Double-wing type flow sensor
A flow sensor and double-wing technology, which is applied in the field of sensors, can solve the problems of low measurement accuracy, unstable outflow coefficient, and easy pollution accumulation, and achieve the effect of large measurement range, stable flow coefficient, and high measurement accuracy
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specific Embodiment approach 1
[0023] Specific implementation mode one: combine figure 1 , image 3 and Figure 4 To illustrate this embodiment, the double-wing flow sensor includes a flow sensor housing 9, the flow sensor housing 9 is composed of two large and small wings, the top of the large wing 1 is used as the head of the flow sensor, and the bottom of the small wing 2 As the tail of the flow sensor, a corner 5 is provided at the junction of the large and small wing shapes, so that the fluid flows and separates at the corner; the head 10 of the large wing shape 1 has a pressure tapping hole 4, and its end surface is provided with a high pressure Cavity 3, the high-pressure chamber 3 communicates with the pressure-taking hole 4; the end face of the small wing-shaped 2 is provided with a low-pressure chamber 7, which communicates with the row holes 6 or grooves at the corners of the large and small wing-shaped.
specific Embodiment approach 2
[0024] Specific implementation mode two: combination figure 2 To illustrate this embodiment, the difference between this embodiment and the double-wing flow sensor described in Embodiment 1 is that the head of the large wing is provided with a groove 8, and the groove 8 communicates with the high-pressure chamber 3 .
specific Embodiment approach 3
[0025] Specific implementation mode three: combination Figure 5 Describe this embodiment, the difference between this specific embodiment and the double-wing flow sensor described in the first or second specific embodiment is that the head 10 of the large wing shape is provided with an upstream passivation surface 12, and the large and small An additional wing 11 protruding outward is added to the corner of the junction of the two airfoils, so that the flow separation is more severe and the pressure drop is more obvious.
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