Investigation of Composite Structure with Dual Fabry–Perot Cavities for Temperature and Pressure Sensing

: To deeply analyze the inﬂuence of diaphragm materials on the temperature and pressure sensitivity of Fabry–Perot interferometer-based dual-parameter ﬁber sensors, the multiple transfer method was used to fabricate the dual Fabry–Perot cavities, respectively, consisting of the following combinations: epoxy resin AB/polydimethylsiloxane (PDMS), Ecoﬂex0030 silicone rubber /PDMS, and PDMS/Ecoﬂex0030 silicone rubber. Experimental results show that the temperature sensitivities are, respectively, 528, 540, and 1033 pm/ ◦ C in the range of 40–100 ◦ C. Within the applied pressure range of 100–400 kPa, the pressure sensitivities are, respectively, 16.0, 34.6, and 30.2 pm/kPa. The proposed sensors have advantages of proper sensitivity, simple fabrication, cost-effectiveness, controllable cavity length, and suitability for practical sensing applications.


Introduction
Optical fiber sensors have been widely used in many domains owing to the advantages of low cost, high sensitivity, fast response time, and good stability. Simultaneously, different sensor structures with diverse sensitivities to various parameters can be used to realize dual-or even multi-parameter sensing, such as temperature, pressure, refractive index, etc. [1,2].
Several studies have characterized the investigations of single or dual-parameter monitoring based on fiber tip bubble [3], Mach-Zehnder interferometer [4], fiber Bragg gratings [5], Sagnac interferometer [6], etc. Due to the advantages of small size, good measurement performance, and survivability in complicated electromagnetic environment [7][8][9][10][11][12][13][14][15][16][17][18][19], Fabry-Perot Interferometer (FPI)-based dual-parameter fiber sensors have been extensively studied for the measurement of temperature and pressure. However, FPI-based fiber sensors impose the limitation of the durability and operation stability of the thin diaphragm that is used to form the FP cavity. Consequently, series of dual FP cavities sensors based on various diaphragms to improve the sensing performance are utilized to monitor the temperature and pressure [7][8][9][10][11][12], which share the characteristic of ultra-high sensitivity. While endlessly pursuing high sensitivity will bring several problems which should be paid more attention, only this kind of fiber sensor can be applied for ultra-precise monitoring applications. Moreover, it will result in a great challenge for the design of the interrogator's bandwidth. Another dual FPI-based fiber sensor consisting of two tiny segments of hollow-core fiber located at the end of lead-in single mode fiber, with a misalignment fusion splicing between the two hollow-core fibers with different core diameter, is reported in [13]. The proposed sensor can be used in simultaneous measurement of pressure and temperature, but its sensitivity should be significantly enhanced. Some chemical etching method-assisted FPI fabrication processes are reported in [14][15][16], which can provide good sensing performances. Unfortunately, the corrosive effects of the chemical etching and the precise etching time are difficult to control. The authors of [17,18] demonstrated easy-to-fabricate dual-FPIs. However, the sensitivity and repeatability of the fabrication for the FP cavity should be improved. By filling a hollow capillary with two sections of PDMS, which are fused to the single-mode fiber, the authors of [19] investigated a novel dual FP cavities-based fiber sensor to detect the temperature and pressure. However, the fabrication of this kind of structure is costly due to the fact an especially made capillary cone is required to inject the PDMS into the hollow capillary.
Although many studies reported dual-parameter monitoring based on FPI structures, it is still worth continuously investigating and demonstrating the design of sensor structures, the selection of sensor materials, and the optimization of fabrication processes. Hence, in this paper, a novel FP cavity with composite structure for fiber sensing based on the multiple transfer method is proposed to measure the temperature and pressure, which possesses the advantages of proper sensitivity, simple fabrication, cost-effectiveness, and controllable cavity length.

Sensing Principle
The composite structure with dual FP cavities studied in this paper is depicted in Figure 1. The sensor consists of a single mode fiber tail and two diaphragms with different materials. the design of the interrogator's bandwidth. Another dual FPI-based fiber sensor consisting of two tiny segments of hollow-core fiber located at the end of lead-in single mode fiber, with a misalignment fusion splicing between the two hollow-core fibers with different core diameter, is reported in [13]. The proposed sensor can be used in simultaneous measurement of pressure and temperature, but its sensitivity should be significantly enhanced. Some chemical etching method-assisted FPI fabrication processes are reported in [14][15][16], which can provide good sensing performances. Unfortunately, the corrosive effects of the chemical etching and the precise etching time are difficult to control. The authors of [17,18] demonstrated easy-to-fabricate dual-FPIs. However, the sensitivity and repeatability of the fabrication for the FP cavity should be improved. By filling a hollow capillary with two sections of PDMS, which are fused to the single-mode fiber, the authors of [19] investigated a novel dual FP cavities-based fiber sensor to detect the temperature and pressure. However, the fabrication of this kind of structure is costly due to the fact an especially made capillary cone is required to inject the PDMS into the hollow capillary.
Although many studies reported dual-parameter monitoring based on FPI structures, it is still worth continuously investigating and demonstrating the design of sensor structures, the selection of sensor materials, and the optimization of fabrication processes. Hence, in this paper, a novel FP cavity with composite structure for fiber sensing based on the multiple transfer method is proposed to measure the temperature and pressure, which possesses the advantages of proper sensitivity, simple fabrication, cost-effectiveness, and controllable cavity length.

Sensing Principle
The composite structure with dual FP cavities studied in this paper is depicted in Figure 1. The sensor consists of a single mode fiber tail and two diaphragms with different materials. The formed structure is composed of three reflective surfaces. The interfaces of SMF/Material 1, Material 1/Material 2, Material 2/air, respectively, are reflective surfaces 1, 2 and 3. When light reaches the end face of the optical fiber, the incident light will be reflected by the reflective surface within a certain wavelength range. However, part of the light will still pass through Reflective Surface 1 and be reflected by Reflective Surfaces 2 and 3 within a certain range. The interference spectrum results from the phase delay caused by optical path difference and the different reflectivity of each reflection surface of the composite structure, as Formula (1) is the dual-beam interference model of the single FP cavity. and represent the reflected light intensity of the two-beam interference, is the wavelength of the incident light, is the refractive index of the FP cavity, is the length between two reflected surfaces, and is the initial phase of the inference. The formed structure is composed of three reflective surfaces. The interfaces of SMF/Material 1, Material 1/Material 2, Material 2/air, respectively, are reflective surfaces 1, 2 and 3. When light reaches the end face of the optical fiber, the incident light will be reflected by the reflective surface within a certain wavelength range. However, part of the light will still pass through Reflective Surface 1 and be reflected by Reflective Surfaces 2 and 3 within a certain range. The interference spectrum results from the phase delay caused by optical path difference and the different reflectivity of each reflection surface of the composite structure, as Formula (1) is the dual-beam interference model of the single FP cavity. I 1 and I 2 represent the reflected light intensity of the two-beam interference, λ is the wavelength of the incident light, n is the refractive index of the FP cavity, L is the length between two reflected surfaces, and ϕ 0 is the initial phase of the inference.
In this paper, an improved three-beam interference model based on the sensor structure is presented and analyzed. According to the principle of multi-beam interference, the corresponding three-beam interference intensity [20] can be described as where I 1 , I 2 , and I 3 , respectively, are the reflected light intensity at the three reflecting surfaces; ϕ 1 , ϕ 2 , and ϕ 3 are the initial phases of the reflected light; and n 1 and n 2 are the refractive index of Material 1 and Material 2, respectively.
where λ 1 , λ 2 are the wavelengths corresponding to the adjacent peaks or valleys in the temperature and pressure test interference spectrum, and L is the length of FP cavity. The optical path difference (OPD) of the reflected light l can be expressed as The wavelength spacing between adjacent peaks or valleys of the sensor interference spectrum is the free spectral range (FSR), the FSR is expressed as where the λ 1 and λ 2 are two adjacent peaks or valleys of the interference spectrum, λ 0 is the mean wavelength of λ 1 and λ 2 , and L corresponds to the cavity length in formula (3). The FSR is mainly affected by the thermal expansion coefficient (which is related to the change of L) and the thermo-optic coefficient (which is related to the change of n). It can be clearly seen that the FSR of the interference spectrum decreases as the n and L increase. For the temperature/pressure measurement of the FPI-based fiber sensor, the response of the sensor can be attributed to thermal expansion effects, thermo-optic effects, elastic deformation effects and refractive index factors. During temperature measurement, the refractive index and cavity length of the FP cavity change as the temperature increases, since these are related to the thermo-optical coefficient and the thermal expansion coefficient, respectively. This results in the variations of OPD. The OPD variation is defined as [21]    ∆l = 2∆nL + 2n∆L = 2nL(δ + α)∆T ∆n = δ∆Tn ∆L = α∆TL (6) where ∆l, ∆T, ∆n and ∆L are the variations of OPD, temperature, refractive index and FP cavity length, respectively; δ and α are the thermo-optic coefficient and thermal expansion coefficient, respectively, that are closely related to the properties of diaphragms. The formula (6) indicates that the temperature-induced OPD variations can be expressed as the change of FPI cavity length and refractive index. For the pressure measurement, the change of FPI cavity length depends on the diaphragm's elastic deformation effects, and Formula (7) shows the pressure sensing principle [22]: where ∆P, h, r, µ and E, respectively, are the change of pressure of the test environment, the thickness, the effective radius, Poisson's Ratio, Young's modulus of the diaphragms. The theoretical interference spectrum is depicted in Figure 2, which is simulated by Matlab platform. It is obtained by comprehensively considering the relevant parameters of the diaphragms, such as thermo-optical coefficient, thermal expansion coefficient, Young's modulus and Poisson's ratio in the proposed formulas. The sensitivity (S) of the prepared sensor is defined as the ratio of the wavelength shift over the corresponding temperature or pressure change. Similarly, we define the ratio of the minimum resolution ( = 20 pm) of the spectrometer (OSA) over the sensor sensitivity S as the minimum measurement accuracy ( )-and the is given by As Table 1 shows the optic and physical properties of the diaphragms, this paper fully demonstrates the different properties of materials that make up different FP cavities. The thermo-optical coefficient and thermal expansion coefficient are closely related to the temperature effect, which, respectively, affect the refractive index and the cavity length of the diaphragms. Young's modulus is the modulus of elasticity along the longitudinal direction, which also indicates the rigidity of the material. The lower Young's modulus induces the greater elastic deformation. Additionally, the tensile strength is similar to Young's modulus. Poisson's ratio effectively reflects the elastic constant of material transverse deformation. The pressure sensing characteristics of the sensors mainly rely on the Young's modulus and Poisson's ratio of the diaphragms.   The sensitivity (S) of the prepared sensor is defined as the ratio of the wavelength shift over the corresponding temperature or pressure change. Similarly, we define the ratio of the minimum resolution Ω (Ω = 20 pm) of the spectrometer (OSA) over the sensor sensitivity S as the minimum measurement accuracy (MMA)-and the MMA is given by [23]

Fabrication Process
As Table 1 shows the optic and physical properties of the diaphragms, this paper fully demonstrates the different properties of materials that make up different FP cavities. The thermo-optical coefficient and thermal expansion coefficient are closely related to the temperature effect, which, respectively, affect the refractive index and the cavity length of the diaphragms. Young's modulus is the modulus of elasticity along the longitudinal direction, which also indicates the rigidity of the material. The lower Young's modulus induces the greater elastic deformation. Additionally, the tensile strength is similar to Young's modulus. Poisson's ratio effectively reflects the elastic constant of material transverse deformation. The pressure sensing characteristics of the sensors mainly rely on the Young's modulus and Poisson's ratio of the diaphragms. Table 1. The optic and physical properties of the diaphragms [24][25][26][27][28][29].  Figure 3 illustrates the fabrication process that is divided into the five steps: (I) The standard single mode fiber (SMF1) is well cut by a fiber cleaver; (II) PDMS, Ecoflex0030 and epoxy resin AB are prepared and stored at ratios of 10:1, 1:1, and 1:1, respectively. The Material 1 is transferred to SMF2 by the multiple transfers method to form the appropriate diaphragm thickness; (III) The SMF1, SMF2 coated with Material 1 are fixed on the fiber holder. The motor is tuned, which holds SMF2, to coaxially shift the tail of SMF2 to access to the tail of SMF1, before moving it away immediately; (IV) The SMF1 is left standing or heated to make the Material 1 solidified to form the diaphragms. The Material 2 is transferred onto Material 1 by repeating steps (II) and (III); (V) The diaphragms are cured on SMF1 and a well-fabricated composite structure with dual FP cavities is completed. In addition, the diaphragm thickness can be controlled by increasing or reducing the transfer times. The multiple transfer method can also be used to increase the diaphragm thickness in batches. Consequently, we achieve a controllable cavity length of about 10-30 µm. It can be heated properly to increase the solidification of the diaphragms, which is also helpful to control the cavity length. fiber holder. The motor is tuned, which holds SMF2, to coaxially shift the ta access to the tail of SMF1, before moving it away immediately; (Ⅳ) The SMF ing or heated to make the Material 1 solidified to form the diaphragms. The transferred onto Material 1 by repeating steps (Ⅱ) and (Ⅲ); (Ⅴ) The diaphrag on SMF1 and a well-fabricated composite structure with dual FP cavities is addition, the diaphragm thickness can be controlled by increasing or reducin times. The multiple transfer method can also be used to increase the diaphra in batches. Consequently, we achieve a controllable cavity length of about can be heated properly to increase the solidification of the diaphragms, whic ful to control the cavity length.

Experimental Results and Analysis
To ensure the reliability and accuracy of the sensors, this paper carried out a comparative analysis, mainly discussing three types of composite structure, followed by -Epoxy resin AB/PDMS; -Ecoflex0030 silicone rubber/PDMS, -PDMS/Ecoflex0030 silicone rubber. The experimental results showed that the other three composite structures have poor responses to the temperature/pressure. Therefore, they are not discussed in this paper. Table 2 displays the diaphragm thickness of the above three composite ( , and ) for temperature/pressure sensing.

Experimental Results and Analysis
To ensure the reliability and accuracy of the sensors, this paper carried out a comparative analysis, mainly discussing three types of composite structure, followed by S 1 -Epoxy resin AB/PDMS; S 2 -Ecoflex0030 silicone rubber/PDMS, S 3 -PDMS/Ecoflex0030 silicone rubber. The experimental results showed that the other three composite structures have poor responses to the temperature/pressure. Therefore, they are not discussed in this paper. Table 2 displays the diaphragm thickness of the above three composite (S 1 , S 2 and S 3 ) for temperature/pressure sensing.

Temperature Sensitivity Analysis
The three samples were tested by the system shown in Figure 5. The temperature increased from 40 to 150 • C with increments of 10 • C. Meanwhile, the spectrometer persistently monitored the change of interference spectrum. The experimental results demonstrate that the measurement range of S 1 was about 40-120 • C, while S 2 and S 3 have a better temperature response around 40-130 • C, which is related to the unique properties of materials at high temperature. The stable experimental results over the range of 40-100 • C were selected for analysis.

Temperature Sensitivity Analysis
The three samples were tested by the system shown in Figure 5. The temper increased from 40 to 150 °C with increments of 10 °C. Meanwhile, the spectrometer sistently monitored the change of interference spectrum. The experimental results de strate that the measurement range of was about 40-120 °C, while and h better temperature response around 40-130 °C, which is related to the unique prop of materials at high temperature. The stable experimental results over the range of 40 °C were selected for analysis. As shown in Figure 6a, this clearly illustrates that the interference peaks exh significant wavelength shift as temperature increases; Figure 6b displays the linear f analysis of temperature response. The experimental results show that the wavelength is about 30.25 nm and the consistency of the red shift is excellent. The temperature s tivity of the sensor is about 528 pm/°C. As revealed in Figure 7a, the temperature resp of has multiple interference peaks and a significant red shift from 1525 to 1610 According to the fitting results shown in Figure 7b, the temperature sensitivity of marginally improved compared to . The wavelength shifts reach up to 32.96 nm, w clearly demonstrates relatively great fitness with a linear curve, and the calculated perature sensitivity is approximately 540 pm/°C. Figure 8a shows the interference trum of . The fitting result in Figure 8b demonstrates that the peak shift of the about 61.46 nm, and the temperature sensitivity reaches up to 1033pm/°C. Almost ex twice the amount was investigated for having high sensitivity. has the bro temperature response range and the highest temperature sensitivity in fabricated sam This is due to the fact that temperature sensitivity mainly relies on the thermal expa coefficient and thermo-optic coefficient of the diaphragms. Additionally, the spec the latter two are slightly similar to a single FP cavity. This is caused by the little d ences of refractive indexes of the two diaphragms. As shown in Figure 6a, this clearly illustrates that the interference peaks exhibit a significant wavelength shift as temperature increases; Figure 6b displays the linear fitting analysis of temperature response. The experimental results show that the wavelength shift is about 30.25 nm and the consistency of the red shift is excellent. The temperature sensitivity of the sensor is about 528 pm/ • C. As revealed in Figure 7a, the temperature response of S 2 has multiple interference peaks and a significant red shift from 1525 to 1610 nm. According to the fitting results shown in Figure 7b, the temperature sensitivity of S 2 is marginally improved compared to S 1 . The wavelength shifts reach up to 32.96 nm, which clearly demonstrates relatively great fitness with a linear curve, and the calculated temperature sensitivity is approximately 540 pm/ • C. Figure 8a shows the interference spectrum of S 3 . The fitting result in Figure 8b demonstrates that the peak shift of the S 3 is about 61.46 nm, and the temperature sensitivity reaches up to 1033pm/ • C. Almost exactly twice the amount S 3 was investigated for having high sensitivity. S 3 has the broadest temperature response range and the highest temperature sensitivity in fabricated samples. This is due to the fact that temperature sensitivity mainly relies on the thermal expansion coefficient and thermo-optic coefficient of the diaphragms. Additionally, the spectra of the latter two are slightly similar to a single FP cavity. This is caused by the little differences of refractive indexes of the two diaphragms.

Pressure Sensitivity Analysis
The schematic diagram of the pressure detection system is illustrated in Figure 9. The pressure test range is set from 100 to 400 kPa with increments of 10 kPa. The fabricated samples are placed in the air chamber and sealed with strong adhesive.  Figure 10a displays that the interference spectrum of has multiple prominent interference peaks over the detected wavelength range. The wavelength peaks increase as gas pressure increases. As described in Figure 10b, the peak shift is 4.78 nm and the fitting correlation coefficient is about 0.998. The calculated pressure sensitivity is 16.0 pm/kPa. The low sensitivity found in is due to the poor elastic effects. Figure 11a also shows the red shift of the spectra as pressure increases and the spectra present a consistent trend. In Figure 11b, the linear fitting result shows that the wavelength shift is about 10.48 nm, and the pressure sensitivity reaches up to 34.6 pm/kPa. More than twice the amount of was fabricated having a high sensitivity to . Figure 12a depicts that the has a

Pressure Sensitivity Analysis
The schematic diagram of the pressure detection system is illustrated in Figure 9. The pressure test range is set from 100 to 400 kPa with increments of 10 kPa. The fabricated samples are placed in the air chamber and sealed with strong adhesive.

Pressure Sensitivity Analysis
The schematic diagram of the pressure detection system is illustrated in Figure 9. The pressure test range is set from 100 to 400 kPa with increments of 10 kPa. The fabricated samples are placed in the air chamber and sealed with strong adhesive.  Figure 10a displays that the interference spectrum of has multiple prominent interference peaks over the detected wavelength range. The wavelength peaks increase as gas pressure increases. As described in Figure 10b, the peak shift is 4.78 nm and the fitting correlation coefficient is about 0.998. The calculated pressure sensitivity is 16.0 pm/kPa. The low sensitivity found in is due to the poor elastic effects. Figure 11a also shows the red shift of the spectra as pressure increases and the spectra present a consistent trend. In Figure 11b, the linear fitting result shows that the wavelength shift is about 10.48 nm, and the pressure sensitivity reaches up to 34.6 pm/kPa. More than twice the amount of was fabricated having a high sensitivity to . Figure 12a depicts that the has a  Figure 10a displays that the interference spectrum of S 1 has multiple prominent interference peaks over the detected wavelength range. The wavelength peaks increase as gas pressure increases. As described in Figure 10b, the peak shift is 4.78 nm and the fitting correlation coefficient R 2 is about 0.998. The calculated pressure sensitivity is 16.0 pm/kPa. The low sensitivity found in S 1 is due to the poor elastic effects. Figure 11a also shows the red shift of the spectra as pressure increases and the spectra present a consistent trend. In Figure 11b, the linear fitting result shows that the wavelength shift is about 10.48 nm, and the pressure sensitivity reaches up to 34.6 pm/kPa. More than twice the amount of S 2 was fabricated having a high sensitivity to S 1 . Figure 12a depicts that the S 3 has a marginally lower pressure sensitivity compared to its high temperature sensitivity. According to Figure 12b, after linear fitting analysis, the wavelength shift and gas pressure sensitivity are calculated to be 9.09 nm and 30.2 pm/kPa. The gas pressure sensitivity of the S 2 was the best one among the fabricated samples. The sample S 2 , which was provided with a wide measurement range, exhibits good response under high pressure.
As Table 3 shows, the performances of the proposed sensor and existing reports were concluded. The results demonstrate that the composite structures with dual FP cavities proposed in this paper possess moderate temperature and pressure sensitivity. However, we found that it is temporarily impossible to realize the simultaneous detection of the dual parameters due to the existing detection scheme and limited bandwidth of the used ASE light source. An ASE light source with a wider spectral range is needed to display more obvious three-beam interference peaks or valleys, and thus we can demodulate the high-frequency and low-frequency components to detect dual parameters simultaneously. marginally lower pressure sensitivity compared to its high temperature sensitivity. According to Figure 12b, after linear fitting analysis, the wavelength shift and gas pressure sensitivity are calculated to be 9.09 nm and 30.2 pm/kPa. The gas pressure sensitivity of the was the best one among the fabricated samples. The sample , which was provided with a wide measurement range, exhibits good response under high pressure.  marginally lower pressure sensitivity compared to its high temperature sensitivity. According to Figure 12b, after linear fitting analysis, the wavelength shift and gas pressure sensitivity are calculated to be 9.09 nm and 30.2 pm/kPa. The gas pressure sensitivity of the was the best one among the fabricated samples. The sample , which was provided with a wide measurement range, exhibits good response under high pressure. (a) (b) Figure 11. (a) The gas pressure (ranging from 100 to 400 kPa, in strides of 10 kPa) response interference spectrum of (Ecoflex0030/PDMS); and (b) pressure sensitivity of . Figure 11. (a) The gas pressure (ranging from 100 to 400 kPa, in strides of 10 kPa) response interference spectrum of S 2 (Ecoflex0030/PDMS); and (b) pressure sensitivity of S 2 . (a) (b) Figure 12. (a) The gas pressure (ranging from 100 to 400 kPa, in strides of 10 kPa) response interference spectrum of (PDMS/Ecoflex0030); and (b) pressure sensitivity of .
As Table 3 shows, the performances of the proposed sensor and existing reports were concluded. The results demonstrate that the composite structures with dual FP cavities proposed in this paper possess moderate temperature and pressure sensitivity. However, we found that it is temporarily impossible to realize the simultaneous detection of the dual parameters due to the existing detection scheme and limited bandwidth of the used ASE light source. An ASE light source with a wider spectral range is needed to display more obvious three-beam interference peaks or valleys, and thus we can demodulate the high-frequency and low-frequency components to detect dual parameters simultaneously.   In addition, as Figures 13 and 14 show, this paper also set up another experiment to verify the repeatability and stability of the sensor. Figure 14 shows the repeatability and stability of the sensors by linearly fitting the peak shift in the heating and cooling experiment. Figure 14 displays that the peak shift error over the temperature range of 60-100 • C is caused by the residual temperature under the cooling process. The fitting curves show similar slopes and a high degree of coincidence. It was proven that the dual FP cavities structure has excellent recovery capability for the thermal expansion effect and thermo-optical effect.
verify the repeatability and stability of the sensor. Figure 14 shows the repeatability and stability of the sensors by linearly fitting the peak shift in the heating and cooling experiment. Figure 14 displays that the peak shift error over the temperature range of 60-100 °C is caused by the residual temperature under the cooling process. The fitting curves show similar slopes and a high degree of coincidence. It was proven that the dual FP cavities structure has excellent recovery capability for the thermal expansion effect and thermooptical effect.

Conclusions
In this paper, a novel composite structure composed of dual FP cavities for fiber sensing based on the multiple transfer method was proposed to measure the temperature and verify the repeatability and stability of the sensor. Figure 14 shows the repeatability and stability of the sensors by linearly fitting the peak shift in the heating and cooling experiment. Figure 14 displays that the peak shift error over the temperature range of 60-100 °C is caused by the residual temperature under the cooling process. The fitting curves show similar slopes and a high degree of coincidence. It was proven that the dual FP cavities structure has excellent recovery capability for the thermal expansion effect and thermooptical effect.

Conclusions
In this paper, a novel composite structure composed of dual FP cavities for fiber sensing based on the multiple transfer method was proposed to measure the temperature and

Conclusions
In this paper, a novel composite structure composed of dual FP cavities for fiber sensing based on the multiple transfer method was proposed to measure the temperature and pressure, which possesses the advantages of proper sensitivity, simple fabrication, costeffectiveness, and controllable cavity length. It was proven that the measured temperature or pressure sensitivity was closely related to the properties and combination modes of the diaphragms. According to the experimental results, by optimizing the combinations and parameters of dual-diaphragms, this study found that the temperature or pressure sensitivity can be adjusted over a certain range within the test temperature range of 40-100 • C and a pressure range of 100-400 kPa. This shows that the composite structure designed with dual FP cavities in this study has a proper sensitivity and can meet various sensitivity-demanding application scenarios.

Data Availability Statement:
The data that support the findings of this study are available from the corresponding author upon reasonable request.