3results about How to "Good wave permeability" patented technology

The invention relates to the technical field of aircrafts, in particular to a composite material rudder wing structure for an aircraft and a preparation method thereof.The composite material rudder wing structure comprises a main beam and sandwich foam layers located on the two sides of the main beam, the main beam and the sandwich foam layers are of a structure with the middle thick and the two ends thin, and the main beam and the sandwich foam layers are connected through an adhesive; the main beam comprises at least three high-modulus glass fiber pultrusion plates, multi-axial glass fiber prepreg is arranged between the adjacent high-modulus glass fiber pultrusion plates, and the main beam and the sandwich foam layer are coated with a glass fiber-epoxy composite material layer. The rudder wing structure has the advantage of being light in weight, and the weight of the rudder wing structure can be reduced by 35%-40% compared with that of an aluminum alloy rudder wing; the rudder wing is made of a glass fiber composite material and has good wave-transparent performance, the surface of the rudder wing is subjected to appearance treatment through fluorocarbon paint, and the requirements for corrosion resistance, aging resistance and wave-transparent related performance are improved.

This invention relates to the fields of radio frequency detection and aircraft skin technology, and discloses a conformal skin radar structure based on a radio frequency microsystem. It includes several planar arrays based on the radio frequency microsystem, assembled according to the curvature requirements of aircraft skin to form irregularly shaped arrays. A conformal skin is attached to the surface of each irregularly shaped array, including an outer electromagnetic wave-transmitting protective skin. A filling portion is provided on the side of the protective skin that is in contact with the irregularly shaped array, and the filling portion is inserted into the splicing seam between adjacent planar arrays. This invention utilizes the integrated design of the irregularly shaped outer electromagnetic wave-transmitting protective skin and the irregularly shaped array based on the radio frequency microsystem. While ensuring electrical performance, it achieves conformal design with the aircraft skin, expanding the installation location of radar equipment on aircraft platforms. Furthermore, the structure is simple and compact, lightweight, easy to manufacture, and inexpensive. Moreover, the filling portion ensures the installation stability of the conformal skin and the irregularly shaped array while improving the electromagnetic performance of the combined irregularly shaped array.

The application provides a high and low temperature resistant, acid and alkali resistant, and radiation resistant wave-transparent polyphenylene sulfide composite material, which is made of the following raw materials in parts by weight: polyphenylene sulfide resin 40-65 parts, high-density polystyrene resin 10-25 parts, low-dielectric glass fiber 15-35 parts, compatibility agent 3-8 parts, low-dielectric filler 10-25 parts, lubricant 1-3 parts, compatibilizer 3-6 parts, and antioxidant 1-2 parts. The application also discloses a preparation method of the wave-transparent polyphenylene sulfide composite material. The wave-transparent polyphenylene sulfide composite material provided by the application can meet the strict requirements of performance of wave-transparent materials in special environment fields such as aerospace, intelligent driving of automobiles, 5G / 6G communication and chemical industry.