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ADVANCED ENGINEERING MATERIALS · 2021 ·Vol. 23 ·期 10 ·2100347 · IF 3.862

A Superhydrophobic Self-Cleaning and Anti-Icing Aluminum Sheet Fabricated by Alkaline Solution

Jialu Zhang,Hao Xu,Jie Guo,Yingying Zhang,Tianchi Chen

The aerospace industry has extremely strict requirements for metal materials, especially the stability of the material at a low temperature and in harsh environment. Herein, superhydrophobic anti-icing aluminum sheets are fabricated with traditional hydrothermal reaction and modified by (heptadecafluoro-1,1,2,2-tetradecyl) triethoxysilane (AC-FAS). Field-Emission Scanning Electron Microscope (SEM), Fourier transform infrared spectroscopy (FTIR), and X-ray photoelectron spectroscopy (XPS) are used to analyze the surface morphology and chemical compositions. The satisfactory properties of superhydrophobicity and anti-icing result from its dense microcosmic array structure and its low surface energy. The prepared superhydrophobic aluminum surface can realize wettability alteration, in which the contact angle increases from 118° on the original aluminum sheets to 155° with a rolling angle of 10°. In addition, the prepared superhydrophobic surface has anti-icing and self-cleaning ability. According to the aforementioned results, it is believed that the superhydrophobic aluminum sheets can be an excellent candidate in the aerospace field.

研究领域: 材料科学 · 表面工程
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ACS Applied Nano Materials · 2021 · IF 5.097

Nanoporous Polybenzoxazine Aerogels for Thermally Insulating and Self-Extinguishing Materials in Aerospace Applications

Shixian Xiong,Yue Yang,Sizhao Zhang,Yunyun Xiao,Hui Ji,Zhouyuan Yang,Feng Ding

Phenolic-based aerogel composites possess particular characteristics, such as low thermal conductivity, light weight, and superior ablative properties, in near-space vehicles. However, their machinability and flammability require further improvement, hampering their application for high-performance thermal protection systems in the aerospace field. Here, we prepare nanoporous polybenzoxazine (PBO) aerogels with outstanding thermally insulating and self-extinguishing properties by an effective-cost ambient pressure drying (APD) approach rather than a conventional high-pressure supercritical drying pattern. The PBO aerogels are prepared by adopting different exchange solvents of tert-butyl alcohol, ethanol, and n-hexane. The results obtained indicate that PBO aerogels (with n-hexane as the exchange solvent) by APD have an optimal three-dimensional nanoporous network structure, a pore size distribution in the range 20–140 nm, an obvious self-extinguishing property (extinguished itself instantly despite exposure to a 1200 °C flame), superior thermal insulation (the cold surface temperature of the sample reached only 36.4 °C after 400 s despite its opposite surface existing at a 65.8 °C atmosphere), and excellent machinable properties (easy-to-form special-shaped sample). PBO aerogels are a great potential candidate material system for thermal protection systems in aerospace applications in the future.

研究领域: 材料科学 · 航天工程
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NUCLEAR INSTRUMENTS & METHODS IN PHYSICS RESEARCH SECTION B-BEAM INTERACTIONS WITH MATERIALS AND ATOMS · 2022 · IF 1.279

Preparation of antistatic AZO/Al2O3-ZnO-Y2O3 composite thermal control coating and its study on electron-resistance radiation performance

Tao Li,Hongjun Kang,Songtao Lu,Wei Qin,Xiaohong Wu

As space exploration moves further and further into deep space, it is a big challenge to develop antistatic inorganic thermal control coating with lightweight and strong adhesion to substrates. Herein, this work reported an inorganic antistatic AZO/Al 2 O 3 -ZnO-Y 2 O 3 composite coating fabricated by PEO combined with ALD methods. The results show that when the Zn/Al ratio of deposited AZO film is 24:1, its overall performance is the optimal, and the emissivity, absorptivity and resistivity are 0.892, 0.409 and 1.15 × 10 –3  Ω·cm, respectively, which can meet thermal control application requirements of spacecraft. Furthermore, the AZO/Al 2 O 3 -ZnO-Y 2 O 3 composite coating shows a good electron-resistance irradiation performance, which is because AZO conductive film is easy to generate free carriers, speed up some electron transport and make electrons better disperse and conduct, thus reducing the penetration depth of electron irradiation. This work provides a material basis for thermal control system of spacecraft with long life and high reliability.

CAS / MDL: 1310-58-3 10361-93-0
研究领域: 材料科学 · 航天工程
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APPLIED SURFACE SCIENCE · 2025 · IF 6.9

Exploring the distinct lubrication mechanisms of functionalized ionic liquids in air and vacuum: Insights into molecular-level behavior and performance

Guanai Qu,Lei Liu,Hongling Fang,Yi Li,Songwei Zhang,Litian Hu

The rapid advancement of the aerospace industry is driving progress in space tribology, with ionic liquids (ILs) emerging as promising lubricants due to their low vapor pressure and superior properties. However, understanding ILs’ lubrication mechanisms in vacuum conditions often depends on extrapolations from atmospheric experiments, raising questions about their consistent behavior across environments. The study explores the lubrication properties of several halogen-free, functionalized oxygen-containing ILs under air and vacuum conditions by using in-situ quadrupole mass spectrometry and molecular dynamics simulations. Results reveal significant differences in their lubricating performance and mechanisms across environments, highlighting the complexity and environmental dependence of their tribological behavior, which is crucial for designing advanced lubricants for extreme conditions.

CAS / MDL: 1934-75-4
研究领域: 材料科学 · 空间 tribology · 化学工程
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ACS Applied Materials & Interfaces · 2019 · IF 8.456

Synthesis of UV-Responsive Self-Healing Microcapsules and Their Potential Application in Aerospace Coatings

Yuye Zhu,Kangli Cao,Min Chen,Limin Wu

Advanced polymer composite coatings in the spacecraft are threatened by harsh space environment factors, such as strong UV radiation, atomic oxygen, thermal cycles, space debris, etc. Their service life can be drastically shortened by the unavoidable formation of cracks caused by these factors (especially strong and abundant UV radiation) during long-term flight. Herein, a UV-responsive microcapsule-based coating is developed for in-orbit damage repairing. UV-responsive microcapsules of which the inner polymeric shell can be degraded rapidly by the outer pure TiO2 shell under UV radiation are produced by UV-initiated polymerization of Pickering emulsions and subsequently embedded into silicon resin matrices. When damaged, some microcapsules will be ruptured under the stimulus of external force, afterward the unbroken ones around the scratched areas will be degraded by UV radiation, as a result, encapsulated healing agents can be released and finally repair cracks. In this system, UV-responsive microcapsules can release more agents more effectively due to the dual release mode, compared with the traditional crack-repairing system. Moreover, the damage of UV radiation in space can be transferred into the favorable ones, which makes it have a potential application in aerospace coatings.

研究领域: 材料科学 · 航空航天工程 · 高分子化学
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ADVANCED FUNCTIONAL MATERIALS · 2022 ·Vol. 32 ·期 46 ·2207239 · IF 19.924

Scalable-Manufactured Plasmonic Metamaterial with Omnidirectional Absorption Bandwidth across Visible to Far-Infrared

Yang Li,Zhequn Huang,Yafen Xu,Heng Zhang,Qixiang Wang,Huaxu Qiao,Wen Shang,Tao Deng,Kehang Cui

Broadband, omnidirectional light absorption in the infrared range is critical for emerging aerospace and ground applications, such as machine vision, autonomous vehicle technology, and aerospace telescope. Broadband absorbers (BBAs) need to possess strong absorption through thin structures for high signal-to-noise ratios, as well as manufacturing scalability and service reliability in harsh environment for practical applications. Such requirements rule out many known absorbing materials such as carbon nanotubes that are intrinsically lossy and fragile. Achieving strong light-matter interaction in the mid- and long-wavelength infrared ranges has been extremely challenging despite long-standing research efforts. Here, an aerospace-grade, ≈2.0 µm-thick hierarchical coral-structured titanium nitride (coral-TiN) plasmonic metamaterial is experimentally realized with over 90% omnidirectional absorption across the visible to the long-wavelength infrared range (0.25–25 µm) using a scalable fabrication method. The broadband optical control of the coral-TiN BBA is achieved by the superposition of the hybridized plasmonic mode in the visible and near-infrared, the cavity mode in the short-wavelength infrared as well as the propagating surface plasmon polariton mode in the mid- and long-wavelength infrared. With conformal alumina coating, the plasmonic absorber demonstrates outstanding reliability in rigorous aerospace-grade tests under harsh mechanical and thermal environmental conditions.

CAS / MDL: 10125-13-0
研究领域: 光学 · 材料科学 · 纳米技术
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FUEL PROCESSING TECHNOLOGY · 2022 · IF 8.129

Synthesis of caged high-energy-density fuel as potential high-performance energetic additive for liquid aerospace fuel

Shuang Ma,Ying Chen,Xianlong Liu,Lun Pan,Xiangwen Zhang,Ji-Jun Zou

High-energy-density (HED) fuels have drawn substantial attention for volume-limited aerospace vehicles because they can provide high propulsion energy. Herein, we report a route for synthesis of HED fuel pentacyclo[5.3.0.0 2,5 .0 3,9 .0 4,8 ]decane (PCD) with strained structure by photoinduced intramolecular [2 + 2] cycloaddition of dicyclopentadiene (DCPD). The reaction conditions, like photosensitizer , solvent, concentration, temperature and light intensity , were optimized for achieving the best photochemical performance, with the high DCPD conversion of 95.89% and high PCD selectivity of 62.08%. The triplet quenching and phosphorescence quenching results show that DCPD cycloaddition proceeds under the photosensitizer photoexcitation , triplet-triplet energy transfer, cyclization and relaxation. Moreover, a reaction kinetic model is established with the reaction rate constant being correlated with light intensity, with the pseudo reaction kinetics parameters and reaction rate equations obtained. As a caged fuel, PCD possesses both high density (1.066 g/cm 3 ) and high volumetric neat heat of combustion (44.43 MJ/L), which is very promising to blend with current high density liquid fuels to obtain high-performance fuels for practical application.

研究领域: 化学 · 材料科学 · 能源科学
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JOURNAL OF ALLOYS AND COMPOUNDS · 2022 · IF 6.371

In-situ formed intergranular TiB2 into lightweight SiC(rGO) composite PDCs enable elevated temperature resistance for aerospace components

Wenyan Huang,Zhichao Xue,Lingjie Li,Shengjian Mao,Yufeng Wang,Yeqi Zhu,Tao Luo,Qianwen Tao,Rongqian Yao

Strengthening interface bonding for superior mechanical/ablation performances of SiC-based aerospace vehicle components remains a major challenge. Attractively, polycarbosilane-vinyltriethoxysilane-graphene oxide with addition of TiN/B (PVG(TiN, B)) were successfully synthesized for the first time. An ingenious route via re-pyrolyzing ball-milling-induced SiC(rGO, TiB 2 ) p fillers/PVG(TiN, B) precursors blends was introduced to prepare lightweight SiC(rGO, TiB 2 ) composite polymer-derived ceramics (PDCs). Interestingly, both SiC(rGO, TiB 2 ) p and PVG(TiN, B) pyrolysis products, composed of β-SiC/SiO x C y /C free (rGO, TiB 2 ), are tightly coupled by each other owing to plentiful Si-dangling bonds. In-situ formed intergranular TiB 2 /B 4 C, well compatible with amorphous ceramic network, can prevent β-SiC grain growth, strengthen interface bonding, and even hinder further crack propagation along the grain boundaries. Particularly, samples re-pyrolyzed at 1300 °C possess unique combination of good hardness (5.44 GPa), excellent fracture toughness (4.70 MPa·m 1/2 ), high flexural strength (41.90 MPa) and outstanding compressive strength (126.33 MPa). Improved high-temperature and ablation resistance gives them distinct advantages of interlocked microstructure under exposure of butane flame. As demonstrated, SiC(rGO, TiB 2 ) composite PDCs were developed into porous ceramics with good thermal insulation , focusing on manufacturing large-size bulk PDCs for thermal protection system of hypersonic vehicles.

研究领域: 材料科学 · 航空航天工程
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MATERIALS CHEMISTRY AND PHYSICS · 2025 · IF 4.7

Thermally stable, robust, superhydrophobic coating based on hydrophobic/hydrophilic dual-size particles

Weiwei Zhang,Huaxia Wang,Huicong Liu,Xianwei Zhao,Pei Li,Liqun Zhu,Haining Chen,Weiping Li

Superhydrophobic coatings have garnered significant attention in the aerospace industry due to their unique functionalities. However, most reported coatings are restricted by poor thermal stability (typically below 400 °C), complex fabrication processes, or reliance on fluorinated raw materials, which limit their practical applications. This study employs a fluorine-free water-based acrylic/organosilicon composite resin and dual-scale SiO2/ZrO2 particles to prepare a high-temperature-resistant superhydrophobic coating. The coating exhibits a water contact angle (WCA) of 156.1° and a sliding angle (SA) of 6.9°. Additionally, it maintains good hydrophobicity even after being treated at 500°C for 1 hour. In addition, the coating demonstrates excellent multifunctional durability, including resistance to 200 abrasion cycles, electrolyte corrosion, acid–base solutions, and common organic solvents. Benefiting from its environmentally friendly composition and simple spray-coating process, this work provides a scalable strategy for fabricating robust superhydrophobic coatings tailored for demanding aerospace environments.

CAS / MDL: 144-55-8
研究领域: 材料科学 · 表面工程 · 航空航天工程 · 纳米技术
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FUEL PROCESSING TECHNOLOGY · 2021 · IF 7.033

Synthesis and comprehensive fuel properties of mono-substituted alkyl adamantanes for advanced aerospace propulsion

Jiawei Xie,Chengxiang Shi,Yunxiao Zhao,Lun Pan,Xiangwen Zhang,Ji-Jun Zou

Design and choice of fuels continue to be improved for aviation propulsion, and alkyl adamantanes have attracted great attention due to their high density, good low-temperature properties and potential characteristics. Herein, we reported a facile route to synthesize mono-substituted alkyl adamantanes via modified Grignard coupling (followed with one-step hydrodeoxygenation), including 1-ethyl-adamantane, 2-ethyl-adamantane, and 1- n -propyl-adamantane with high yields (> 75%). The process was modified via concentrating the Grignard reagents and altering the solvent, and one-step hydrodeoxygenation catalyzed by commercial Pd/C and zeolites was developed. Subsequently, comprehensive characteristics of alkyl diamondoid series, such as oxidation stability and combustion properties , were evaluated using pressure differential scanning calorimetry , rapid small-scale oxidation test, and hot-plate ignition test. Also, the specific impulse of alkyl diamondoids were revealed by theoretical calculation. The high-density alkyl diamondoids present adequate oxidation stability and possess better combustion characteristics over JP-10, thus can be considered as potential high-energy-density fuel for aerospace propulsion .

研究领域: 化学工程 · 能源科学 · 材料科学
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CRYSTENGCOMM · 2022 ·Vol. 24 ·期 10 ·1859-1865 · IF 3.756

Flexible Al2O3/ZrO2 nanofibrous membranes for thermal insulation

Shouzhen Li,Fan Wu,Xuan Zhang,Guangting Han,Yang Si,Jianyong Yu,Bin Ding

Developing ceramic materials for thermal insulation is vital for various applications. However, ceramics have been considered intrinsically rigid and brittle due to the limited crystallographic slips and structural collapse during service. Their lack of flexibility has hampered many high-end applications of ceramic materials. We developed flexible Al2O3/ZrO2 nanofibrous membranes via sol–gel electrospinning and calcination. Al2O3/ZrO2 nanofibrous membranes had flexibility from −196 °C to 1300 °C and low thermal conductivity (∼0.03166 W m−1 K−1 at room temperature). They also supported 1350-times their weight without suffering structual damage. Hence, Al2O3/ZrO2 nanofibrous membranes could be used for thermal insulation in aerospace and industrial fields, and even in harsh environments.

研究领域: 材料科学 · 热工程 · 纳米技术
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Polymer Chemistry · 2023 ·Vol. 14 ·期 19 ·2317-2325 · IF 4.6

High-performance boron-containing phthalonitrile resins

Wenjing Kong,Jiaqi Sun,Muyao Gao,Tianhao Li,Ming Liu,Yujie Song

Phthalonitrile resins as a unique class of high-performance materials have attracted increasing interest in wide application fields including aerospace, electronic packaging and flame-retardant materials. In this article, the boron element was incorporated into phthalonitrile resins to improve the processibility and thermal stability. The synthetic borate and aryl borate-modified resorcinol-based phthalonitrile monomers (BPN and PBPN) showed lower melting points than traditionally employed RPN. The presence of hydroxyl groups leads to autocatalytic curing behavior of BPN and PBPN. Due to the presence of the boron-branched structures in the polymer backbone of the modified phthalonitrile resins, these resins exhibited better thermal stability than traditionally investigated RPN and their mechanical properties are stable over a wide temperature range, which is crucial in service under harsh environments. The results suggest that boron-modified phthalonitrile resins possess great potential in the field of high-temperature resistant materials.

研究领域: 材料科学 · 化学工程 · 航空航天工程 · 高分子科学
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