『The principle of orifice flowmeter』Related information(clamp on meter|electromagnetic meter|venturi meterrotameter|orifice meter|ultrasonic flow meter|mass flow meter|coriolis mass flow meter|coriolis flow meter|magnetic flow meter|magmeter flow meter|magflow flow meter|mag meter flow meter|electromagnetic flow meter|vortex flow meter|turbine flow meter|thermal mass flow meter|thermal flow meter|rotameter flow meter)

1. Principle and formula of orifice plate differential pressure flowmeter
Principle and formula of orifice plate differential pressure flowmeter: The orifice plate differential pressure flowmeter consists of a throttling device, a pressure pipe, and a differential pressure gauge. Its working principle is based on the throttling principle of fluid flow, which means that when fluid flows in a pipeline with a throttling device, a static pressure difference will be generated at the pipe wall before and after the throttling device. Specifically, when a fluid flows in a pipeline, it has two forms of energy: static pressure energy and kinetic energy. In the absence of external energy, according to the law of conservation of energy, the sum of static pressure energy and kinetic energy possessed by a fluid, as well as the energy loss used to overcome fluid flow resistance, always remains constant. When the fluid flows through the throttling device, due to the obstruction effect of the throttling device, the fluid near the pipe wall is blocked, and some kinetic energy is converted into static pressure energy, resulting in a difference in fluid static pressure before and after the throttling device. Formula: The flow calculation formula of orifice plate differential pressure flowmeter is derived based on Bernoulli equation and flow coefficient. Bernoulli equation: For any two cross-sections in a pipeline, the Bernoulli equation is followed. The formula is: $frac {p {1} {rho}+frac {V_ {1} ^ {2}} {2}=frac {p {2}} {rho}+frac {V_ {2} ^ {2}} {2} $, where $p {1} $and $p {2} $are the fluid static pressures at sections I and II, $V_ {1} $and $V_ {2} $are the fluid flow velocities at sections I and II, respectively, and $rho $is


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