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A fast switching valve device and switching method for large-diameter wind tunnel applications

A valve device and fast switching technology, applied in the field of wind tunnel experiments, can solve problems such as the complex structure of fast-opening valves, and achieve the effects of improving service life, reducing damage, and reducing quality

Active Publication Date: 2022-03-18
HUAZHONG UNIV OF SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] In view of the above defects or improvement needs of the prior art, the present invention provides a fast opening and closing valve device and a switching method for large-diameter wind tunnel applications, thereby solving the problem of the quick-opening valve structure applied to large-diameter wind tunnels in the prior art complex technical issues

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  • A fast switching valve device and switching method for large-diameter wind tunnel applications
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  • A fast switching valve device and switching method for large-diameter wind tunnel applications

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Embodiment Construction

[0040] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0041]In describing the present invention, it is to be understood that the terms "center", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", The orientations or positional relationships indicated by "top", "bottom", "inner", "outer", etc. are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the...

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Abstract

The invention discloses a fast switch valve device and a switch method for large-diameter wind tunnel applications, belonging to the technical field of wind tunnel experiments, including electrical control components, gas pipelines, one-way valves, multiple solenoid valves, valve core bases, Supporting ribs, springs and movable conical valve core, the base of the valve core is fixed and installed at the entrance of the wind tunnel through the supporting ribs, the base of the valve core is provided with a ring cavity, and the ring cavity is arranged coaxially with the wind tunnel. There is a ventilation hole in the support rib, and the ventilation hole connects the driving pipeline assembly with the ring cavity, and the movable cone valve core is arranged inside the pneumatic actuator assembly, and the movable cone valve core is connected to the bottom of the ring cavity through a spring and Reciprocating and horizontally moving along the axis of the circular cavity, the end face of the movable frustum valve core is engaged and sealed with the tapered section when the wind tunnel is closed, and is flush with the end face of the tapered part of the base of the valve core when it is opened. The switching valve device proposed by the invention can reduce the damage of the hypersonic temporarily charged large-diameter wind tunnel and the valve plug, and improve the service life.

Description

technical field [0001] The invention belongs to the technical field of wind tunnel experiments, and more specifically relates to a fast switching valve device and a switching method for large-diameter wind tunnel applications. Background technique [0002] In aerospace research, a new principle or design often requires experimentation. There are generally three methods of experimentation: numerical simulation, wind tunnel test and flight test. Numerical simulation costs less, but the setting of boundary conditions required for simulation is often not accurate enough to simulate the flow in real conditions. Although the flight test can truly simulate the actual flight situation, it costs a lot of money, and only a limited number of sensors can be arranged to collect data. Compared with the first two methods, the cost of wind tunnel test is in the middle. Compared with the flight test, the wind tunnel test can measure the parameters of any position through multiple tests; c...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16K31/122F16K1/00F16K1/38G01M9/04
CPCF16K31/1221F16K1/00F16K1/38G01M9/04
Inventor 吴杰赵家权张臻薛涛
Owner HUAZHONG UNIV OF SCI & TECH