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82 results about "C banding" patented technology

Lethal and sublethal damage repair inhibiting image guided simultaneous all field divergent and pencil beam photon and electron radiation therapy and radiosurgery

A medical accelerator system is provided for simultaneous radiation therapy to all treatment fields. It provides the single dose effect of radiation on cell survival. It eliminates the inter-field interrupted, subfractionated fractionated radiation therapy. Single or four beams S-band, C-band or X-band accelerators are connected to treatment heads through connecting beam lines. It is placed in a radiation shielding vault which minimizes the leakage and scattered radiation and the size and weight of the treatment head. In one version, treatment heads are arranged circularly and connected with the beam line. In another version, a pair of treatment heads is mounted to each ends of narrow gantries and multiple such treatment heads mounted gantries are assembled together. Electron beam is steered to all the treatment heads simultaneously to treat all the fields simultaneously. Radiating beam's intensity in a treatment field is modulated with combined divergent and pencil beam, selective beam's energy, dose rate and weight and not with MLC and similar devices. Since all the treatment fields are treated simultaneously the dose rate at the tumor site is the sum of each of the converging beam's dose rate at depth. It represents the biological dose rate. The dose rate at d-max for a given field is the individual machine dose rate. Its treatment options includes divergent or pencil beam modes. It enables to treat a tumor with lesser radiation toxicities to normal tissue and higher tumor cure and control.
Owner:SAHADEVAN VELAYUDHAN

Global navigation systems antenna

A phased array antenna that can be utilized in one or multiple Global Navigation Satellite Systems. This type of GNSS phased array antenna is often referred to as a CRPA. Various C-Band CRPA embodiments are illustrated to provide advanced performance in a compact real estate size that may fit within L-Band GPS ARINC and L-Band GPS 7-element CRPA size. A Large L-Band CRPA embodiment of the present invention provides for a substantial number of degrees of freedom that can be utilized to provide for advanced beam steering and null steering for advanced interference and multipath mitigation to form nulls over specific geographic regions.
Owner:OHIO UNIV

All-satellite electromagnetic compatibility verification method and system based on electric propulsion radiation emission simulator

InactiveCN108205089ATo solve the requirement that ignition can only be carried out in a vacuum environmentEnables EMC assessmentMeasuring interference from external sourcesC bandingElectromagnetic radiation
Provided are an all-satellite electromagnetic compatibility verification method and system based on an electric propulsion radiation emission simulator. The method includes firstly obtaining a radiation emission parameter of an electric propulsion system under a real ignition condition under vacuum conditions; constructing an electric propulsion electromagnetic radiation emission simulator which can generate the same electromagnetic radiation emission as the radiation emission parameters under the actual ignition conditions of the electric propulsion system; finally, in the all-satellite electromagnetic compatibility test, and the electric propulsion radiation emission simulator is used instead of the electric propulsion radiation emission under vacuum ignition conditions, to complete thetesting and evaluation of the satellite electromagnetic compatibility of the electric propulsion system. According to the all-satellite electromagnetic compatibility verification method and system, the range of radiated interference intensity of an electric thruster working normally to the satellite, and the test frequency band covers the frequency range of 1 GHz to 31 GHz; the magnitude of the electromagnetic radiation interference of the electric propulsion work is confirmed through the testing of three phases, and the electromagnetic radiation effect of the electric propulsion work processdoes not affect the normal operation of the all-satellite communication load in the L-band, C-band, Ku-band and Ka-band.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY

C-band space-borne synthetic aperture radar moving object imaging method

The invention provides a C-band space-borne synthetic aperture radar moving object imaging method. The method comprises the following steps: receiving raw echo data, carrying out imaging processing onthe raw echo data through an SAR range migration imaging algorithm, extracting a defocused ROI complex image data matrix S0 comprising moving target information, and initializing equivalent motion parameters alpha and beta of a target in the azimuth direction and distance direction; constructing a focusing operator Gamma (.) by utilizing the equivalent motion parameters alpha and beta; establishing a compressed sensing sparse reconstruction model based on the ROI complex image data matrix S0 and the focusing operator Gamma (.), and reconstructing a model sparse solution X through a soft threshold iterative algorithm; establishing a minimum error model, and updating the equivalent motion parameters alpha and beta through the model sparse solution X; and when judging that equivalent motionparameters alpha and beta meet algorithm terminal conditions, outputting a sparse solution amplitude matrix |X|. The method can obtain a final two-dimensional amplitude image through the parameterizedsparse reconstruction technique, thereby effectively suppressing asymmetrical sidelobes due to higher-order motion of the target.
Owner:TSINGHUA UNIV

Miniature C-band band-pass filter with low insertion loss and excellent high-order harmonic suppression

The invention discloses a miniature C-band band-pass filter with low insertion loss and excellent high-order harmonic suppression, which comprises an input port, an output port, an input inductor, an output inductor, an input capacitor, an output capacitor, five parallel resonance units, four zero set units, two cross-coupled capacitors and the like. All components comprise more than two layers and are realized by low-temperature co-fired ceramic technology, the input inductor, the output inductor, the input capacitor and the output capacitor are in a strip line design according to distributed parameters, intervalve inductors and intervalve capacitors adopt space coupling and distributed parameters, the cross-coupled capacitors are dielectric tablet 'Z'-shaped capacitors, and all the five parallel resonance units are in a three-layer folding and coupling strip line design. The band-pass filter of a stacked structure based on the low-temperature co-fired ceramic technology has the advantages of small size, light weight, high reliability, low insertion loss, excellent high-order harmonic suppression and the like, and meets the requirements of fields such as electronic communication and the like on miniaturization and integration of the electronic components.
Owner:WUXI NANLIGONG TECH DEV

Semiconductor optical amplifier

A polarization-independent SOA is provided which uses an InP substrate (11) as a semiconductor substrate and uses GaInNAs having introduced tensile strain as an active layer (14). With this configuration, the polarization independence is achieved by introducing the tensile strain, and high saturation optical output power is realized by reducing the film thickness of the active layer (14) as well as the gain peak wavelength is increased by reducing the band gap of the active layer (14) through use of GaInNAs made by adding nitrogen (N) to GaInAs as a material of the active layer (14) so as to achieve high gain especially in C-band and L-band even when band filling exits at the time of injecting a high current into the active layer (14).
Owner:FUJITSU LTD

System and method for filling gaps in radar coverage

A method of positioning a plurality of radar units in a defined area amongst one or more legacy radar units that provide legacy radar coverage in the defined area is disclosed. The steps of identifying a location of each legacy radar unit, setting a threshold altitude, and determining a legacy occultation of each legacy radar unit from a landscape level up to the threshold altitude are also disclosed. Mapping the legacy occultation of the legacy radar units to provide a three dimensional occultation map in the defined area and locating gaps below the threshold altitude in the legacy radar coverage as a function of the occultation map are also disclosed. Identifying a plurality of sites as a function of the gaps where the sites are accessible to receive a radar unit is also disclosed. Determining an anticipated radar coverage of a radar unit positioned at each of the sites and determining a reduction in the gaps as a function of the anticipated radar coverage are also disclosed. Selecting sites as a function of the reduced gaps is also disclosed. X band, C band or S band radar units can be positioned at the selected sites. The threshold altitude can be 10,000 or 15,000 feet. Affected populations and costs can also be considered in radar placement.
Owner:LAPOINT BLASE IND +1

Kinematic and dynamic mixed dimensionality reduction solving method for 10-bar underactuated mechanism

The invention provides a kinematic and dynamic mixed dimensionality reduction solving method for a 10 bar underactuated mechanism. The method comprises the following steps: step 1, a 10 bar mechanism mathematical model is established according to a Radarsat 2 battery panel deployment mechanism, wherein Radarsat 2 is a high resolution commercial radar satellite carrying a C band sensor; step 2, corresponding geometric equation is created according to the 10 bar mechanism mathematical model; step 3, the geometric equation is solved, and a dynamic model is established through combination with the Euler Lagrange equation; step 4, dynamic parameters of a 10 bar mechanism are solved according to the dynamic model. With adoption of the method, the dynamic parameters of the 10 bar mechanism can be solved, sizes of rod members of the Radarsat 2 battery panel deployment mechanism are optimized, and the battery panel deployment process stability and reliability in actual application satellite deployment process are improved.
Owner:SHANGHAI JIAO TONG UNIV

Quantitative detection method and device for upconverting fluorescent test strips

The invention discloses a quantitative detection method and a quantitative detection device for upconverting fluorescent test strips. The quantitative detection method comprises the following steps: under the excitation of 980nm near-infrared laser, capturing a fluorescent signal emitted by a test strip standard substance by using an image sensor, extracting the brightness values of pixels corresponding to regions, where a T band and a C band are positioned, from the image sensor, and calculating a ratio of the average brightness value of a T-band region to the average brightness value of a C-band region to obtain a linear relationship between the ratio and the correspondingconcentration of an item to be detected; take a plurality of test strips to be detected for detecting different items, extracting the brightness values of the pixels corresponding to the regions, where the T band and the C band are positioned, on each test strip to be detected, and calculating the ratio of the average brightness value of the T-band region to the average brightness value of the C-band region on each test strip to be detected, and acquiring the concentration of each item to be detected according to the linear relationship obtained in the step(1).Through the quantitative detection method and the quantitative detection device, not only simultaneous detection of multiple upconverting fluorescenttest strips can be achieved, but also quantitative detection can be achieved, and the detection accuracy is high.
Owner:ZHEJIANG UNIV

Method and system for determining optical dispersion displacement optical fiber C band transmission system

InactiveCN1505285AReduce the impactReduce the impact of FWM effectsElectromagnetic transmissionC bandingFiber amplifier
The invention disclose a conformation method of a kind of dispersion displacement fiber (G.653) band C transmission system, the method confirms the relay transmission series of the system firstly. Then the method uses above relay series to confirm the minimal simplex wave input power and the maximal simplex wave input power of G.653 fiber amplifier, further confirms the maximal transmission distance. Finally, the method confirms proper compensation plan according to the dispersion coefficient and the simplex transmission distance of G.653 fiber. The invention also discloses a system according to above method, which can use the G.653 fiber resources fully.
Owner:HUAWEI TECH CO LTD
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