Super-hydrophobic material and vibrating deicing coupled active and passive anti-icing device and method

An anti-icing device, super-hydrophobic technology, applied in the direction of de-icing devices, chemical instruments and methods, fluids using vibration, etc., can solve the problems of incomplete de-icing and the inability to prevent the icing of aircraft parts, and achieve good adaptability , a wide range of effects

Active Publication Date: 2017-09-05
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
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AI Technical Summary

Problems solved by technology

[0008] The purpose of the present invention is to provide a coupling of superhydrophobic material and vibration deicing for the problem that the surface of aircraft components cannot be completely iced by relying solely on the superhydrophobic surface, and the traditional mechanical deicing method has the problem of incomplete deicing. Active and passive anti-icing device and method thereof

Method used

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  • Super-hydrophobic material and vibrating deicing coupled active and passive anti-icing device and method
  • Super-hydrophobic material and vibrating deicing coupled active and passive anti-icing device and method

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Embodiment 1

[0055] As shown in the figure, the device of this embodiment includes a hydrophobic material film for being arranged on the surface of the anti-icing object, a flexible piezoelectric fiber film, an acceleration sensor for measuring the vibration of the flexible piezoelectric fiber film, a dynamic analysis module, and a function generator. A device, a power amplifier, a power supply, a flexible piezoelectric fiber film and a hydrophobic material film are bonded together, and the flexible piezoelectric fiber film is located between the anti-icing object and the hydrophobic material film. The anti-icing objects aimed at by the present invention can be the wings and empennages of various types of aircraft (including but not limited to helicopters, rotorcraft, and fixed-wing aircraft), and can also be anti-icing components such as wind turbine blades, power transmission wires, and high-speed trains. Take an airplane wing as an example.

[0056] Such as figure 2 As shown, the hydr...

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Abstract

The invention discloses a super-hydrophobic material and vibration deicing coupled active and passive anti-icing device and method. The device and method aim to solve the problems that the icing phenomenon of the surface of an aircraft part cannot be completely eradicated only by means of a super-hydrophobic surface, and deicing is not thorough through a traditional mechanical deicing method. The device comprises a hydrophobic material thin film, a flexible piezoelectric fiber thin film, an acceleration sensor, a dynamic analysis module, a function generator, a power amplifier and a power source, wherein the acceleration sensor is used for measuring the vibration of the flexible piezoelectric fiber thin film. According to experiment simulation environments and icing meteorological conditions under a real atmospheric environment, the hydrophobic material thin film and the flexible piezoelectric fiber thin film are used and matched with each other, and by means of vibration control over on the flexible piezoelectric fiber thin film, the purpose of low-energy-consumption deicing is achieved. The device can be used for surface deicing treatment of various airplanes, wind turbines, high-speed trains, electric transmission lines and other easily-frozen parts, and is wide in application range, high in value, good in prospect and worthy of large-scale popularization and application.

Description

technical field [0001] The invention relates to the field of anti-icing, in particular to the field of anti-icing equipment and methods, in particular to an active and passive anti-icing device coupled with superhydrophobic materials and vibration deicing and a method thereof. The invention provides a device and method capable of carrying out low energy consumption anti-icing on anti-icing objects under icing weather conditions, which can be used for aircraft (including rotorcraft, Helicopter, fixed-wing aircraft (wings and empennages), wings, empennages, wind turbine blades, power transmission wires and high-speed trains and other anti-icing components with low energy consumption have high application value and good application prospects. Background technique [0002] Icing is a physical phenomenon that widely exists in flight practice, and it is one of the main hidden dangers of flight safety accidents. When the aircraft flies under the ambient temperature below the freez...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B08B7/02B06B1/06B06B3/02H02G7/16B64D15/16
CPCH02G7/16B64D15/16B06B1/0603B06B3/02B08B7/026B06B2201/55Y02E10/72
Inventor 肖春华梁鉴倪章松赖庆仁刘蓓
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
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