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52results about How to "Reduced Radar Cross Section" patented technology

Electromagnetic shielding conformal optical window with longitude and latitude-shaped mesh structure

The invention provides an electromagnetic shielding conformal optical window with a longitude and latitude-shaped mesh structure, which belongs to the technical field of electromagnetic shielding of optical transparent pieces. The electromagnetic shielding conformal optical window comprises a conformal optical window and is characterized in that: (1) a longitude and latitude-shaped metal mesh is manufactured on the inner side surface of the conformal optical window shell; and the longitude and latitude-shaped metal mesh covers the whole inner side surface of the conformal optical window shell; or (2) a longitude and latitude-shaped metal mesh and a conformal optical window inner shell are manufactured on the inner surface of the conformal optical window shell from outside to inside in turn; the longitude and latitude-shaped metal mesh covers the whole inner surface of the conformal optical window shell and outer surface of the conformal optical window inner shell; the latitude-shaped metal mesh consists of metal longitudes and metal latitudes; the metal latitudes are uniformly arranged in an equivalent centre angle along a circumferential direction; the metal longitudes are arranged at equal intervals according to a metal mesh cycle along a generatrix direction; and the metal longitudes and the metal latitudes are electrically connected with one another. The electromagnetic shielding conformal optical window with the longitude and latitude-shaped mesh structure is suitable for electromagnetic shielding technology of military or civil conformal optical windows for remote measuring and sensing, medical diagnosis, secret communication, aerospace equipment and the like.
Owner:HARBIN INST OF TECH

Radar and infrared comprehensive stealth structure of thrust augmentation type turbofan engine

The invention provides a structure suitable for a thrust augmentation type turbofan engine and capable of realizing backward radar and infrared comprehensive stealth. The structure comprises a shielding support plate, an inner cone and a trailing edge blowing flame stabilizer, and is simple in structure, high in reliability, small in weight gain and small in aerodynamic loss, and the radar and infrared stealth performance can be remarkably improved only by virtue of the self structure.
Owner:AECC SICHUAN GAS TURBINE RES INST

Radar energy absorbing deformable low drag vortex generator

A family of Radar energy Absorbing Deformable Low Drag Vortex Generators (RAD-LDVG) is described herein. This family of devices are fabricated in such a way that it can conform to aircraft surface features while reducing radar returns from structural details. Vortex generators (VGs) are typically used to reattach or smooth gross flowfields over aircraft surfaces. By doing so, an airfoil or wing can maintain attached flow at higher angles of attack and / or higher lift coefficients than one without the VGs. These devices are also used to reattach and / or smooth flows that encounter crossflow-induced instabilities and / or adverse pressure gradients on the upper surfaces of wings or near aircraft boattails. Other uses include reduction of buffet, vibration, flutter, cavity resonance or general bluff-body pressure drag reduction. Although conventional rigid VGs do generate vortical aerodynamic structures, two major problems are often experienced: i.) the inability to conform to curved surfaces, ii.) the generation of radar cross-section spikes produced by the VGs themselves.
Owner:UNIVERSITY OF KANSAS

Reflecting plate based on frequency selection surface units

InactiveCN102904063AReduced Scattering Cross SectionAvoid couplingAntennasElectricityScattering cross-section
The invention discloses a reflecting plate based on frequency selection surface units. The reflecting plate is mainly used for solving the problems that an existing reflecting plate is relatively large in size, cannot be applied to antennae with smaller sizes and cannot reduce the antenna radar cross section in a multi-angle manner. The reflecting plate comprises Z frequency selection surface units (1) and a base plate (2), wherein Z is larger than or equal to 4; the Z frequency selection surface unit are uniformly distributed on the surface of the base plate in a rectangular array; each frequency selection surface unit consists of four pasters; each paster (11) comprises a rectangular trunk (111) and n arc-shaped branch knots (112), and the n arc-shaped knot are alternatively arranged on two sides of the rectangular trunk; and the four pasters respectively rotate 90 degrees, 180 degrees and 270 degrees by utilizing the bottom left corners of the pasters as centers, so as to form a crossed distribution structure of the four pasters. According to the reflecting plate, the electric size of each frequency selection surface unit is prolonged, the space is fully utilized, the resonant frequency is reduced, and the reflecting plate can be applied to the antennae with smaller sizes and can be used for reducing the antenna radar scattering cross section in a multi-angle manner.
Owner:XIDIAN UNIV

Conformal antenna array seeker modeling simulation method

The present invention discloses a conformal antenna array seeker modeling simulation method. The method comprises: S1. selecting rectangular microstrip patch antenna elements as directed radiation antenna elements of a conformal antenna array seeker, and performing location configuration on the rectangular microstrip patch antenna elements according to a shape of a seeker carrier platform, wherein a plurality of rectangular microstrip patch antenna elements form an antenna array; S2. applying a mathematical relationship of Euler rotation transformation to complete derivation of a far-field radiation pattern function of the conformal antenna array seeker; and S3. applying a genetic optimization algorithm to optimally design a far-field radiation pattern of the conformal antenna array seeker. By use of the method disclosed by the present invention, a radar diffusion cross section of the seeker can be reduced, an excellent electromagnetism stealth property is achieved, and the highest sidelobe value of the far-field radiation pattern is significantly improved.
Owner:SHANGHAI INST OF ELECTROMECHANICAL ENG

Low-RCS (radar cross section) microstrip patch antenna based on polarization conversion

The invention discloses a low-RCS microstrip patch antenna based on polarization conversion. The low-RCS microstrip patch antenna based on polarization conversion is used for solving the defect of poor scattering performance of existing microstrip patch antennas. The low-RCS microstrip patch antenna based on polarization conversion comprises a radiating unit (1), a dielectric slab (2), a metal ground slab (3), a coaxial joint (4) and a polarization conversion surface (5). The upper surface and the lower surface of the dielectric slab (2) are printed with the radiating unit (1), and the polarization conversion surface (5) as well as the metal ground slab (3) respectively; the polarization conversion surface (5) is composed of four polarization conversion unit groups (51), and the center of the polarization conversion surface (5) is provided with a square area (6); every polarization conversion unit group (51) comprises a plurality of polarization conversion units (511) with the symmetric axises provided with square notches (512) which point to the same direction. The low-RCS microstrip patch antenna based on polarization conversion has the advantages of being stable in radiating performance and high in scattering performance and can serve as a communication antenna on a low-RCS device.
Owner:XIDIAN UNIV

Ultra wide band low radar cross section microstrip antenna

The invention provides an ultra wide band low radar cross section microstrip antenna and aims to solve a technical problem of narrow bandwidth of a microstrip antenna reduction radar cross section inthe prior art. The microstrip antenna comprises a medium substrate, a metal floor, a polarized conversion surface, a radiation unit and a coaxial connector, wherein the metal floor is printed at a lower surface of the medium substrate, the polarized conversion surface is printed at an upper surface of the medium substrate, the center position of an upper side of the medium substrate is provided with a rectangular chamber, an upper portion of the chamber is provided with the radiation unit fixed with an output end of the coaxial connector, the polarized conversion surface is composed of four polarized conversion unit sets, each polarized conversion unit set comprises multiple decreasing fractal units, and arrangement direction difference of decreasing fractal units of the adjacent polarizedconversion unit sets is 900. The microstrip antenna is advantaged in that the ultra wide band decrement microstrip antenna radar cross section has stable performance, and the microstrip antenna can be applied to antenna systems with the complex electromagnetic environment to reduce electromagnetic interference among antennas in a wide band.
Owner:XIDIAN UNIV +1

Composite materials comprising conductive nano-fillers

The invention relates to composite materials comprising conductive nano-fillers. A process for the production of a composition comprising one or more conductive nano- filler(s), one or more polyarylethersulphone thermoplastic polymer(s) (A), one or more uncured thermoset resin precursor(s) (P), and optionally one or more curing agent(s) therefor, wherein said process comprises mixing or dispersing a first composition comprising one or more conductive nano-filler(s) and one or more polyarylethersulphone thermoplastic polymer(s) (A) with or into one or more uncured thermoset resin precursor(s) (P), and optionally one or more curing agent(s) therefor.
Owner:CYTEC TECH CORP

Coating for the concealment of objects from the electromagnetic radiation of antennas

An assembly comprising a device and an obstacle subjected to an incident electromagnetic wave of wavelength λ. The obstacle is formed from an electrically conductive material and has a substantially cylindrical shape of transverse dimensions r with respect to a longitudinal axis (O, ez). The longitudinal axis is substantially perpendicular to a propagation direction of the incident electromagnetic wave. The obstacle further has a maximum transverse dimension d such that the ration λ / d is less than 1. The device is placed on all or a part of a surface of the obstacle and comprises a sleeve with a dielectric coating of equivalent relative permittivity EREQ, of height hP along a longitudinal axis of the sleeve, substantially equal to formula A, and a sleeve with an electrically conductive coating placed on the periphery of the dielectric coating.
Owner:AIRBUS SAS

Liquid patch antenna

The invention discloses a liquid patch antenna. The liquid patch antenna comprises a medium base plate which is provided with a metal floor, an exciting end port, a metal probe, a nonmetal radiation patch in which liquid is poured, and a nonmetal short circuit patch in which liquid is poured, wherein the nonmetal short circuit patch is vertically fixed to the metal floor; one end of the nonmetal short circuit patch is connected to the metal floor to form an earth short circuit, and the other end of the nonmetal short circuit patch is connected to the nonmetal radiation patch which is parallelto the metal floor; the nonmetal short circuit patch and the nonmetal radiation patch form an inverted L-shaped structure; liquid in the nonmetal short circuit patch is communicated with the liquid inthe nonmetal radiation patch; one end of the metal probe passes through the medium base plate and then extends into the nonmetal radiation patch, and the other end of the metal probe is equipped withthe exciting end port; and the metal probe is parallel with and close to the nonmetal short circuit patch without direct contact. The liquid patch antenna has the characteristics of being high in radiation efficiency, high in gain, high in impedance bandwidth and universal radiation, and the working frequency ranges from 2.26-3.24GHz.
Owner:SOUTH CHINA UNIV OF TECH

Ultra-wideband bionic antenna with low radar scattering cross section

The invention discloses an ultra-wideband bionic antenna with a low radar scattering cross section, and mainly solves the problems that existing ultra-wideband antenna radar has high scattering cross section and can be easily found by radar. The ultra-wideband bionic antenna with the low radar scattering cross section comprises a radiation unit (2), a radiant floor (3) and an SMA coaxial adapter substitute. The antenna radiating unit and the antenna radiation floor are respectively printed on both sides of a medium material board (1), and are respectively connected with an inner core (4) and an outer core (5) of the SMA coaxial adapter substitute. The radiating unit is designed to be a sectoral structure comprising a rectangular column and a plurality of arc strips symmetrically arranged on the rectangular column in accordance with a design thinking similar to insect antennae, the degrees of the central angles of the arc strips are identical, and the sizes of semi-diameters are progressively increased according to equal intervals from the top to the bottom; and both sides of the radiant floor are rectangles with inversed 90-degree arc angles. The invention has the advantages of wide frequency band and good hiding performance, thereby being capable of being used as the ultra-wideband antenna on a hiding target vector.
Owner:XIAN CETC XIDIAN UNIV RADAR TECH COLLABORATIVE INNOVATION INST CO LTD

Radial multi-beam gap waveguide slot antenna array applied to microwave band

The invention discloses a radial multi-beam gap waveguide slot antenna array applied to a microwave band. The radial multi-beam gap waveguide slot antenna array comprises three parts of a gap waveguide radial feeding network, a slot antenna array and a coaxial-gap waveguide conversion structure. By a design of a bottom-layer feeding network and each slot sub-array in a top layer in a radial direction, generation of random numbers of radial wave beams can be achieved, the size and the direction of each wave beam are independently adjustable, and a beam split phenomenon is proposed according toa certain radial asymmetric construction mode of the antenna.
Owner:SOUTHEAST UNIV
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