# US 8,770,639 B2 · Bumper assembly

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- Number: US 8,770,639 B2
- Document ID: US8770639B2
- Status: Granted
- Kind: B2
- Application number: 13/810,784
- Filed: 2011-08-03
- Published: 2013-05-16
- Granted: 2014-07-08
- Earliest claimed: 2010-08-03
- Assignees: Cosma Engineering Europe AG
- Applicants: Michael Blümel; Christian Hengst; Ernst Lindtner
- Inventors: Michael Blümel; Christian Hengst; Ernst Lindtner
- Web page: https://patentgrep.com/patent/US8770639B2

## CPC

- B60R 19/34: destroyed upon impact, e.g. one-shot type
- B21D 53/88: other parts for vehicles, e.g. cowlings, mudguards
- B60R 19/03: characterised by material, e.g. composite (B60R19/18 takes precedence)
- B60R 19/18: {characterised by the cross-section;} Means within the bumper to absorb impact
- B21D 22/02: Stamping using rigid devices or tools
- B21D 22/022: {by heating the blank or stamping associated with heat treatment (C21D takes precedence)}
- B21D 37/16: Heating or cooling
- B60R 19/26: comprising yieldable mounting means ({B60R19/38 takes precedence;} springs, shock absorbers, or means for damping vibrations per se F16F)
- B60R 2019/1813: {made of metal}
- B60R 2019/182: {of light metal, e.g. extruded}
- B60R 2019/1826: {of high-tension steel}
- C21D 1/673: for die quenching
- C21D 8/0221: characterised by the working steps
- C21D 8/0294: involving a localised treatment
- C21D 9/46: for sheet metals
- Y10T 29/49622: Vehicular structural member making
- Y10T 29/49826: Assembling or joining
- B60R: VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B21D: WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL (working or processing of wire B21F)
- C21D: MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING (surface treatment of metallic material involving at least one process provided for in class C23 and at least one process covered by this subclass C23F17/00; unidirectional solidification of eutectic materials or unidirectional demixing of eutectoid materials C30B)
- Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION

## Abstract

A method of making a beam-box crash management system comprises forming a first shell (100a) from a fist sheet metal blank by a hot forming process. The first shell has a high tensile strength beam portion (102a) and integrally formed there-with a first low yield strength crash box portion (104a)proximate a first end of the beam portion and second low yield strength crash box portion proximate a second end of the beam portion. The first shell also has an open face extending continuously along the beam portion and each of the first and second crash box portions (104a, 106a). A closing element (100b) is formed from a second sheet metal blank, and is fixedly secured adjacent to the open face of the first shell.

## Claims

### Claim 1

A method of making a beam-box crash management system, comprising:
forming a first shell from a first sheet metal blank by a hot forming process, the first shell having a high tensile strength beam portion and integrally formed therewith a first low yield strength crash box portion proximate a first end of the beam portion and a second low yield strength crash box portion proximate a second end of the beam portion, the first shell having an open face extending continuously along the beam portion and each of the first and second crash box portions;
forming a closing element from a second sheet metal blank, wherein forming the closing element comprises forming a second shell by a hot forming process, the second shell having a high tensile strength beam portion and integrally formed therewith a first low yield strength crash box portion proximate a first end of the beam portion and a second low yield strength crash box portion proximate a second end of the beam portion, the second shell having an open face extending continuously along the beam portion and each of the first and second crash box portions; and
fixedly securing the second shell adjacent to the open face of the first shell.

### Claim 2 (depends on 1)

A method according to claim 1, wherein the tensile strength of the beam portions of the first and second shells is between approximately 1300 N/mm2 and approximately 1600 N/mm2.

### Claim 3 (depends on 1)

A method according to claim 1, wherein the yield strength of the first and second crash box portions of the first and second shells is between approximately 200 N/mm2 and 450 N/mm2.

### Claim 4 (depends on 1)

A method according to claim 1, wherein fixedly securing the second shell adjacent to the open face of the first shell comprises one of thermally joining, adhesively bonding and mechanically coupling the second shell to the first shell.

### Claim 5

A method of making a beam-box crash management system, comprising:
heating a first sheet metal blank to at least an austenitizing temperature of the metal;
hot forming the austenitic blank in a pair of cooled tools to form a first one piece beam-box component having a generally three-sided channel structure with one open side;
during the hot forming process, cooling a beam portion of the formed component at a first rate that is sufficiently rapid to harden the beam portion into an essentially martensitic structure with a tensile strength of between about 1300 N/mm2 and about 1600 N/mm2, and cooling crash box portions of the formed component at a second rate that is slower than the first rate, such that the crash box portions achieve a yield strength of between approximately 200 N/mm2 and 450 N/mm2;
forming a closing element from a second sheet metal blank, wherein forming the closing element comprises:
heating a second sheet metal blank to at least an austenitizing temperature of the metal;
hot forming the austenitic blank in a pair of cooled tools to form a second one piece beam-box component having a generally three-sided channel structure with one open side;
during the hot forming process, cooling a beam portion of the formed component at a first rate that is sufficiently rapid to harden the beam portion into an essentially martensitic structure with a tensile strength of between about 1300 N/mm2 and about 1600 N/mm2, and cooling crash box portions of the formed component at a second rate that is slower than the first rate, such that the crash box portions achieve a yield strength of between approximately 200 N/mm2 and 450 N/mm2; and
fixedly securing the second one piece beam component along the open side of the first one piece beam-box component.

### Claim 6 (depends on 5)

A method according to claim 5, wherein the crash box portions of the first and second one piece beam-box components include a first crash box portion integrally formed with the beam portion proximate a first end of the beam portion and a second crash box portion integrally formed with the beam portion proximate a second end of the beam portion, the first end being opposite the second end.

### Claim 7 (depends on 5)

A method according to claim 5, wherein fixedly securing the second one piece beam-box component along the open side of the first one piece beam-box component comprises one of thermally joining, adhesively bonding and mechanically coupling the second one piece beam-box component to the first one piece beam-box component.

### Claim 8

A beam-box crash management system, comprising:
a first one piece shell having a high tensile strength beam portion and integrally formed therewith a first low yield strength crash box portion proximate a first end of the beam portion and a second low yield strength crash box portion proximate a second end of the beam portion, the first one piece shell having an open face extending continuously along the beam portion and each of the first and second crash box portions; and
a closing element fixedly secured adjacent to the open face of the first one piece shell, wherein the closing element includes a second one piece shell having a high tensile strength beam portion and integrally formed therewith a first low yield strength crash box portion proximate a first end of the beam portion and a second low yield strength crash box portion proximate a second end of the beam portion, the second one piece shell having an open face extending continuously along the beam portion and each of the first and second crash box portions.

### Claim 9 (depends on 8)

A beam-box crash management system according to claim 8, wherein the tensile strength of the beam portions of the first and second one-piece shells is between approximately 1300 N/mm2 and about 1600 N/mm2.

### Claim 10 (depends on 8)

A beam-box crash management system according to claim 8, wherein the yield strength of the first and second crash box portions of the first and second one piece shells is between approximately 200 N/mm2 and 450 N/mm2.

### Claim 11 (depends on 8)

A beam-box crash management system according to claim 8, wherein the second one piece shell is fixedly secured adjacent to the open face of the first one piece shell by one of thermal joining, adhesive bonding and mechanical coupling of the second one piece shell to the first one piece shell.

### Claim 12

A beam-box crash management system, comprising:
a first beam-box shell, fabricated from a first sheet metal blank, having a high tensile strength beam portion and integrally formed therewith a first low yield strength crash box portion proximate a first end of the beam portion and a second low yield crash box portion proximate a second end of the beam portion, the first end being opposite the second end, and the first beam-box shell having one open side defining a first rim;
a second beam-box shell, fabricated from a second sheet metal blank, having a high tensile strength beam portion and integrally formed therewith a first low yield strength crash box structure proximate a first end of the beam portion and a second low strength crash box structure proximate the second end of the beam portion, the first end being opposite the second end, and the second beam-box shell having one open side defining a second rim;
wherein the first beam-box shell is fixedly secured to the second beam-box shell such that the first rim abuts the second rim, and such that the beam portion of the first beam-box shell is aligned with the beam portion of the second beam-box shell and the first and second crash box structures of the first beam-box shell are aligned with a respective one of the first and second crash box structures of the second beam-box shell.

### Claim 13 (depends on 12)

A beam-box crash management system according to claim 12, wherein the second rim is received within the first rim in a nesting arrangement when the first beam-box shell is fixedly secured to the second beam-box shell.

### Claim 14 (depends on 12)

A beam-box crash management system according to claim 12, wherein the tensile strength of the beam portion is between approximately 1300 N/mm2 and approximately 1600 N/mm2.

### Claim 15 (depends on 12)

A method according to claim 12, wherein the yield strength of each of the first and second crash box portions is between approximately 200 N/mm2 and 450 N/mm2.
