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Water-absorbing ice-shaped cutter, ice-shaped measuring device and ice-shaped measuring method

A cutter and ice shape technology, applied in the field of wind tunnel test, can solve the problems of affecting fidelity, random freezing, destroying the shape of ice accretion, etc., and achieve the effect of simple structure, high fidelity and accurate ice shape

Active Publication Date: 2021-11-09
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the device cuts the nitrogen gas to blow off the ice and melted water, due to the low temperature of the nitrogen gas, it is easy to cause random freezing on the surface of the ice shape in the overflow of the water, destroying the shape of the ice accumulation, and affecting the fidelity of the ice shape acquisition. The device uses a hot knife Heating by means of electric heating, it is easy to cause electric shock accidents in the humid environment of icing wind tunnels, and the safety is not good
[0006] In addition, when nitrogen blows off ice and melted water, due to the low temperature of nitrogen, it is easy to cause random freezing on the surface of the ice shape during the process of water overflow, which affects the fidelity of ice shape acquisition

Method used

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  • Water-absorbing ice-shaped cutter, ice-shaped measuring device and ice-shaped measuring method
  • Water-absorbing ice-shaped cutter, ice-shaped measuring device and ice-shaped measuring method
  • Water-absorbing ice-shaped cutter, ice-shaped measuring device and ice-shaped measuring method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0054] like Figure 1 - Figure 10 As shown, the first embodiment of the present invention provides a water absorbent ice cutter, including a cutting assembly 10, a water supply assembly 30, a collector container 40, a gas supply assembly 50, an emitter 60, a water absorbing assembly 70;

[0055] The effluent of the water supply assembly 30 is coupled to the inlet of the emitter 60, and the water supply port of the water supply assembly 30 is connected to the effluent port of the collecting container 40;

[0056] The air intake port of the air supply assembly 50 is connected to a gas source, and the air outlet portion of the air supply assembly 50 is connected to the air outlet of the emitter 60;

[0057] The jet of the emitter 60 is connected to the inlet of the cutting assembly 10, and the outlet of the cutting assembly 10 is connected to the heat recovery port of the collecting container 40, the cutting assembly (10) forms a receiving chamber; The water absorbing assembly 70 is a...

Embodiment 2

[0107] This Example 2 provides an ice-shaped measuring device (not shown in the drawings), including a measuring bracket, a measuring plate, a square paper, and a water absorbent ice cutter according to any one of embodiments 1. The square paper is placed on the measuring board, the measuring plate and the ice cutter on the bracket, the measuring plate and the ice cutter to move along the bracket, and The measuring plate is located above the ice cutter.

[0108] In the above scheme, the ice cutter is slid on on the measuring bracket, and the measuring plate also slides on the measuring bracket, the measuring plate is mounted above the ice cutter, and the moving ice cutter is relative to the position of the measuring bracket, First move the ice cutter to the one side of the aircraft model, and then the arc of the cut portion needs to move along the aircraft model and cut until the desired ice is cut; then move the position on the measuring bracket The ice of the position is measure...

Embodiment 3

[0111] like Figure 11 As shown, this Example 3 provides a method of using the above-described ice-shaped measuring device for ice-shaped measurement, including the following steps:

[0112] Step S10: The ice-shaped measuring device as described in Example 2 is placed in the wind tunnel;

[0113] Step S20: Adjust the height of the ice cutter relative to the measurement bracket to the desired measurement of the measuring ice position;

[0114] Step S30: Move the ice cutter horizontally to the target height of the aircraft model, the ice cutter is telescopically move along the aircraft model until after cutting out the gap, the ice cutter stops moving, moving the ice cutter away from Aircraft model;

[0115] Step S40: Adjusting the height of the measurement plate as height at the time of cutting the ice cutter;

[0116] Step S50: Move the measuring board horizontally to the cutting slit, insert the pre-cut front fang surface and the aircraft model with the aircraft model in the slit ...

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Abstract

The invention is applicable to the technical field of wind tunnel test, and provides a water-absorbable ice-shaped cutter, an ice-shaped measuring device and an ice-shaped measuring method, wherein the water-absorbable ice-shaped cutter includes a cutting assembly, a water supply assembly, a water collection container, an air supply component, ejector, and water-absorbing component; the water outlet of the water supply component is connected to the water inlet of the ejector, the water inlet of the water supply component is connected to the water outlet of the water collection container; the air inlet of the air supply component is connected to the air source, and the The hot air outlet of the gas assembly is connected to the air inlet of the ejector; the air ejector of the ejector is connected to the inlet of the cutting assembly, the outlet of the cutting assembly is connected to the heat recovery port of the water collection container, and the cutting assembly forms an accommodation cavity; The assembly is at least partly located in the accommodating cavity, and the water absorbing assembly is used for absorbing the water generated during cutting by the cutting assembly; the water inlet, the air inlet, and the air injection port of the ejector communicate with each other. The method of the invention can absorb water during the cutting process, and the obtained ice shape has high fidelity.

Description

Technical field [0001] The present invention relates to a wind tunnel test field, and more particularly to a water absorbent ice cutter, an ice measuring device, and an ice measurement method. Background technique [0002] When the aircraft is rich in low-temperature clouds rich in cold droplets, their winding surface is prone to the phenomenon of frozen, and the ice phenomenon has a serious threat to the flight safety of the aircraft. Therefore, the aircraft model ice test is carried out in the froble wind tunnel. It is known as an important part of the design and verification of the aircraft to prevent ice system. [0003] In the Ice wind tunnel test for the aircraft model, it is necessary to accurately obtain two-dimensional cross-sectional shapes (Ice), and the accuracy and speed of ice acquisition directly affect the quality efficiency of the test. In the prior art, the acquisition method of frozen air-blowing ice is mainly hot knife cuts, which can be divided into two categ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F25C5/08G01M9/02G01M9/06G01M9/08
CPCF25C5/08G01M9/02G01M9/06G01M9/08
Inventor 张平涛郭龙易贤张轲孙才国李自雨
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT