Epoxy coatings are extensively used for corrosion protection of metallic substrates because of their excellent film-forming capability,high adhesion,and favorable mechanical properties. However,in harsh marine environments,their long-term service stability is often limited by micro defects generated during the curing process,the water absorption behavior of polar resin networks,and the subsequent continuous penetration of chloride ions,oxygen,and water molecules into the coating/substrate interface. To address these limitations,an epoxy composite coating system containing a tannic acid-modified bismuth-based metal-organic framework (TA-BiMOF) as a multifunctional filler was developed,aiming to simultaneously enhance the mechanical stability and long-term anti-corrosion performance of the coating.
TA-BiMOF was synthesized through a mild room-temperature solution route and systematically characterized by scanning electron microscopy (SEM),energy dispersive spectrometry (EDS),X-ray photoelectron spectroscopy (XPS),Fourier-transform infrared spectroscopy(FT-IR),X-ray diffraction (XRD),Raman spectroscopy,N2 adsorption-desorption,and thermogravimetric analysis. The results confirmed that tannic acid modification preserved the primary framework structure of BiMOF while regulating crystal growth,suppressing agglomeration,and enriching the particle surface with oxygen-containing functional groups. Compared with pristine BiMOF,TA-BiMOF showed a more homogeneous and refined morphology,and its elemental composition changed from 18.14%(mass fraction,the same below) C,8.18% O,and 73.05% Bi to 20.31% C,11.06% O,and 68.62% Bi,indicating successful tannic acid incorporation. XPS analysis further revealed an approximately 0.3 eV positive shift in the Bi 4f peaks,suggesting altered coordination environments around Bi sites after polyphenol modification. In addition,tannic acid significantly optimized the pore characteristics of the framework:the Brunauer-Emmett-Teller (BET) specific surface area of TA-BiMOF increased from 194.68 to 321.74 m2/g,whereas the average pore diameter decreased from 5.38 to 2.91 nm,and the microporous surface area reached 277.98 m2/g with a micropore volume of0.11 cm3/g. These changes indicate that TA-BiMOF possesses a finer and more developed porous architecture,which is beneficial for strengthening matrix-filler interactions and increasing the tortuosity of diffusion pathways for corrosive species. Thermogravimetric analysis also showed that TA-BiMOF exhibited continuous mass loss over a broader temperature range than BiMOF,indicating that tannic acid modification altered the thermal decomposition behavior of BiMOF and broadened its massloss temperature range.
The modified filler was then incorporated into epoxy at a loading of 1% to fabricate TA-BiMOF/EP composite coatings,while neat epoxy and BiMOF/EP coatings were prepared as controls under identical conditions. The SEM results of the cross-section after liquid nitrogen embrittlement showed that the pure EP coating had a relatively flat cross-section and typical brittle fracture characteristics,with irregular micropores and local defects inside,whereas BiMOF/EP displayed increased roughness but also obvious interfacial gaps and local particle aggregation,reflecting insufficient compatibility between unmodified BiMOF and the epoxy matrix. In contrast,TA-BiMOF/EP exhibited a much denser microstructure and a more compact filler/matrix interface without obvious debonding features,demonstrating that tannic acid effectively improved filler dispersion and interfacial compatibility. This microstructural optimization directly translated into improved surface and mechanical properties. The static water contact angle of TA-BiMOF/EP coating increased from 59.5°of pure EP to 74.5°,significantly higher than the 69.1°of BiMOF/EP,indicating a decrease in surface wettability and an enhancement in resistance to water infiltration. The pull-off adhesion strength increased from 10.21 MPa for neat EP to 14.84 MPa for BiMOF/EP and 14.00 MPa for TA-BiMOF/EP,corresponding to a 37.1%increase for the TA-BiMOF-filled coating relative to the unfilled system. Tensile testing revealed a pronounced difference between unmodified and modified filler effects. Although pristine BiMOF increased stiffness,it also caused premature failure,reducing the tensile strength to approximately 45 MPa and the elongation at break to about 2.5%,indicating severe stress concentration arising from poor interfacial compatibility. By contrast,TA-BiMOF/EP achieved the best balance of strength and ductility,with a tensile strength of 71.8 MPa,representing a 19.7% increase over neat EP (~60 MPa),while maintaining an elongation at break of about 6%,exhibiting the best balance of strength and toughness. These results indicate that tannic acid modification enables more efficient stress transfer across the filler/matrix interface and mitigates the embrittlement typically associated with rigid particulate fillers. The anti-corrosion performance of the coatings was evaluated by electrochemical impedance spectroscopy in 3.5% NaCl solution during immersion for up to 70 d. Neat EP showed rapid electrochemical degradation,as evidenced by a strong shrinkage of the Nyquist capacitive arc,a decrease in low-frequency impedance modulus to 9.55×107 Ω·cm2 after70 d,and a concomitant increase in coating capacitance to 7.76×10-9 F/cm2,indicating severe water uptake and loss of barrier integrity. In contrast,BiMOF/EP maintained a much higher low-frequency impedance of6.92×1010 Ω·cm2 and a much lower coating capacitance of2.00×10-11 F/cm2 after 70 d,confirming that the introduction of MOF particles effectively retarded electrolyte penetration by increasing diffusion-path tortuosity. TA-Bi-MOF/EP maintained a stable electrochemical response throughout the entire immersion period. Its Nyquist plots remained highly overlapped over time,and the low-frequency phase angle stayed close to 90°,indicating persistent capacitive behavior and excellent coating integrity. After 70 d of saline exposure,TA-BiMOF/EP still retained a low-frequency impedance modulus of4.79×1010 Ω·cm2 and a low coating capacitance of 1.62×10-11 F/cm2,with its low-frequency impedance being approximately 2.7 orders of magnitude higher than that of neat EP. Equivalentcircuit fitting further showed that TA-BiMOF/EP maintained the highest charge-transfer resistance throughout the test period,confirming the most effective suppression of interfacial corrosion reactions. Post-immersion substrate characterization after coating delamination further corroborated the electrochemical results. Severe underfilm corrosion,abundant corrosion products,and obvious pitting were observed on the steel surface beneath neat EP,accompanied by an oxygen content of 14.8%(atomic fraction,the same below) and a small amount of chlorine. Bi-MOF/EP offered partial protection,preserving a relatively smooth substrate with only minor discoloration and an oxygen content of 1.7%. Notably,the steel protected by TA-BiMOF/EP retained a bright metallic appearance with clear grinding marks,a Fe content of85.5%,and no detectable oxygen,indicating that corrosion was nearly completely suppressed during prolonged immersion.
The superior performance of TA-BiMOF/EP can therefore be attributed to the synergistic integration of multiple mechanisms,including MOF-induced tortuous diffusion pathways for physical barrier enhancement,tannic acid-mediated interfacial strengthening between filler and epoxy matrix,reduced curing-induced microdefects through improved filler dispersion,and possible metal-chelation-assisted passivation by the polyphenolic groups of tannic acid. Overall,this work demonstrated that tannic acid functionalization was an effective strategy for tailoring Bi-MOF toward high-performance epoxy anti-corrosion coatings,offering a viable materials design route for constructing mechanically reinforced and electrochemically durable protective systems for marine metallic infrastructure.
Titanium alloys and high-temperature alloys are core materials in aerospace engineering,widely used in aero-engine transmission components such as end teeth and splines,which operate under harsh conditions of high temperature,high pressure,high speed,and severe wear. Fretting wear is a major cause of failure for these components,seriously affecting their service life and reliability. Under extreme conditions like high temperature and load,the fretting wear behavior of materials becomes more complex,imposing stricter requirements on material performance. Key factors influencing titanium alloy fretting wear include frequency,displacement amplitude,normal load,and ambient temperature. This study aimed to investigate the effect of different normal loads on the fretting wear performance of titanium alloy-high-temperature alloy friction mating pairs at 500 ℃,reveal the underlying wear mechanisms,and provide theoretical data and practical references for the antifretting damage design of aerospace components.
Cylindrical specimens of titanium alloy (18 mm×20 mm) and high-temperature alloy (18 mm×21 mm) were selected. All specimens underwent standardized grinding,polishing,cleaning,and drying to ensure no oil,rust,or impurities,with consistent initial surface roughness.Their key physical and mechanical properties are as follows:titanium alloy has a tensile strength of 1 130 MPa,yield strength of885 MPa,elastic modulus of 120 GPa,Poisson’ s ratio of0.33,density of4.48 g/cm3,and elongation of 8%;high-temperature alloy exhibits a tensile strength of 1 654 MPa,yield strength of 1 321 MPa,elastic modulus of 218 GPa,Poisson’ s ratio of0.29,density of 8.3 g/cm3,and elongation of 16.4%.
Fretting wear tests were conducted using a tangential fretting wear tester. Normal load was applied via a voice coil motor-driven electric cylinder with closed-loop compensation,and horizontal displacement was provided by another voice coil motor with grating sensor feedback. The ambient temperature and humidity were constant,and a program-controlled heating mode ensured the specimens stably reached 500 ℃. Test parameters included normal loads of200,210 N,and 230 N,displacement amplitude of20 μm,frequency of4 Hz,cycle number of 10 000, and cylinder-on-cylinder orthogonal contact. After testing,scanning electron microscopy (SEM) was used for wear-scar morphology analysis, energy-dispersive spectroscopy (EDS) for elemental-distribution characterization,and a white-light interferometer for three-dimensional (3D) morphology characterization. Results showed that increasing normal load significantly altered the fretting behavior of the friction pair. At 200 N and 210 N,the friction displacement (F-D) curves exhibited a typical parallelogram shape (slip regime) with distinct loading,slipping,unloading,and reverse slip ping stages,stable friction force plateaus,and complete relative slip. At 230 N,the curve transformed into an elliptical shape (partial slip regime) without obvious plateaus,with only slight edge slip and central adhesion. The parallelogram curve at 210 N was narrower than at 200 N, indicating weakened relative slip with increasing load. The friction coefficient (the ratio of frictional force to normal load) gradually decreased with increasing load:1.00 at 200 N,0.60 at 210 N,and 0.55 at 230 N,with the stabilization time shortening sequentially (ta>tb>tc).3D morphology and SEM observations revealed more severe damage to titanium alloy than high-temperature alloy at 200 N and 210 N,with wear debris accumulation and adhesion features on the latter. At 230 N,only slight edge damage was observed,with a flat scar center and minimal material loss. Micro-morphologically,slight plowing marks,debris accumulation,and spalling were seen at 200 N and 210 N (indicating fatigue and adhesive wear),while 230 N showed only slight scratches and mild fatigue wear. EDS analysis indicated full-area O element distribution at 200 N and 210 N (confirming oxidative wear),with Ti detected on high-tem perature alloy scars and Ni,Cr,Co on titanium alloy scars (indicating element migration and transfer film formation). At 230 N,O was only slightly distributed at edges,and element migration weakened significantly. The wear mechanism evolved from the synergy of adhesive,fatigue, and oxidative wear at 200 N and 210 N to mild fatigue and weak oxidative wear at 230 N. This study systematically investigated the fretting wear performance of titanium alloy-high-temperature alloy friction mating pairs under dif ferent normal loads at 500 ℃. As the load increased from 200 N to 230 N,the friction coefficient decreased,the fretting regime shifted from slip to partial slip,and material damage was significantly reduced. The wear mechanism transitioned from dominant adhesive wear with syner gistic fatigue and oxidative wear at lower loads to mild fatigue and weak oxidative wear at higher loads,attributed to suppressed relative slip and reduced oxygen penetration under high loads. These findings provided critical theoretical data and practical guidance for the anti-fretting design of aerospace components,and offered valuable references for tribological research on high-performance alloy pairs under extreme temperature and load conditions.