When simulating or conducting land mine blast tests on armored vehicles to assess potential occupant injury, the preference is to use the Hybrid III anthropomorphic test device (ATD). In land blast events, neither the effect of body-borne equipment (BBE) on the ATD response nor the dynamic response index (DRI) is well understood. An experimental study was carried out using a drop tower test rig, with a rigid seat mounted on a carriage table undergoing average accelerations of 161 g and 232 g over 3 ms. A key aspect of the work looked at the various lumbar spine assemblies available for a Hybrid III ATD. These can result in different load cell orientations for the ATD which in turn can affect the load measurement in the vertical and horizontal planes. Thirty-two tests were carried out using two BBE mass conditions and three variations of ATDs. The latter were the Hybrid III with the curved (conventional) spine, the Hybrid III with the pedestrian (straight) spine, and the Federal Aviation Administration (FAA) Hybrid III which also has a straight spine. The results showed that the straight lumbar spine assemblies produced similar ATD responses in drop tower tests using a rigid seat. In contrast, the curved lumbar spine assembly generated a lower pelvis acceleration and a higher lumbar load than the straight lumbar spine assemblies. The maximum relative displacement of the lumbar spine occurred after the peak loading event, suggesting that the DRI is not suitable for assessing injury when the impact duration is short and an ATD is seated on a rigid seat on a drop tower. The peak vertical lumbar loads did not change with increasing BBE mass because the equipment mass effects did not become a factor during the peak loading event.
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October 2017
Research-Article
Effects of Lumbar Spine Assemblies and Body-Borne Equipment Mass on Anthropomorphic Test Device Responses During Drop Tests
Daniel Aggromito,
Daniel Aggromito
Department of Mechanical and
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
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Mark Jaffrey,
Mark Jaffrey
Defence Science and Technology Group,
Department of Defence,
506 Lorimer Street,
Fishermans Bend, Victoria 3207, Australia
Department of Defence,
506 Lorimer Street,
Fishermans Bend, Victoria 3207, Australia
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Allen Chhor,
Allen Chhor
Pacific ESI,
277-279 Broadway,
Glebe, New South Wales 2037, Australia
277-279 Broadway,
Glebe, New South Wales 2037, Australia
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Bernard Chen,
Bernard Chen
Department of Mechanical and
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
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Wenyi Yan
Wenyi Yan
Department of Mechanical and
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
e-mail: Wenyi.Yan@monash.edu
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
e-mail: Wenyi.Yan@monash.edu
Search for other works by this author on:
Daniel Aggromito
Department of Mechanical and
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
Mark Jaffrey
Defence Science and Technology Group,
Department of Defence,
506 Lorimer Street,
Fishermans Bend, Victoria 3207, Australia
Department of Defence,
506 Lorimer Street,
Fishermans Bend, Victoria 3207, Australia
Allen Chhor
Pacific ESI,
277-279 Broadway,
Glebe, New South Wales 2037, Australia
277-279 Broadway,
Glebe, New South Wales 2037, Australia
Bernard Chen
Department of Mechanical and
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
Wenyi Yan
Department of Mechanical and
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
e-mail: Wenyi.Yan@monash.edu
Aerospace Engineering,
Monash University,
Clayton, Victoria 3800, Australia
e-mail: Wenyi.Yan@monash.edu
1Corresponding author.
Manuscript received November 2, 2016; final manuscript received July 10, 2017; published online August 16, 2017. Assoc. Editor: Brian D. Stemper.
J Biomech Eng. Oct 2017, 139(10): 101004 (8 pages)
Published Online: August 16, 2017
Article history
Received:
November 2, 2016
Revised:
July 10, 2017
Citation
Aggromito, D., Jaffrey, M., Chhor, A., Chen, B., and Yan, W. (August 16, 2017). "Effects of Lumbar Spine Assemblies and Body-Borne Equipment Mass on Anthropomorphic Test Device Responses During Drop Tests." ASME. J Biomech Eng. October 2017; 139(10): 101004. https://doi.org/10.1115/1.4037401
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