Calibration device and method of rotor blade embedded micro pressure sensors

A technology of pressure sensors and rotor blades, which is applied to measuring devices, measuring fluid pressure, instruments, etc., can solve the problems of increasing sensor damage rate, failure to detect, and unguaranteed test accuracy, so as to enhance the reliability of sensors and improve Calibration efficiency, the effect of eliminating the influence of external factors

Inactive Publication Date: 2019-11-05
LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
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AI Technical Summary

Problems solved by technology

[0005] Secondly, because every test of the rotor blade needs to calibrate the pressure sensor, that is to say, every calibration must be carried out outside the blade, thus increasing the damage rate of the sensor;
[0006] Finally, because each test on the rotor blade needs to embed several sensors, it cannot be ruled out that the sensor has been damaged during the embedding process after sensor calibration, but it cannot be found, so that the accuracy of the test cannot be guaranteed.

Method used

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  • Calibration device and method of rotor blade embedded micro pressure sensors
  • Calibration device and method of rotor blade embedded micro pressure sensors

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Embodiment Construction

[0026] All features disclosed in this specification, or steps in all methods or processes disclosed, may be combined in any manner, except for mutually exclusive features and / or steps.

[0027] Any feature disclosed in this specification (including any appended claims, abstract and drawings), unless expressly stated otherwise, may be replaced by alternative features which are equivalent or serve a similar purpose. That is, unless expressly stated otherwise, each feature is one example only of a series of equivalent or similar features.

[0028] The rotor blade embedded miniature pressure sensor calibration device of this embodiment includes four parts: a constant temperature and constant pressure container, a data acquisition unit, a pressure adjustment unit, and a temperature adjustment unit.

[0029] The constant temperature and constant pressure container includes three parts: a sealed container, an observation window and a paddle tray. The sealed container is welded by low...

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Abstract

The invention discloses a calibration device method of rotor blade embedded micro pressure sensors. The device and the method aim to realize integral calibration of the embedded pressure sensors on arotor blade. The method specifically includes the steps that the micro pressure sensors are embedded in the rotor blade and then placed in a closed container, the pressure and temperature in the closed container are adjusted, data acquisition of the micro pressure sensors is completed through a data acquisition system outside the closed container after the target temperature and pressure are reached, and performance parameters of the micro pressure sensors are calibrated through a computer. Compared with a traditional embedding-after-calibration method, the calibration device achieves the integral calibration of the sensors after the sensors are embedded in the blade, the sensors embedded in the blade are calibrated before testing, and the influence of external factors before testing is avoided.

Description

technical field [0001] The invention relates to the field of wind tunnel tests, in particular to a calibration device and a calibration method for a miniature pressure sensor embedded in a rotor blade. Background technique [0002] Helicopters are different from other aircrafts. Because of their characteristics of hovering in the air, vertical take-off and landing, and low-speed maneuvering, they are widely used in military and civilian fields. With the expansion of its functional application, the research on helicopter technology has been continuously deepened. The unsteady load measurement of rotor blades is an important content in helicopter technology. The method of embedding pressure sensors on the surface of rotor blades is widely used at home and abroad, which has the characteristics of good test accuracy and high dynamic response frequency. [0003] In order to obtain accurate pressure data, the pressure sensor needs to be calibrated before the unsteady load test of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01L25/00G01L27/00
CPCG01L25/00G01L27/002
Inventor 尹熹伟张卫国卢翔宇任晓波史喆羽袁红刚
Owner LOW SPEED AERODYNAMIC INST OF CHINESE AERODYNAMIC RES & DEV CENT
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