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An approach for including social impact measures in systems design exploration

Published online by Cambridge University Press:  06 July 2023

Daniel C. Richards
Affiliation:
Department of Mechanical Engineering, Brigham Young University, Provo, UT, USA
Phillip D. Stevenson
Affiliation:
Department of Mechanical Engineering, Brigham Young University, Provo, UT, USA
Christopher A. Mattson
Affiliation:
Department of Mechanical Engineering, Brigham Young University, Provo, UT, USA
John L. Salmon*
Affiliation:
Department of Mechanical Engineering, Brigham Young University, Provo, UT, USA
*
Corresponding author J. L. Salmon johnsalmon@byu.edu
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Abstract

Engineered products have economic, environmental, and social impacts, which comprise the major dimensions of sustainability. This paper seeks to explore interactions between design parameters when social impacts are incorporated into the concept development phase of the systems design process. Social impact evaluation is increasing in importance similar to what has happened in recent years with environmental impact consideration in the design of engineered products. Concurrently, research into new airship design has increased. Airships have yet to be reintroduced at a large scale or for a range of applications in society. Although airships have the potential for positive environmental and economic impacts, the social impacts are still rarely considered. This paper presents a case study of the hypothetical introduction of airships in the Amazon region of Brazil to help local farmers transport their produce to market. It explores the design space in terms of both engineering parameters and social impacts using a discrete-event simulation to model the system. The social impacts are found to be dependent not only on the social factors and airship design parameters but also on the farmer-airship system, suggesting that socio-technical systems design will benefit from integrated social impact metric analysis.

Information

Type
Research Article
Creative Commons
Creative Common License - CCCreative Common License - BY
This is an Open Access article, distributed under the terms of the Creative Commons Attribution licence (http://creativecommons.org/licenses/by/4.0), which permits unrestricted re-use, distribution and reproduction, provided the original article is properly cited.
Copyright
© The Author(s), 2023. Published by Cambridge University Press
Figure 0

Figure 1. Three circles representing the relationship between economic, environmental, and social impacts (McKenzie 2004).

Figure 1

Figure 2. A selection of high-level design parameters of an axisymmetric airship.

Figure 2

Figure 3. Steps for predicting social impact of engineered products, building upon those suggested by Stevenson et al. (2020).

Figure 3

Figure 4. Regional map around Manaus, the location of the market where all produce is sold in the simulation, and the communities that the airship services.

Figure 4

Figure 5. Daily production over 1 year for the nine fruits in the four cities included in the study (IBGE–Instituto Brasileiro de Geografia e Estatística 2017).

Figure 5

Table 1. Number of farmers and distances from each city to Manaus (IBGE–Instituto Brasileiro de Geografia e Estatística 2017)

Figure 6

Figure 6. High-level airship design parameter interaction.

Figure 7

Figure 7. Integration of airship design parameters and indicator variables for evaluation of the social impact metrics.

Figure 8

Figure 8. State diagram of the discrete-event simulation.

Figure 9

Table 2. Ranges of system design parameters used in simulation set

Figure 10

Figure 9. Social impact indicators, totaled for all farmers in all cities, are plotted against the linked airship design parameters. The Z-axes show the social impacts, with X- and Y-axes showing payload and cruise speed. The color scale denotes desirability with green indicating most desirable and pink, least desirable. The $ x $ shown in the payload-cruise plane marks the maximum impact on the contour plot projected onto that plane. Note that the axes in the impact to income graph in the lower left are rotated 270° about the vertical axis (relative to what is shown in the other three graphs) to better show the decrease to the impact at higher payloads and cruise speeds.

Figure 11

Figure 10. Impact to farmer income is shown for a single, constant payload amount. The discrete surface slices correspond to different fleet sizes (left) and different load thresholds (right). At this payload of between 5 and 6 tons, single-airship fleets are less profitable than larger fleets at low speeds since they cannot transport all of the produce. At higher speeds and fleet sizes, the operational costs increase more rapidly. Higher load thresholds result in more productive trips.

Figure 12

Figure 11. Helium refill cost as a function of airship payload.

Figure 13

Figure 12. Fuel consumption as a function of airship payload, with cruise speed and load threshold held constant (left), and of cruise speed, with payload and load threshold held constant (right).

Figure 14

Figure 13. Shown is one day’s activity for two airship designs differing only by a payload of one ton. The airships follow a similar schedule until hour 2075 (denoted by vertical line, Event A). The smaller airship is also unable to visit the fourth city before returning to the hub to unload its cargo. The larger airship loads only a small amount of fruit from the fourth city (Event B). The smaller airship is ultimately able to transport more fruit due to a more productive trip to the fourth city after unloading first in Manaus (Event C).

Figure 15

Figure 14. Depending on the system configuration, the routes taken by the fleets can vary considerably. The diagrams above are three points on the spectrum of possible route options. The weight of the arrows indicate more trips traversing that leg. The return legs are shown as dashed red lines.

Figure 16

Table 3. Results of neural network model fitting

Figure 17

Table 4. Results of optimization using various weightings corresponding to potential stakeholder preferences

Figure 18

Figure 15. The contour plots of each impact are shown with optimal designs described in Table 4. These points, with markers defined in the bottom, right, show the tradeoffs for each impact to achieve the desired objectives of each cost function weighting. The color scale denotes desirability with green indicating most desirable and pink least desirable.

Figure 19

Figure 16. Fleet utilization as a function of airship payload, with cruise speed and load threshold held constant (left), and of cruise speed, with payload and load threshold held constant (right).

Figure 20

Figure 17. Fleet utilization and operational cost per ton. Lower utilization means the airship transports all of the produce more quickly, but this is more costly. Lower utilization may also mean that the fleet’s freight transportation capacity is over-designed for the given scenario.

Figure 21

Table 5. Shown is the design optimized for time and cost and the optimal-impact design

Figure 22

Table 6. Results of optimization using a range of average load rates and a constant load threshold of one ton