A subway tunnel air valve with high temperature resistance, high strength, low leakage and low flow resistance
A high-strength, low-leakage technology, applied in the direction of valve lift, heat preservation, valve details, etc., can solve the problems that cannot fully meet the requirements, achieve the effect of improving rigidity and strength, improving sealing performance, and reducing flow resistance coefficient
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Embodiment 1
[0034] like Figures 1 to 7 , Figure 11 As shown, a subway tunnel air valve with high temperature resistance, high strength, low leakage and low flow resistance includes valve body 1, blade 2A, valve seat 3A, sealing plate 4, rotating shaft 5, bearing 6, driving mechanism 7 and connecting Rod mechanism 8.
[0035] The frame section of the valve body 1 is "C" shaped and protrudes into the valve body 1. Both ends of the upper and lower frames of the valve body 1 are flanged upwards and connected with the two side frames by bolts. The valve seat 3A is located on the valve body. 1. On the inner wall of the upper and lower frames, the valve seat 3A is in the shape of an arch bridge and fits with the protrusions of the upper and lower frames.
[0036] The sealing sheet 4 is arranged on the inner wall of the frame on both sides of the valve body 1 , the sealing sheet 4 is in the shape of an arch bridge, and the sealing sheet 4 fits with the protrusions of the frames on both sides....
Embodiment 2
[0040] The difference between the second embodiment and the first embodiment lies in the structure of the valve seat.
[0041] like Figure 12 As shown, the valve seat 3B includes a baffle 310B and a pressing piece 320B. The baffle 310B is fixed on the protrusions of the upper and lower frames, and the pressing piece 320B is arranged on one side of the baffle 310B.
Embodiment 3
[0043] The difference between the third embodiment and the first embodiment lies in the structure of the blades.
[0044] like Figure 9 As shown, the blade 2B includes two airfoils 210B with the same shape and a straight cross-section. The two sides of the airfoil 210B are provided with connecting plates 211B. The blade 2B is symmetrically connected to the corresponding connecting plate 211B by bolts or rivets from the center of the airfoil 210B. One side of the blade 2B is provided with a shrapnel 220B, and the side of one blade 2B with the shrapnel 220B is overlapped with the side of the other blade 2B without the shrapnel 220B between the two blades 2B, and the rotating shaft 5 is passed through a bolt or The rivets are installed between the two blades 210B of the blade 2B.
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