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42results about How to "Reduce size and complexity" patented technology

Image frequency rejection frequency mixer structure for terahertz wave band

The invention belongs to the technical field of terahertz devices, and provides an image frequency rejection frequency mixer structure for a terahertz wave band. The image frequency rejection frequency mixer structure includes an E-plane rectangular waveguide Chinese character 'tian'-shaped branch wire bridge 3dB directional coupler, micro-strip waveguide double probes, two frequency mixers, and a power combiner. A radio-frequency signal can generate two-channel radio-frequency signals with an equal amplitude and a 90-dgress phase difference via the E-plane rectangular waveguide Chinese character 'tian'-shaped branch wire bridge 3dB directional coupler, and the two-channel radio-frequency signals are input into two-channel frequency mixers respectively; a local oscillation signal can generate two-channel signals with an equal amplitude and a same phase via micro-strip waveguide double probes, and the two way signals are input into the two-channel frequency mixers respectively; two-channel frequency mixer intermediate frequency output signals are combined via the power combiner, and then are output; and each input end of the power combiner is provided with a 90-deree phase shifter for allowing the corresponding frequency mixer intermediate frequency output signal to generate a 90-degree phase shift, so that the two-channel frequency mixer intermediate frequency output signals are stacked in phase and output. The image frequency rejection frequency mixer structure is simple in structure and is applied to the terahertz wave band.
Owner:UNIV OF ELECTRONIC SCI & TECH OF CHINA

Satellite spectrum sensing method and system based on equal-amplitude equal-interval multi-wavelength light source

The invention discloses a satellite spectrum sensing method and system based on an equal-amplitude equal-interval multi-wavelength light source. Based on an equal-amplitude, equal-interval and multi-wavelength satellite spectrum sensing method, a photon technology is introduced into a spectrum sensing technology in the satellite navigation electric field, the equal-amplitude equal-interval and multi-frequency wavelength is used as the light source, the sensing of a microwave frequency channel is achieved on each optical wavelength, and meanwhile, an I/Q demodulation technology is combined to achieve high-precision sensing and treatment of a radio frequency signal. According to the method and system provided by the invention, the parallel multi-channel microwave frequency sensing is completed on an optical path, so that the volume and complexity of the system are greatly reduced; the method and system are applicable to strict requirements on the volume, weight and power consumption of an on-satellite system module in a satellite navigation system; the limitation of the traditional sensing device in the electric field on the losses of frequency bands close to the navigation system isbroken, and the problem of ultra wide band signal sensing and treatment of the satellite navigation system is solved.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY

Surface Figure Test Method For Large Convex Optical Surfaces

A method of testing figure quality of a convex mirror in which an optical quality substrate material is used. The substrate has a front convex surface that has to be polished and figured to high accuracy, typically λ/10 (HeNe), and a rear concave surface which only needs to be polished and figured to moderate surface figure accuracy, typically about 1-λ (HeNe). Three separate interferometric null tests are then carried out to produce three independent sets of optical path difference (OPD) data. Null lenses, or nulling computer generated holograms (CGHs), are designed and used as needed in each test setup so that spherical aberration is corrected. All three separate interferometric tests are either ideal null tests, or near null tests. From the three sets of OPD data, surface figure errors on the rear and front surfaces of the test optic, h1(xi,yj) and h2(xi,yj), are calculated as well as the OPD error OPDI(xi,yj) introduced by refractive index inhomogeneity in the substrate material. The rear surface is then corrected, generally using a computer-controlled polishing machine, to reduce rear surface errors hi(xi,yj) to a manageably small level. The front convex surface of the test optic is then corrected to reduce surface figure error h2(xi,yj) to within some specified amount. The front mirror surface can be figured to any required accuracy in spite of residual surface figure error in the rear surface, h1(xi,yj), and the effects of refractive index inhomogeneity in the substrate material OPDI(xi,yj). The convex front surface is then coated with a reflective coating to produce the finished convex mirror.
Owner:MCKECHNIE THOMAS STEWART
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