A Calculation Method of High Pressure Air Resource Consumption in Wind Tunnel Group

A high-pressure air and resource consumption technology, applied in the field of wind tunnel testing, can solve problems such as being unsuitable for wind tunnel group consumption measurement, and achieve the effect of high-pressure air resource consumption and cost saving

Active Publication Date: 2022-06-03
CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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Problems solved by technology

[0009] The purpose of the present invention is to provide a calculation method for the consumption of high-pressure air resources in wind tunnel groups, aiming to solve the technical problem that the calculation method in the prior art is not suitable for the measurement of wind tunnel group consumption

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  • A Calculation Method of High Pressure Air Resource Consumption in Wind Tunnel Group
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  • A Calculation Method of High Pressure Air Resource Consumption in Wind Tunnel Group

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Embodiment Construction

[0040] Aspects of the present invention will be described more fully hereinafter with reference to the accompanying drawings. However, the present invention may have

[0041] The terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the present disclosure. use here

[0045] Figure 1 is a schematic diagram of the physical topology between the high-pressure air system and the wind tunnel.

[0066] (3) software part: mainly for data consumption statistics, pipeline topology visualization and so on.

[0069] It should be noted that the pipelines in this application, if not specified, all include two parts of the gas transmission main pipe and the gas transmission branch pipe.

[0076]

[0079]

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Abstract

The present invention is applicable to the technical field of wind tunnel test, and provides a method for calculating the consumption of high-pressure air resources in a wind tunnel group, which includes the following steps: constructing a topology model; establishing a monitoring system; collecting the status of the wind tunnel being tested in the wind tunnel group , collect the state of the high-pressure air system; obtain the pressure difference of the tank group consumed by the wind tunnel being tested; update the topology model; traverse the updated topology model to obtain the guaranteed volume of the wind tunnel being tested; calculate the wind tunnel being tested by the differential pressure method The high-pressure air resource consumption of the cave; the high-pressure air system includes a high-pressure unit, a high-pressure tank group, a main gas pipeline, gas pipelines, and valves. The present invention expresses the actual physical topology relationship between the high-pressure air system and the wind tunnel by building a model. Therefore, the calculation method of the high-pressure air resource consumption of the wind tunnel group in the embodiment of the present invention can automatically identify The high-pressure tank group, gas main pipe, and gas branch pipes in use in the wind tunnel.

Description

A calculation method for high pressure air resource consumption in wind tunnel clusters technical field The invention belongs to the technical field of wind tunnel test, particularly relate to a kind of calculation method of high pressure air resource consumption of wind tunnel group Law. Background technique Large-scale wind tunnel equipment and facilities are important national strategic resources, aerospace, ground transportation, building bridges, Wind tunnel tests are required in many fields such as renewable energy and environmental protection. According to the gas velocity in the cave, wind tunnels are generally divided into Low speed, high speed, ultra-high speed and other types, each type of wind tunnel is divided according to the diameter of the test section, test type, test time, etc. The points are further divided into large / small, conventional / special (such as icing, acoustics, low temperature, etc.), transient / continuous and other different wind tunnel...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/18G06F16/23
CPCG06F17/18G06F16/23
Inventor 罗昌俊司洞洞王小飞马永一郑娟袁宗泽明丽洪
Owner CALCULATION AERODYNAMICS INST CHINA AERODYNAMICS RES & DEV CENT
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