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Study on the Thermal Degradation Behavior of FKM O-rings

  • Lee, Jin Hyok (Department of Polymer Engineering, Pusan National University) ;
  • Bae, Jong Woo (Rubber Research Team, Korea Institute of Footwear & Leather Technology) ;
  • Choi, Myoung Chan (Rubber Research Team, Korea Institute of Footwear & Leather Technology) ;
  • Yoon, Yoo-Mi (Rubber Research Team, Korea Institute of Footwear & Leather Technology) ;
  • Park, Sung Han (Agency for Defense Development) ;
  • Jo, Nam-Ju (Department of Polymer Engineering, Pusan National University)
  • Received : 2018.11.13
  • Accepted : 2018.11.23
  • Published : 2018.12.31

Abstract

The degradation mechanism and physical properties of an FKM O-ring were observed with thermal aging in this experiment. From X-ray photoelectron spectroscopy (XPS) analysis, we could observe carbon (285 eV), fluoro (688 eV), and oxygen (531 eV) peaks. Before thermal aging, the concentration of fluoro atoms was 51.23%, which decreased to 8.29% after thermal aging. The concentration of oxygen atoms increased from 3.16% to 20.39%. Under thermal aging, the FKM O-ring exhibited debonding of the fluoro-bond by oxidation. Analysis of the C1s, O1s, and F1s peaks revealed that the degradation reaction usually occurred at the C-F, C-F2, and C-F3 bonds, and generated a carboxyl group (-COOH) by oxidation. Due to the debonding reaction and decreasing mobility, the glass transition temperature of the FKM O-ring increased from $-15.91^{\circ}C$ to $-13.79^{\circ}C$. From the intermittent CSR test, the initial sealing force was 2,149.6 N, which decreased to 1,156.2 N after thermal aging. Thus, under thermal aging, the sealing force decreased to 46.2%, compared with its initial state. This phenomenon was caused by the debonding reaction and decreasing mobility of the FKM O-ring. The S-S curve exhibited a 50% increase in modulus, with break at a low strain and stress state. This was also attributed to the decreasing mobility due to thermal aging degradation.

Keywords

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Scheme 1. Chemical structure of FKM rubber

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Scheme 2. Intermittent CSR jig

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Figure 1. XPS spectra of FKM O-ring; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

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Figure 2. XPS spectra, C1s level of FKM O-ring; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

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Figure 3. XPS spectra, O1s level of FKM O-ring; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

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Figure 4. XPS spectra, F1s level of FKM O-ring; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

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Figure 5. DSC analysis result of FKM O-rings; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

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Figure 6. Load vs. displacement of FKM O-ring by intermittent CSR test method; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

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Figure 7. Strain/stress curve of FKM O-ring; (a) non-treated, (b) thermal aging treated (170℃, 24 days).

Table 1. The Formulation of FKM O-ring

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Table 2. Atomic Concentration (%) of the Different Elements Consisting the FKM O-ring According to Thermal Aging at Atmosphere

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