Figures & data
Figure 1. Classification of Fiber metal laminates based on metal alloys (Sinmazçelik et al., Citation2011). (adapted and modified).
![Figure 1. Classification of Fiber metal laminates based on metal alloys (Sinmazçelik et al., Citation2011). (adapted and modified).](/cms/asset/dcdb7310-9109-443a-b72c-d771564bce0b/lmst_a_2369856_f0001_c.jpg)
Figure 2. (a) schematic representation of specimen preparation using vacuum bagging method and (b) schematic of an alternate layer of Ti sheets and carbon fiber prepregs.
![Figure 2. (a) schematic representation of specimen preparation using vacuum bagging method and (b) schematic of an alternate layer of Ti sheets and carbon fiber prepregs.](/cms/asset/e9c0e10e-6176-4410-ab46-c84e6c4ef456/lmst_a_2369856_f0002_c.jpg)
Figure 4. Image of experimental setup indicating two machining conditions: (a) Cryogenic machining and (b) Dry machining and instruments for various response measurements.
![Figure 4. Image of experimental setup indicating two machining conditions: (a) Cryogenic machining and (b) Dry machining and instruments for various response measurements.](/cms/asset/6d630e5f-58fc-4eff-b1f2-63ac4a8650db/lmst_a_2369856_f0004_c.jpg)
Table 1. Details about machine tool and cutting tool.
Figure 7. Surface roughness measurement for dry and cryogenic machining under same cutting parameters (a) surface roughness (μm) comparison for both machining conditions, (b) measurement of surface roughness of holes through surface roughness tester, and (c) tangled Ti chips around the drill bit during dry machining.
![Figure 7. Surface roughness measurement for dry and cryogenic machining under same cutting parameters (a) surface roughness (μm) comparison for both machining conditions, (b) measurement of surface roughness of holes through surface roughness tester, and (c) tangled Ti chips around the drill bit during dry machining.](/cms/asset/81cb0d38-9670-476c-805d-d5718b5da52f/lmst_a_2369856_f0007_c.jpg)
Figure 8. Flank wear progression for (a) cryogenic machining, (b) dry machining, and (c) Dry vs. Cryogenic comparison with respect to the number of holes drilled.
![Figure 8. Flank wear progression for (a) cryogenic machining, (b) dry machining, and (c) Dry vs. Cryogenic comparison with respect to the number of holes drilled.](/cms/asset/5ec87a13-73dc-41cc-ac6b-aa96af35172f/lmst_a_2369856_f0008_c.jpg)
Figure 9. Flank wear images of drill bits for the dry and cryogenic environments, where (1) corner wear, (2) chemical reactivity due to Ti6Al4V on the tool, (3) BUE on the corner, (4) abrasion, and (5) catastrophic failure.
![Figure 9. Flank wear images of drill bits for the dry and cryogenic environments, where (1) corner wear, (2) chemical reactivity due to Ti6Al4V on the tool, (3) BUE on the corner, (4) abrasion, and (5) catastrophic failure.](/cms/asset/1db5a9c4-716f-45c9-bf4a-b79039b93b49/lmst_a_2369856_f0009_c.jpg)
Figure 11. comparison of (a) power consumption and (b) specific cutting energy while drilling HTCL during dry and cryogenic environments.
![Figure 11. comparison of (a) power consumption and (b) specific cutting energy while drilling HTCL during dry and cryogenic environments.](/cms/asset/6ac0222b-e22f-40bc-ac79-22363c1a95a6/lmst_a_2369856_f0011_c.jpg)
Table 2. Details of Life cycle inventory.
Table 3. Database to produce 1 unit of solid carbide drill bit (Maheshwari et al., Citation2023).
Table 4. Database for production of one HTCL workpiece sample.
Table 5. Data sources for LCI.
Figure 14. Relative indicator results of the respective project variants for dry and cryogenic machining.
![Figure 14. Relative indicator results of the respective project variants for dry and cryogenic machining.](/cms/asset/03cdf01c-3b88-4078-bfc9-ca8ea9208db9/lmst_a_2369856_f0014_c.jpg)
Table 6. Impact assessment results of various categories under both cutting conditions.