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79results about How to "Accurate flow measurement" patented technology

Method for calculating steam admission enthalpy of air-cooling condenser of direct air-cooling unit

ActiveCN103487272AOvercome the shortcoming of imprecise inlet steam enthalpyOvercome the disadvantage of inaccurate inlet steam flowStructural/machines measurementEnergy balancingEngineering
The invention discloses a method for calculating steam admission enthalpy of an air-cooling condenser of a direct air-cooling unit. The method specifically includes the first step of measuring the flow of condensed water entering a deaerator, the steam leakage flow of a front shaft seal and a rear shaft seal of a high pressure cylinder and the steam leakage flow of a front shaft seal and a rear shaft seal of an intermediate pressure cylinder, the steam admission flow of a low pressure shaft seal, the steam leakage flow of a steam admission valve rod of the high pressure cylinder and the steam leakage flow of a steam admission valve rod of the intermediate pressure cylinder, and the flow of seal water entering a feed pump; the second step of calculating the steam extraction flow, the water feed flow, the main steam flow, the high pressure cylinder exhaust steam flow and the reheat steam flow from the first section to the fourth section according to energy balance and mass balance of a high pressure heater and the deaerator; the third step of calculating the steam extraction flow from the fifth section to the seventh section according to heat balance and mass balance of a low pressure heater, and calculating exhaust steam energy and exhaust steam flow of the lower pressure cylinder of a turbine according to energy balance and mass balance of the turbine; the fourth step of calculating exhaust steam enthalpy of the low pressure cylinder, namely, the steam admission enthalpy of the air-cooling condenser, and enabling the steam admission enthalpy to serve as a benchmark for calculating heat load of the air-cooling condenser. The measuring results can be more accurate.
Owner:STATE GRID CORP OF CHINA +1

Measuring method of liquid full pressure gradient-flow relation in low-permeability reservoir

The invention provides a measuring method of the liquid full pressure gradient-flow relation in a low-permeability reservoir. The measuring method includes the steps that 1, a thin glass tube communicator device is adopted for measuring the static starting pressure gradient in a low-permeability rock core; 2, a multifunctional rock core displacement device is adopted for measuring the steady state pressure gradient-flow relation; 3, the starting pressure gradient, obtained through the static method, of the low-permeability rock core and the steady state pressure gradient-flow data obtained through measurement by the steady-state method are drawn in the same graph, and then the liquid flowing full pressure gradient-flow relation of the low-permeability rock core is obtained. By means of the measuring method of the liquid full pressure gradient-flow relation in the low-permeability reservoir, the starting pressure of the low-permeability rock core can be measured accurately, the liquid flowing pressure gradient-flow relation can be obtained on the basis of the full pressure gradient, and the obtained flow characteristics of the low-permeability rock core are more accurate and can be used for flowing characteristics description of the low-permeability reservoir.
Owner:CHINA PETROLEUM & CHEM CORP +1

Moderate thrust aero-engine testing switching device

InactiveCN105403409AAir flow test is simple and convenientEasy loading and unloadingEngine testingAviationEngineering
The invention provides a moderate thrust aero-engine testing switching device comprising a pedestal, air inlet openings, an inner sealing ring, an upper cover disc, and a pressing plate. The pedestal in the shape of a ring, and is provided with an annular-shaped concave groove. The inner sealing ring is disposed on the inner side top part of the annular-shaped concave groove of the pedestal, and the upper cover disc is disposed on the outer side top part of the annular-shaped concave groove of the pedestal. The outer side surface of the pedestal is provided with more than twenty air inlet openings facing the outer side horizontally, and the air inlet openings are disposed uniformly along the circumference of the pedestal. The position of the pressing plate in the annular-shaped concave groove is fixedly disposed on the bottom surface of the upper cover disc by the bolt. The moderate thrust aero-engine testing switching device is advantageous in that the test of the air flow between the high pressure turbine disc and low pressure turbine disc is simple and convenient, the assembly and the disassembly are easy, and the connection with the device of the test board is convenient; the flow measurement is accurate, and the flowing of the air flow is good.
Owner:CHINA HANGFA GUIZHOU LIYANG AVIATION POWER CO LTD
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