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186results about How to "Reduce measurement uncertainty" patented technology

Vector measurement method for passive intermodulation interference

ActiveCN103675448ASelf-intermodulation reductionNarrow down the measurement rangeSpectral/fourier analysisTransmitters monitoringLocal oscillator signalAudio power amplifier
The invention provides a vector measurement method for passive intermodulation interference. The vector measurement method for the passive intermodulation interference comprises the steps that firstly a computer module adjusts the output frequency of a frequency reference unit, and a frequency reference signal is output; the frequency reference signal is used by a first signal source, a second signal source and a local oscillator source module after power division is conducted on the frequency reference signal, and then a testing signal with a frequency F1, a testing signal with a frequency F2 and a local oscillator signal L0 are generated; a part of the testing signal F1 and a part of the testing signal F2 are amplified by an amplifier module after power division is conducted on the testing signal F1 and the testing signal F2, then the signals are combined to generate a +43dBm dual-tone signal used for testing, reciprocal mixing is conducted on the other part of the testing signal F1 and the other part of the testing signal F2 after the other part of the testing signal F1 and the other part of the testing signal F2 pass through a frequency multiplication module, the frequency of an obtained signal is 2F1-F2 after filtering, and the signal is received by a reference receiver to serve as a PIM reference signal. By the adoption of the vector measurement method for the passive intermodulation interference, self-intermodulation and self-calibration of an instrument can be achieved, vector compensation for the self-intermodulation of the instrument can be achieved, the self-intermodulation of a system is greatly reduced, the measurement range of the system is widened, and the uncertainty of measurement is reduced; the time-frequency conversion technology can be directly adopted by a measurement result, and the time domain response to a PIM product can be observed.
Owner:CHINA ELECTRONIS TECH INSTR CO LTD

Water cooling balance

ActiveCN104180966AEliminate the effects of aerodynamic measurementsExtended service lifeAerodynamic testingLeaking waterCooling effect
The invention discloses a water cooling balance which comprises a rod-type balance and a water-cooled jacket. Two water flow pipelines are arranged in the rod-type balance. The two ends of each water flow pipeline are arranged on the two end faces of the rod-type balance respectively. A switching joint is arranged between the water-cooled jacket and the rod-type balance and fixed to one end face of the rod-type balance through a screw. A water inlet switching pipeline and a water outlet switching pipeline are arranged on the switching joint. One end of the water inlet switching pipeline and one end of the water outlet switching pipeline correspond to openings of the two water flow pipelines on the end faces of the rod-type balance in position and the other end of the water inlet switching pipeline and the other end of the water outlet switching pipeline correspond to a water inlet and a water outlet of the water-cooled jacket in position. The defects that a corrugated pipe type water cooling balance is large in drag measurement error and inconvenient to install and use and a corrugated pipe is prone to being damaged and leaking water are overcome. In addition, due to the fact that corrugated pipe related devices are omitted, the length of the balance is reduced, the diameter of the balance is increased, the rigidity and the cooling effect of the balance are greatly improved, the temperature effect is reduced, and measurement uncertainty is obviously reduced.
Owner:INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT

Attitude precision estimation method of multiple high-accuracy inertial navigations system

The invention provides an attitude precision estimation method of multiple high-accuracy inertial navigation systems. According to the method, a set of laser tracker, an attitude measuring head, a signal generator, a swing table or turntable, and a data recording device are used to realize the attitude precision estimation of multiple high-accuracy inertial navigation systems at the same time through initial alignment calibration and synchronous data acquisition, wherein the swing table or turntable is used for providing a dynamic swing environment and can realize pitching, horizontal rolling and longitudinal swing according to a given period and amplitude value, the laser tracker and components matched with the laser tracker can measure three attitude angles of the swing table under a geographical system in real time, the signal generator sends TTL (transistor-transistor-logic) synchronizing level to the laser tracker and the laser inertial navigation systems so as to trigger data output, and the data recording device is used for receiving attitude data sent by the laser tracker and the inertial navigation systems in real time and storing the attitude data into lines. The method is quite suitable for the attitude precision estimation of the laser inertial navigation systems and can be used for estimating the attitude precision of multiple high-accuracy laser inertial navigation systems at the same time by using simplest equipment components.
Owner:中国人民解放军92537部队

High-hydrostatic-pressure low-frequency calibrating cavity and testing method thereof

The invention discloses a high-hydrostatic-pressure low-frequency calibrating cavity and a testing method thereof. The high-hydrostatic-pressure low-frequency calibrating cavity mainly comprises a metal cavity, a transmitting transducer, a reciprocal transducer, a manual pressure pump and a pressure gauge, wherein the metal cavity is a cylindrical closed stainless steel cavity, sound bearing media fill the metal cavity, the transmitting transducer, the reciprocal transducer and a to-be-tested hydrophone are mounted in the metal cavity, and the transmitting transducer and the reciprocal transducer are symmetrically mounted on two sides in the metal cavity; the manual pressure pump is communicated with the metal cavity through a liquid inlet valve and is used for applying high hydrostatic pressure into the metal cavity, and the liquid inlet valve is used for communicating or separating the metal cavity with or from the manual pressure pump; a liquid draining hole in the metal cavity is communicated with a liquid draining valve, and the pressure gauge is used for monitoring the pressure in the metal cavity. The high-hydrostatic-pressure low-frequency calibrating cavity has the beneficial effects that the low-frequency receiving sensitivity of the to-be-tested hydrophone can be tested by comparing the hydrophone with the reciprocal transducer.
Owner:THE 715TH RES INST OF CHINA SHIPBUILDING IND CORP

Device and method for calibrating flow-dividing vacuum leaking hole

The invention relates to a device and a method for calibrating a flow-dividing vacuum leaking hole, in particular to the device and the method for calibrating the vacuum leaking hole, the leakage value of which is less than 1*10-8 Pa.m3/s by adopting flow-dividing technology, and belongs to the field of measuring technology. The device consists of the calibrated leaking hole, a valve, an ionization gauge, a small hole, a flow-dividing chamber, a non-evaporable getter pump, an ultrahigh vacuum calibrating chamber, a metering hole, a very high vacuum pumping chamber, an oil-free bi-turbo molecular pump air exhauster set, a quadrupole mass spectrometer, a flow meter, a super-high vacuum calibrating chamber, the metering hole, a super-high vacuum pumping chamber and a common molecular pump air exhauster set. The method adopts a fixed flow method gas micro-flow meter to provide a known gas flow rate, so the measuring range of the flow rate is wide and uncertainty of the measurement is low; and by adopting a flow-dividing method to calibrate the vacuum leaking hole, the method of the invention completely avoids a nonlinear error of the quadrupole mass spectrometer and can precisely calibrate the vacuum leaking hole the leakage value of which is less than 1*10-8 Pa.m3/s.
Owner:NO 510 INST THE FIFTH RES INST OFCHINA AEROSPAE SCI & TECH

Method for measuring sight line stabilizing accuracy of photoelectric sight-stabilizing system

The invention discloses a method for measuring the sight line stabilizing accuracy of a photoelectric sight-stabilizing system, and belongs to the technical field of optical measurement. The method is characterized by comprising the following steps that: a plane reflector is fixed on an inner ring frame of the photoelectric sight-stabilizing system to be measured, the photoelectric sight-stabilizing system to be measured is in a vibration state, a measuring laser beam is subjected to strength stabilization, spatial filtering and collimation and then irradiates the plane reflector, a complementary metal oxide semiconductor (CMOS) camera transmits a light spot image sequence of a reflected light beam imaged on a target surface to an image recording and processing system, and the image recording and processing system performs a series of processing on the light spot image sequence to obtain a light spot center-of-mass coordinate sequence, a stabilizing accuracy value sequence and stabilizing accuracy value sequence standard deviation, so that the stabilizing accuracy is measured. By the method, the high-accuracy measurement of the sight line stabilizing accuracy of the photoelectric sight-stabilizing system is realized; and the method can be popularized to the fields of measurement of the stabilizing accuracy of a gun control system and the like, and is wide in application prospect.
Owner:中国兵器工业第二0五研究所

Gas combustion heat measuring device and combustion heat measuring method utilizing the same

The invention relates to a gas combustion heat measuring device and a combustion heat measuring method utilizing the same. The measuring device comprises an oxygen bomb calorimeter and a gas gathering balancing unit. The combustion heat measuring method comprises the following steps: filling combustible gas to be measured with a volume equal to an inner volume V of the oxygen bomb into the oxygen bomb through the gas gathering balancing unit; employing a direct combustion method to enable the combustible gas with a volume equal to the inner volume V of the oxygen bomb to combust directly in the oxygen bomb; calculating a combustion heat of the combustible gas by using a premeasured thermal capacity k of the oxygen bomb system and a temperature rise delta t generated during combustion of the combustible gas in the oxygen bomb according to a formula. The calorific value of the combustible gas is measured by employing a direct combustion method, so that measuring uncertainty is little and measured value can be directly traced to international system of units, besides the device with a reasonable structure is easy to operate, and has a promising application prospect. Therefore, natural gas trade settlement can be realized by metering energy.
Owner:NAT INST OF METROLOGY CHINA

Suspended swing arm contourgraph for ultra-large diameter surface shape detection

The invention discloses a suspended swing arm contourgraph for ultra-large diameter surface shape detection, belongs to the technical field of optical detection and aims at solving the problem that when a swing arm contourgraph existing in the prior art is used for measuring a large-diameter optical element surface shape, the arm is too long to cause reduction of detection accuracy. The suspended swing arm contourgraph for ultra-large diameter surface shape detection comprises a suspension device, a connecting piece A, an air-borne turntable, a connecting piece B, a measuring arm, a weight balancing piece, a connecting piece C and a displacement sensor, wherein the air-borne turntable is connected with the suspension device through the connecting piece A in a suspended mode; the measuring arm is fixed to the air-borne turntable through the connecting piece B; a measuring head of the displacement sensor is fixed to one end of the measuring arm through the connecting piece C; the weight balancing piece is arranged at the other end of the measuring arm. By the adoption of the suspended swing arm contourgraph for ultra-large diameter surface shape detection, the accuracy and stability of swing arm contour detection can be improved.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Special worktable for laser tracker and laser tracking measurement method

The invention discloses a special worktable for a laser tracker, which is capable of moving the laser tracker to an extension line of the link between the point A and the point B to the utmost extent and keeping the pointing direction of the laser track consistent with the link between the point A and the point B to the utmost extent when in measurement of the distance between the point A and the point B in the three-dimensional space. The special worktable for the laser tracker comprises a mount, a vertical angle regulator, a horizontal angle regulator, a horizontal translation regulator and a lifting regulator, wherein the mount is matched with a base of the laser tracker, the vertical angle regulator, the horizontal angle regulator, the horizontal translation regulator and the lifting regulator are used for regulating the mount. The interferometry function of the laser tracker can be utilized by the worktable during measurement, horizontal rotation and vertical rotation of the laser tracker are avoided, and accordingly uncertainty in measurement of the laser tracker is reduced, and measurement precision of the point A and the point B is guaranteed. In addition, the invention further discloses a laser tracking measurement method.
Owner:CHINA ERZHONG GRP DEYANG HEAVY IND

Real thrust measuring and calculating method for test run of aero-engine on indoor test bed

The invention belongs to the technical field of aero-engines and particularly relates to a real thrust measuring and calculating method for test run of an aero-engine on an indoor test bed. The real thrust measuring and calculating method specifically comprises the steps of 1 determining the spatial position of a control body, 2 arranging a rear cross section measuring point on a lip rear cross section (2), 3 arranging front cross section measuring point on a far front cross section (1), 4 obtaining wind speed values and static pressure values on the measuring points, and 5 obtaining a real thrust value of the test run of the aero-engine on the indoor test bed. According to the real thrust measuring and calculating method, the area of air intake cross section of the engine is reasonably selected, the flow pipe surface for air flowing in a test run workshop serves as a control face, an air intake channel additional resistance correction formula is derived and real thrust is calculated by applying momentum theorem. The real thrust measuring and calculating method has the advantages of being clear in control body division, fewer in correction terms, simple and convenient to calculate and the like, and the problem of real thrust measurement and calculation during the test run of the aero-engine on the indoor test bed can be solved.
Owner:BEIJING CHANGCHENG INST OF METROLOGY & MEASUREMENT AVIATION IND CORP OF CHINA
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