APPARATUS AND METHODS FOR ADDITIVELY MANUFACTURED STRUCTURES WITH AUGMENTED ENERGY ABSORPTION PROPERTIES

Abstract

Apparatus and methods for additively manufactured structures with augmented energy absorption properties are presented herein. Three dimensional (3D) additive manufacturing structures may be constructed with spatially dependent features to create crash components. When used in the construction of a transport vehicle, the crash components with spatially dependent additively manufactured features may enhance and augment crash energy absorption. This in turn absorbs and re-distributes more crash energy away from the vehicle's occupant(s), thereby improving the occupants' safety.

Claims

1. An energy absorbing structure comprising: an additively manufactured component positioned between a first structure and a second structure, the additively manufactured component comprising: at least one shell layer; and a spatially dependent profile configured to selectively distribute energy imparted on at least one of the first structure and the second structure.

2. The energy absorbing structure of claim 1, wherein the additively manufactured component further comprises a heat treated region.

3. The energy absorbing structure of claim 1, wherein the additively manufactured component is configured to selectively distribute energy from the at least one of the first structure and the second structure by absorbing an amount of energy; and wherein the amount of energy absorbed is based at least in part upon the spatially dependent profile.

4. The energy absorbing structure of claim 3, wherein the spatially dependent profile comprises a shell parameter.

5. The energy absorbing structure of claim 4, wherein the shell parameter comprises at least one of a shell thickness; a cross-sectional geometry; a sell dimension, and a shell density.

6. The energy absorbing structure of claim 3, wherein the spatially dependent profile comprises a shell material.

7. The energy absorbing structure of claim 3, wherein the additively manufactured component is configured to absorb the amount of energy based upon at least one of an intended air-bag deployment profile and a deceleration profile.

8. The energy absorbing structure of claim 1, wherein the internal cavity comprises foam.

9. The energy absorbing structure of claim 1, wherein the additively manufactured component is a frame rail.

10. A method of absorbing energy, the method comprising: configuring an additively manufactured component to include at least one shell layer and a spatially dependent profile; and positioning the additively manufactured component between a first structure and a second structure to selectively distribute energy imparted on at least one of the first structure and the second structure.

11. The method of claim 10, wherein configuring the additively manufactured component comprises at least one of varying a shell thickness, varying a material density, and varying a material of the shell region.

12. The method of claim 10, wherein configuring the additively manufactured component further comprises injecting a foam into a hollow region of the additively manufactured component.

13. A energy absorbing structure comprising an additively manufactured component, the additively manufactured component comprising: a shell having a variable cross section profile, the shell defining an internal hollow region within the additively manufactured component.

14. The energy absorbing structure of claim 13, wherein the additively manufactured component further comprises at least one additively manufactured reinforcement element.

15. The energy absorbing structure of claim 13, wherein the variable cross section profile is configured to enhance at least one of a deformation mode and an energy absorption capacity.

16. The energy absorbing structure of claim 13, wherein the variable cross section profile comprises a gauged thickness, a thickness of the gauged thickness being determined at least in part by a function of a length of the additively manufactured component.

17. The energy absorbing structure of claim 16, wherein the variable cross section profile comprises at least one initiation feature configured to initiate a structural collapse of the additively manufactured component during an impact event.

18. The energy absorbing structure of claim 17, wherein the at least one initiation feature is configured to initiate a structural collapse of the additively manufactured component during an impact event via at least one of a geometrical variation or a material variation.

19. The energy absorbing structure of claim 17, wherein the at least one initiation feature is an additively manufactured feature based upon a print parameter of a three dimensional (3D) printer.

20. The energy absorbing structure of claim 17, wherein the additively manufactured component is configured to perform at least one of substantially absorb an amount of impact energy and substantially re-distribute an amount of impact energy during the impact event.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0035] Various aspects of techniques for additively manufacturing structures with augmented energy absorption properties will now be presented in the detailed description by way of example, and not by way of limitation, in the accompanying drawings, wherein:

[0036] FIGS. 1A-D illustrate an example 3-D printer system during different stages of operation;

[0037] FIG. 2A illustrates a side view perspective of an additively manufactured crash component prior to inserting a foam block according to an embodiment.

[0038] FIG. 2B illustrates a front view perspective of the additively manufactured crash component after inserting the foam block according to the embodiment of FIG. 1A.

[0039] FIG. 3A illustrates a side view perspective of a structurally gauged crash component according to an embodiment.

[0040] FIG. 3B illustrates a two dimensional representation of the structurally gauged crash component according to the embodiment of FIG. 2A.

[0041] FIG. 3C illustrates a first cross section of the structurally gauged crash component according to the embodiment of FIG. 2A.

[0042] FIG. 3D illustrates a second cross section of the structurally gauged crash component according to the embodiment of FIG. 2A.

[0043] FIG. 3E illustrates a graph of acceleration versus time plots relating to a structurally gauged crash component according to the embodiment of FIG. 2A.

[0044] FIG. 4A illustrates a two dimensional representation of a structurally gauged crash component according to another embodiment.

[0045] FIG. 4B illustrates a first cross section of the structurally gauged crash component according to the embodiment of FIG. 3A.

[0046] FIG. 4C illustrates a second cross section of the structurally gauged crash component according to the embodiment of FIG. 3A.

[0047] FIG. 5 illustrates an additively manufactured bumper according to an embodiment.

[0048] FIG. 6A illustrates a conceptual flow diagram for additively manufacturing closed shell crash structures according to the teachings herein.

[0049] FIG. 6B illustrates a conceptual flow diagram for additively manufacturing open cell crash structures according to the teachings herein.

[0050] FIGS. 7A-7C illustrate an example cross section of a rectangular tube that may include an area that acts as a crumple initiator.

[0051] FIGS. 8A-8B are diagrams providing an example of a mandrel and a structural lattice that may be made using the mandrel.

DETAILED DESCRIPTION

[0052] The detailed description set forth below in connection with the drawings is intended to provide a description of exemplary embodiments of additively manufacturing structures with augmented energy absorption, and it is not intended to represent the only embodiments in which the invention may be practiced. The term “exemplary” used throughout this disclosure means “serving as an example, instance, or illustration,” and should not necessarily be construed as preferred or advantageous over other embodiments presented in this disclosure. The detailed description includes specific details for the purpose of providing a thorough and complete disclosure that fully conveys the scope of the invention to those skilled in the art. However, the invention may be practiced without these specific details. In some instances, well-known structures and components may be shown in block diagram form, or omitted entirely, in order to avoid obscuring the various concepts presented throughout this disclosure.

[0053] The use of 3-D printing provides significant flexibility for enabling manufacturers of mechanical structures and mechanized assemblies to manufacture complex parts. Additive manufacturing may enable techniques for manufacturing structures with augmented energy absorption properties, and more specifically to additively manufacturing collision components of a transport vehicle. For example, 3-D printing techniques provide manufacturers with the flexibility to design and build parts having energy absorption properties, which may be used for collision components of a transport vehicle.

[0054] FIGS. 1A-D illustrate respective side views of an exemplary 3-D printer system. In this example, the 3-D printer system is a powder-bed fusion (PBF) system 100. FIGS. 1A-D illustrate PBF system 100 during different stages of operation. The particular embodiment illustrated in FIGS. 1A-D is one of many suitable examples of a PBF system employing principles of this disclosure. It should also be noted that elements of FIGS. 1A-D and the other figures in this disclosure are not necessarily drawn to scale, but may be drawn larger or smaller for the purpose of better illustration of concepts described herein. PBF system 100 may include a depositor 101 that may deposit each layer of metal powder, an energy beam source 103 that may generate an energy beam, a deflector 105 that may apply the energy beam to fuse the powder material, and a build plate 107 that may support one or more build pieces, such as a build piece 109. PBF system 100 may also include a build floor 111 positioned within a powder bed receptacle. The walls of the powder bed receptacle 112 generally define the boundaries of the powder bed receptacle, which is sandwiched between the walls 112 from the side and abuts a portion of the build floor 111 below. Build floor 111 may progressively lower build plate 107 so that depositor 101 may deposit a next layer. The entire mechanism may reside in a chamber 113 that may enclose the other components, thereby protecting the equipment, enabling atmospheric and temperature regulation and mitigating contamination risks. Depositor 101 may include a hopper 115 that contains a powder 117, such as a metal powder, and a leveler 119 that may level the top of each layer of deposited powder.

[0055] Referring specifically to FIG. 1A, this figure illustrates PBF system 100 after a slice of build piece 109 has been fused, but before the next layer of powder has been deposited. In fact, FIG. 1A illustrates a time at which PBF system 100 has already deposited and fused slices in multiple layers, e.g., 150 layers, to form the current state of build piece 109, e.g., formed of 150 slices. The multiple layers already deposited have created a powder bed 121, which includes powder that was deposited but not fused.

[0056] FIG. 1B illustrates PBF system 100 at a stage in which build floor 111 may lower by a powder layer thickness 123. The lowering of build floor 111 causes build piece 109 and powder bed 121 to drop by powder layer thickness 123, so that the top of the build piece and powder bed are lower than the top of powder bed receptacle wall 112 by an amount equal to the powder layer thickness. In this way, for example, a space with a consistent thickness equal to powder layer thickness 123 may be created over the top of build piece 109 and powder bed 121.

[0057] FIG. 1C illustrates PBF system 100 at a stage in which depositor 101 is positioned to deposit powder 117 in a space created over the top surfaces of build piece 109 and powder bed 121 and bounded by powder bed receptacle walls 112. In this example, depositor 101 progressively moves over the defined space while releasing powder 117 from hopper 115. Leveler 119 may level the released powder to form a powder layer 125 that has a thickness substantially equal to the powder layer thickness 123 (see FIG. 1B). Thus, the powder in a PBF system may be supported by a powder material support structure, which may include, for example, a build plate 107, a build floor 111, a build piece 109, walls 112, and the like. It should be noted that the illustrated thickness of powder layer 125 (i.e., powder layer thickness 123 (FIG. 1B)) is greater than an actual thickness used for the example involving 150 previously-deposited layers discussed above with reference to FIG. 1A.

[0058] FIG. 1D illustrates PBF system 100 at a stage in which, following the deposition of powder layer 125 (FIG. 1C), energy beam source 103 generates an energy beam 127 and deflector 105 applies the energy beam to fuse the next slice in build piece 109. In various exemplary embodiments, energy beam source 103 may be an electron beam source, in which case energy beam 127 constitutes an electron beam. Deflector 105 may include deflection plates that may generate an electric field or a magnetic field that selectively deflects the electron beam to cause the electron beam to scan across areas designated to be fused. In various embodiments, energy beam source 103 may be a laser, in which case energy beam 127 is a laser beam. Deflector 105 may include an optical system that uses reflection and/or refraction to manipulate the laser beam to scan selected areas to be fused.

[0059] In various embodiments, the deflector 105 may include one or more gimbals and actuators that may rotate and/or translate the energy beam source to position the energy beam. In various embodiments, energy beam source 103 and/or deflector 105 may modulate the energy beam, e.g., turn the energy beam on and off as the deflector scans so that the energy beam is applied only in the appropriate areas of the powder layer. For example, in various embodiments, the energy beam may be modulated by a digital signal processor (DSP).

[0060] The use of additive manufacturing in the context of additively manufacturing structures with augmented energy absorption properties provides significant flexibility and cost saving benefits that enable manufacturers of mechanical structures and mechanized assemblies to manufacture parts with complex geometries at a lower cost to the consumer. The manufacturing techniques described in the foregoing relate to structurally designing components to improve their ability of absorbing the crash energy and undergoing controlled deformation, thereby reducing the crash pulse borne by the occupants of the vehicle, and preventing intrusion into the occupant compartment. In some instances, processes for manufacturing components may include both additively manufactured parts and commercial off the shelf (COTS) components.

[0061] During a vehicle crash, collision (impact) pulse transmits through the vehicle components. When the impact energy is not properly absorbed by the crash structure, the crash pulse represents a danger to the occupants of the vehicle. Crash pulse transmission to vehicle occupants (i.e. the passenger(s) and/or the driver), depend upon the design of the vehicle's structure, components, and chassis. Accordingly, there is a need to design a vehicle's components to absorb and/or to reduce the transmission of crash pulse to the occupant. This need carries over into, among other arenas, the design of vehicles using additively manufactured components and structures.

[0062] Apparatus and methods for additively manufactured structures with augmented energy absorption properties are presented herein. Three dimensional (3D) additive manufacturing structures may be constructed with spatially dependent features to create crash components. When used in the construction of a transport vehicle, the crash components with spatially dependent additively manufactured features may enhance and augment crash energy absorption. This in turn reduces the peak of the crash pulse, thereby improving the occupants' safety.

[0063] FIG. 2A illustrates a side view perspective 200a of an additively manufactured crash component 204 prior to inserting a foam block 202 according to an embodiment. FIG. 2B illustrates a front view perspective 200b of the additively manufactured crash component 204 after inserting the foam block 202. As shown in FIG. 2A, the crash component 204 may be hollow with a shell-like exterior and have an internal lattice 206 to provide structural support.

[0064] During manufacture, in order to insert the foam block 202 into the hollow regions of the crash component 204, the crash component 204 may be heated. In this way the foam block 202 may soften upon contact with crash component 204 and flow around the internal lattice 206. Once the temperature is reduced, the foam block 202 may re-solidify to fill the interior hollow regions of the crash component 204 as shown in FIG. 2B. The foam block 202 may include materials for enhancing support strength while enhancing the ability for the crash component to absorb crash energy. For instance, the foam block 202 may include metal materials and/or expanded polypropylene.

[0065] The crash component 204 may be a part of an automobile frame and/or structure and may provide an energy absorption region during a crash (impact) event. For instance, the crash component 204 may be part of an automobile frame crush rail or automobile chassis; and the crash component 204 may be an additively manufactured structure which is positioned between a first chassis region and a second chassis region to absorb crash energy. By absorbing crash energy, the crash component (structure) 204 may advantageously reduce the transmission of the crash force between the first and second chassis regions by absorbing it.

[0066] Although FIGS. 2A and 2B illustrate an embodiment in which the foam block 202 is inserted following heating of the crash components 204, other embodiments which do not require heating are possible. For instance, a foam may be injected without heat into some or all of the hollow region of the crash component 204. In this way some or all of the hollow region may be occupied by foam in order to tailor the manner in which the crash component 204 absorbs crash energy during an impact event.

[0067] In addition to having the lattice 206, the crash component 204 may have additional geometrical features made possible during the 3D printing process. For instance, during the 3D printing process, a spatially dependent profile may be additively manufactured into the crash component 204. In this way the crash component 204 may advantageously be tailored with 3D print parameters, materials, and geometrical variations to enhance the structural properties for absorbing crash energy.

[0068] FIG. 3A illustrates a side view perspective and FIG. 3B illustrates a two dimensional representation of a structurally gauged crash component 300 according to an embodiment. Structural gauging is when the thickness of a part is varied across the part's cross-section to obtain a required structural performance. As shown in FIGS. 3A and 3B, the crash component 300 has a top shell layer 302 and a bottom shell layer 304. The crash component 300 may be an additively manufactured crash component similar to that of FIGS. 2A and 2B, except additional geometrical and material features may be varied during the 3D printing process in order to tailor and enhance the crash energy absorption properties.

[0069] The shell thickness of the top shell layer 302 may be varied as a function of distance by forming the notches 306a-c. In the embodiment shown, the shell thickness of the bottom shell layer 304 is constant, although this need not be the case. The notches of the top shell layer 302 may be formed so that during a crash (impact) event, the crash component 300 may crush or deform initially at one or more of the notches 306a-c. In this way the spatial profile of the crash component 300 is tailored to incorporate a crush initiation feature, also referred to as crush initiator. The crush initiation feature or crush initiator may be a cutout or indent, for example. During a crash, the crush initiation feature may provide a controlled energy absorption crush location where the crash energy, or a substantial amount of crash energy, is absorbed into the crash component 300. Controlling the crash energy via crush initiation features may save lives by absorbing and re-distributing energy away from passengers and/or occupants of the automobile or transport structure. In an aspect, the crush initiators, e.g., notches may be along the outer surface of the component

[0070] FIG. 3C illustrates a first cross section of the structurally gauged crash component 500 delineated by the line d.sub.a of FIG. 3B, and FIG. 3D illustrates a second cross section delineated by the line d.sub.b drawn through the notch 306b in FIG. 3B. As illustrated by the cross sections of FIGS. 3C and 3D, the top shell layer 302 and the bottom shell layer 304 may be part of continuous shell region. In the shell region delineated by the line d.sub.a, the top shell layer 302 has thickness t.sub.a, and the bottom shell layer 304 has thickness t.sub.a (see also FIG. 3B). In the shell region delineated by the line d.sub.b, the top shell layer 502 has thickness t.sub.b inside the notch 306b, and the bottom shell layer 304 has thickness t.sub.a. By additively manufacturing the notch 306b to have thickness t.sub.b less than thickness t.sub.a, the notch 306b may enhance the energy absorption properties of the manufactured crash component 300. For instance, as shown in FIG. 3E, the energy absorption properties may be tailored to reduce a net acceleration experienced by the transport vehicle's occupant(s).

[0071] Although FIGS. 3A-3D illustrate the crash component 300 as using structurally gauged notches 306a-c in the top shell layer 302 to implement crush initiation features; other embodiments are possible. In addition to notches 306a-c, other parameters, or shell parameters, may be varied during the additive manufacturing process to form a spatially dependent crash structure profile. In some embodiments fewer or greater notches may be used. In other embodiments, the material properties including shell density and/or shell material may be varied during the additive manufacturing process. For instance, the crash component 300 may use one alloy of material in one region while using another alloy in an adjacent region. In an alternative embodiment, one or more of the notches 306a-c may also have a different shape than the curved shape shown. For example, stair-stepped shapes, notched shapes, triangular shapes, rectangular shapes, or numerous other geometrical configurations may be possible as described in certain examples below.

[0072] Additionally, the notches may be formed in a manner which maintains the structural integrity of the crash component 300. For instance, during normal operation the crash component 300 may provide structural stability within the framework of an automobile or transport vehicle so as to enhance a load bearing strength. Additionally, the crash structure may be tailored to reduce mass. In this way the additively manufactured crash component 300 may advantageously enhance a load bearing strength to mass ratio and/or figure of merit.

[0073] FIG. 3E illustrates a graph 320 of acceleration versus time plots 322 and 324 relating to the structurally gauged crash component 300. Plot 322 may represent the acceleration profile experienced by an occupant in a vehicle during a crash without a crash component installed, and plot 324 may represent the acceleration profile experienced by the occupant when the crash component 300 is installed in part of the vehicle's structure or frame. As shown in FIG. 3E, the crash component 300 enhances energy absorption in a manner which reduces the net acceleration peaks at times labeled time.sub.1 and time.sub.2. This reduction in peak acceleration indicates that crash pulse experienced by the occupant is reduced, thereby improving the occupant's chances of survival.

[0074] Although the crash component 300 of FIGS. 3A-3D has been tailored to reduce peaks of a deceleration profile experienced during a crash, other profiles may be used. For instance, the crash component 300 may be tailored to absorb energy based upon an intended air-bag deployment profile. Alternatively and additionally, the manufactured crash structure may be configured to absorb an amount of crash energy based upon alternative deceleration profiles having greater or fewer peaks.

[0075] FIG. 4A illustrates a two dimensional representation of a structurally gauged crash component 400 according to another embodiment. The crash component 400 is similar to the crash component 300, except the spatially dependent profile is additively manufactured to have a different geometry. For instance, unlike the crash component 300, the crash component 400 does not have notches 306a-c. Instead, the crash component 400 is additively manufactured with a top shell layer 402 and a bottom shell layer 404, both having a variable spatially dependent profile. The shell thickness may be additively manufactured so that the top shell layer 402 and the bottom shell layer 404 form a structure with enhanced load bearing strength to mass ratio and/or figure of merit. Having variable thickness may advantageously tailor the crash component 400 to absorb a substantial amount of crash energy; additionally the crash energy may be absorbed in a manner which follows a desired deceleration profile.

[0076] FIG. 4B illustrates a first cross section of the structurally gauged crash component 400 delineated by the line d.sub.1 of FIG. 4A, and FIG. 4B illustrates a second cross section delineated by the line d.sub.2 of FIG. 4A. As shown the cross section profile delineated by the line d.sub.1 may have a shell profile with shell thickness t.sub.1; and the cross section profile delineated by the line d.sub.2 may have a shell profile with shell thickness t.sub.2 greater than t.sub.1. In an aspect, variable thickness may be achieved by additively manufacturing a structure. Because additively manufacturing is used, no secondary operation needs to be performed and no tooling is required for the variable thickness profiles to be achieved in the structure.

[0077] Although FIGS. 4A-4C illustrate a crash component 400 with spatially dependent profiles represented by shell thickness variations; other configurations are possible. For instance, in other configurations a shell material density may be varied; alternatively a shell material or alloy may be varied a function of position. These alternative configurations are deemed to fall within the scope of the present disclosure.

[0078] Additionally, alternative structures other than closed shell structures may be used to make crash components. For instance, skeletal features and rib (reinforcement) features may be additively manufactured into a transport structure. These reinforcement features may also be additively manufactured to have spatially dependent profiles for enhancing crash energy absorption. Also, crash component features and elements may be co-printed at the same time. For instance, a reinforcement feature may be concurrently printed with a lattice feature within a crash component.

[0079] FIG. 5 illustrates a cross-sectional view of an additively manufactured bumper 500 according to an embodiment. The additively manufactured bumper has a support region 506 with hollow sections 508a-c. Adjacent the support region 506 is an additively manufactured lattice 504 having a first lattice density; and in front of the bumper is a series of additively manufactured lattice elements 502a-j having a second lattice density less than the first lattice density. The additively manufactured bumper may be placed in the front or rear of a transport vehicle so that during a crash, the lattice elements 502a-j may absorb energy first by being located closest to the point of impact. In the event of an impact with a pedestrian, such an architecture would prevent significant harm to the pedestrian. Having a series of lattice elements 502a-j with lower density at the impact location may advantageously absorb energy and reduce the crash pulse transmitted to either the occupants of the vehicle, or the pedestrian being impacted. The higher density lattice 504 may further absorb crash energy before it reaches the support region 506. Having hollow sections 508a-c may further reduce mass of the bumper structure while maintaining a high load bearing strength to mass ratio and/or figure of merit.

[0080] Although the additively manufactured bumper 500 shows an embodiment using an additively manufactured lattice 504 of a first lattice density and a series of lattice elements 502a-j of a second density located at a defined impact location, other configurations are possible. For instance, additional lattice regions of variable densities may be included between the series of lattice elements 502a-j and the support region 506. Also, greater or fewer hollow sections 508a-c may be included within the support region 506. In addition to having lattice elements 502a-j, skeletal features may also be implemented with reinforcement sections which may be concurrently printed with the lattice elements 502a-j. In other embodiments, foam may be injected into the lattice regions to enhance energy absorption properties. These features disclosed in the illustrations above may be implemented individually, or combined in part or in whole to maximize the safety profile for the occupants in the vehicle or other transport structure.

[0081] Often energy absorbing structures may be used so that a catastrophic failure of a part may be controlled or avoided. For example, energy absorbing structures may be used so that the catastrophic failure of a part may be controlled under a crash load. In an aspect, higher energy absorbing structures may be additively manufactured. For example, higher energy absorbing structures may be additively manufactured, may be achievable by (1) additive deposition of a lower strength, higher ductility material at specific spots to act as a crumple initiator, (2) using a mandrel (plastic, metal) to create a structural lattice in the shape of a thin walled crash rail, (3) using specific high ductility, low yield materials placed strategically in the lattice, or (4) using multiple mixed materials in specific geometric patterns to cause crash energy to be directed to areas where conversion may take place.

[0082] FIG. 6A illustrates a conceptual flow diagram 600 for additively manufacturing closed shell crash structures (components) according to the teachings herein. In step 602 the additively manufactured crash component (structure) is defined to be a closed structure having a shell. The crash component may correspond to crash component 300 and/or crash component 400 and be defined to absorb crash energy based upon an occupant deceleration profile. The crash component may additionally be defined to have crush initiation features. In step 604 the shell cross section profile is varied using additive manufacturing. Shell parameters including thickness, material type, and density may be varied as a function of position.

[0083] FIG. 6B illustrates a conceptual flow diagram 630 for additively manufacturing open cell crash structures (components) according to the teachings herein. Open cell crash components may include bumpers and structures created with open regions and reinforcement structures. In step 632 a target impact location for the crash structure having an open cell structure may be defined by using computational methods. In step 634 at least one reinforcement structure may be additively manufactured with a spatially dependent profile according to a deceleration profile; and a lattice may be concurrently co-printed with the reinforcement structure.

[0084] FIGS. 7A-7C illustrate an example cross section of a rectangular tube 700 that may include an area that acts as a crumple initiator 714. The rectangular tube 700 may include sides of an initial tube 702. Materials such as a first material 704, a second material 708, and a third material 710 may be additive deposited, e.g., using a cold spray nozzle 706. As discussed above, in one aspect, an additive deposition of a lower strength, higher ductility material at specific spots may be used to act as a crumple initiator 714. Optionally, the rectangular tube 700 may be coated with an external layer 712 made of first material 712. Examples of lower strength, higher ductility material that may be used may include, but are not limited to magnesium, copper, aluminum, titanium, iron, plastics, ceramics, or combinations thereof. The lower strength, higher ductility material may, however, be any material that is at least one of lower strength or higher ductility as compared to a material on to which the additive deposition is occurring. In an aspect, the additive deposition may be coldspray additive manufacturing, printer using a 3-D printer system, other additive manufacturing or some combination of these. (The example of FIGS. 7A-7C uses coldspray.) Coldspray is a manufacturing process wherein the material being deposited is kept below its melting point, configured to impact the base material at a speed high enough to induce solid state welding. The locations or spots where the lower strength, higher ductility material may be directed may be any area where a small increase in strength may provide a crumple initiator 718 or crumple location.

[0085] As discussed above, one aspect may additively deposit material on a standardized extrusion or other part to selectively strengthen some areas over other areas. For example, the initial tube 702 may be a standardized extrusion or other part. Selectively strengthening some areas over other areas may better control crumpling. For example, material 708 may be repeated multiple times to increase crumpling areas of a structure. Increased crumpling may increase energy absorption. For example, one aspect may coldspray material 708, 3-D printing material 708, or otherwise additively manufacturing materials 708 onto a standardized extrusion or other part to selectively strengthen some areas over other areas. In an aspect, coldspraying (or otherwise additively manufacturing) material onto a standardized extrusion or other parts may better control crumpling. For example, crumpling may be increased. Increased crumpling may increase energy absorption of a part having the increased crumpling.

[0086] As discussed above, one aspect may use a tube 702 that may be a hollow square composite tube (e.g. carbon fiber composite) and coldspray a strong ductile aluminum alloy on the outside to create a hybrid CFRP-aluminum crash rail. In an aspect, hollow square composite tube may be brittle, e.g., before the addition of the strong ductile aluminum alloy on the outside to create the hybrid CFRP-aluminum crash rail.

[0087] As discussed above, one aspect may use additive deposition. The additive deposition may be an additive deposition of metals with higher ductility and lower strength. The higher ductility and lower strength material may be, but is not limited to magnesium, copper, aluminum, titanium, iron, plastics, ceramics, or combinations thereof, for example. The higher ductility and lower strength material may be additive deposition through coldspray (or otherwise additively manufacturing). The higher ductility and lower strength material may be additive deposition at specific areas. The coldspray (or otherwise additively manufacturing) at specific areas may allow for tunable crumple propagation.

[0088] FIGS. 8A-8B are diagrams 800 providing an example of a mandrel 802 and a structural lattice 804 that may be made using the mandrel 802. In an aspect, the mandrel may be sacrificial. Accordingly, the mandrel may be removed after the deposition is complete in some examples. The structural lattice 804 may include a first material 806 and a second material 808. The first material 806 and the second material 808 may be cold spray deposited 810 (or otherwise additively manufactured).

[0089] As discussed above, one aspect may use of the mandrel 802 (e.g., of plastic, metal) to create the structural lattice 804 in the shape of a thin walled crash rail. The structural lattice 804 may be wrapped around, placed on, secured to, or otherwise coupled or connected to a structure (such as a tube). The structural lattice 804 may provide increased strength to the structure, e.g., tube. The increased strength to the structure may allow the structure to be used as a thin walled crash rail.

[0090] As discussed above, one aspect may increase a structural lattice's ability to absorb energy with specific high ductility, low yield materials placed strategically in the lattice 804. For example, the structural lattice 804 may be made of various materials, including, but not limited to magnesium, copper, aluminum, titanium, iron, plastics, ceramics, or combinations thereof. The material or materials used may provide the structural lattice 804 with the ability to absorb energy. The materials may be specific high ductility, low yield materials placed strategically in the lattice. The location of the materials within the structural lattice 804 may increase the structural lattice's 804 ability to absorb energy. As discussed above, one aspect may increase a structural lattice's 804 ability to absorb energy with multiple mixed materials in specific geometric patterns to cause crash energy to be directed to areas where conversion may take place.

[0091] The previous description is provided to enable any person skilled in the art to practice the various aspects described herein. Various modifications to these exemplary embodiments presented throughout this disclosure will be readily apparent to those skilled in the art, and the concepts disclosed herein may be applied to other techniques for printing structures with augmented energy absorption properties. Thus, the claims are not intended to be limited to the exemplary embodiments presented throughout the disclosure, but are to be accorded the full scope consistent with the language claims. All structural and functional equivalents to the elements of the exemplary embodiments described throughout this disclosure that are known or later come to be known to those of ordinary skill in the art are intended to be encompassed by the claims. Moreover, nothing disclosed herein is intended to be dedicated to the public regardless of whether such disclosure is explicitly recited in the claims. No claim element is to be construed under the provisions of 35 U.S.C. § 112(f), or analogous law in applicable jurisdictions, unless the element is expressly recited using the phrase “means for” or, in the case of a method claim, the element is recited using the phrase “step for.”