular embodiment, the tunnel nose 15 is made of a material having an average thickness comprised between 0.8 mm and 2.0 mm. For example, the tunnel nose 15 is made by hot stamping a tailor welded blank having a first portion, corresponding to the front portion 21, consisting of a material having an average thickness of 1.1 mm and an ultimate tensile strength above 1000 MPa after hot stamping and a second portion, corresponding to the rear portion 23, having a material average thickness of 0.9 mm and an ultimate tensile strength above 1500 MPa after hot stamping. It can be verified that the product of the ultimate tensile strength by the average thickness of the rear portion 23, which is 1200 MPa.Math.mm, is higher than that of the front portion 21, which amounts to 1100 MPa.Math.mm.
[0067] The Method for producing the above described rear structure will now be described. It comprises the steps of: [0068] providing a blank [0069] stamping the blank into the shape of the tunnel nose [0070] attaching the tunnel nose to the lower dash panel; and [0071] attaching the tunnel nose to the seat cross-member.