Figures & data
Figure 1. Calculated MPRT as a function of LC (or OLED) response time at different frame rates.
Reproduced from Ref. [Citation14], with the permission of AIP Publishing.
![Figure 1. Calculated MPRT as a function of LC (or OLED) response time at different frame rates.Reproduced from Ref. [Citation14], with the permission of AIP Publishing.](/cms/asset/08fbf9da-824b-4463-b8e2-b26e22fb8c4a/tlcy_a_1625138_f0001_c.jpg)
Table 1. Measured physical properties of MX-40593. T = 22°C and λ = 633 nm.
Table 2. Measured GTG response time of our VA cell with overdrive and undershoot. d = 3.3 μm, λ = 633 nm and T = 22°C.
Figure 2. Schematic diagram of the proposed single-rubbing VA-FIS mode.
Reproduced from Ref. [Citation23], with the permission of The Society for Information Display.
![Figure 2. Schematic diagram of the proposed single-rubbing VA-FIS mode.Reproduced from Ref. [Citation23], with the permission of The Society for Information Display.](/cms/asset/fdca2df7-2cf1-4bee-89ae-36975c2848c5/tlcy_a_1625138_f0002_c.jpg)
Figure 3. Simulated (a) VT and (b) TT curves for VA-FIS with and without bottom alignment layer. (λ = 550 nm. Here, polyimide alignment layer is used with 70 nm thick).
Reproduced from Ref. [Citation23], with the permission of The Society for Information Display.
![Figure 3. Simulated (a) VT and (b) TT curves for VA-FIS with and without bottom alignment layer. (λ = 550 nm. Here, polyimide alignment layer is used with 70 nm thick).Reproduced from Ref. [Citation23], with the permission of The Society for Information Display.](/cms/asset/61b5593e-b834-405d-a20a-f31b9a75da62/tlcy_a_1625138_f0003_c.jpg)
Figure 4. (a) Schematic 3D diagram of the proposed DIPS structure; (b) top view and (c) cross-section view.
Reproduced from Ref. [Citation31], with the permission of Taylor & Francis Group.
![Figure 4. (a) Schematic 3D diagram of the proposed DIPS structure; (b) top view and (c) cross-section view.Reproduced from Ref. [Citation31], with the permission of Taylor & Francis Group.](/cms/asset/f1916e85-ba98-4b75-b6cd-af7d0f4cbf1d/tlcy_a_1625138_f0004_c.jpg)
Figure 5. Simulated VT curves for conventional IPS and DIPS. (w1 = 3 µm, w2 = 2.5 µm, g= 7.5 µm, h = 3.5 µm, and d= 9 µm for IPS; w1 = 3 µm, w2 = 2.5 µm, g= 3 µm, h = 3.5 µm, d= 9 µm, and l= 20 µm for DIPS).
Reproduced from Ref. [Citation31], with the permission of Taylor & Francis Group.
![Figure 5. Simulated VT curves for conventional IPS and DIPS. (w1 = 3 µm, w2 = 2.5 µm, g= 7.5 µm, h = 3.5 µm, and d= 9 µm for IPS; w1 = 3 µm, w2 = 2.5 µm, g= 3 µm, h = 3.5 µm, d= 9 µm, and l= 20 µm for DIPS).Reproduced from Ref. [Citation31], with the permission of Taylor & Francis Group.](/cms/asset/a7d83965-4a30-45da-bedc-7650aa2da00c/tlcy_a_1625138_f0005_c.jpg)
Figure 6. Pareto front defined in (a) CIE 1931 and (b) CIE 1976 with different FWHM light sources.
Reproduced from Ref. [Citation33], with the permission of Springer Nature.
![Figure 6. Pareto front defined in (a) CIE 1931 and (b) CIE 1976 with different FWHM light sources.Reproduced from Ref. [Citation33], with the permission of Springer Nature.](/cms/asset/8453a8f7-361a-492a-ab75-b99651c8a41f/tlcy_a_1625138_f0006_c.jpg)
Figure 7. Schematic diagram and working principle of the proposed backlight with a functional reflective polarizer (FRP) and a patterned half-wave plate. (TN: twisted nematic alignment; HG: homogeneous alignment).
Reproduced from Ref. [Citation33], with the permission of Springer Nature.
![Figure 7. Schematic diagram and working principle of the proposed backlight with a functional reflective polarizer (FRP) and a patterned half-wave plate. (TN: twisted nematic alignment; HG: homogeneous alignment).Reproduced from Ref. [Citation33], with the permission of Springer Nature.](/cms/asset/57cbf23e-f2c5-4419-9abd-66b3d3febb2e/tlcy_a_1625138_f0007_c.jpg)
Figure 8. Schematic diagram of the proposed device structure with an in-cell polarizer.
Reproduced from Ref. [Citation41], with the permission of The Optical Society.
![Figure 8. Schematic diagram of the proposed device structure with an in-cell polarizer.Reproduced from Ref. [Citation41], with the permission of The Optical Society.](/cms/asset/2867d8c0-2e1a-445a-b61e-e912be616173/tlcy_a_1625138_f0008_c.jpg)
Figure 9. Working mechanism of (a) conventional LCD panel with depolarization effects, and (b) the proposed LCD panel with decoupled depolarization effects.
Reproduced from Ref. [Citation41], with the permission of The Optical Society.
![Figure 9. Working mechanism of (a) conventional LCD panel with depolarization effects, and (b) the proposed LCD panel with decoupled depolarization effects.Reproduced from Ref. [Citation41], with the permission of The Optical Society.](/cms/asset/8c2e073e-1f6d-432d-93a5-246ea0866da1/tlcy_a_1625138_f0009_c.jpg)
Figure 10. Simulated isocontrast contour for the proposed device configuration in MVA mode. (a) Polarizer thickness is 24 µm, and (b) Polarizer thickness is 29 µm. For the 24-µm thick polarizer: CRmax= 12,277:1, CRmin= 132:1, and CRave = 4685:1. For the 29 µm thick polarizer: CRmax = 23,163:1, CRmin = 149:1, and CRave = 7223:1.
Reproduced from Ref. [Citation41], with the permission of The Optical Society.
![Figure 10. Simulated isocontrast contour for the proposed device configuration in MVA mode. (a) Polarizer thickness is 24 µm, and (b) Polarizer thickness is 29 µm. For the 24-µm thick polarizer: CRmax= 12,277:1, CRmin= 132:1, and CRave = 4685:1. For the 29 µm thick polarizer: CRmax = 23,163:1, CRmin = 149:1, and CRave = 7223:1.Reproduced from Ref. [Citation41], with the permission of The Optical Society.](/cms/asset/01790da2-723f-480d-a428-42dc0bc8f440/tlcy_a_1625138_f0010_c.jpg)