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