Plate bottom flexural-tensile stress monitoring system and method for existing runway surface structure

A technology of stress monitoring and bending and pulling, which is applied in the direction of measuring, measuring force, and measuring devices by measuring the change in optical properties of materials when they are stressed, can solve problems such as damage, high cost, and difficulty, and achieve high detection accuracy , fast speed and broad application prospects

Inactive Publication Date: 2019-01-11
CIVIL AVIATION UNIV OF CHINA
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Problems solved by technology

However, due to the weak structural performance of the fiber grating sensor, it is easy to cause damage due to construction or assembly during the pre-embedding process, and the survival rate of the sensor canno...

Method used

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  • Plate bottom flexural-tensile stress monitoring system and method for existing runway surface structure
  • Plate bottom flexural-tensile stress monitoring system and method for existing runway surface structure
  • Plate bottom flexural-tensile stress monitoring system and method for existing runway surface structure

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Embodiment Construction

[0011] The device and method for monitoring bending and tension stress at the bottom of the slab bottom for existing pavement structures provided by the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0012] like figure 1 — figure 2 As shown, the bending-tensile stress monitoring device for the bottom of the existing pavement structure provided by the present invention includes a plurality of fiber grating sensors 7, armored optical fibers 3, Main optical cable 4, fiber grating demodulator 5, main control terminal 6, splitter 8, optical fiber jumper 9 and temperature-compensated grating sensor; wherein each runway centerline lighting hole 1 and the grounding belt lighting hole 2 are separated on the side wall A plurality of fiber grating sensors 7 are installed at a distance, and are respectively connected to the output end of the splitter 8 through an optical fiber jumper 9 to form a test group; t...

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Abstract

The invention discloses a plate bottom flexural-tensile stress monitoring system and method for a existing runway surface structure. The plate bottom flexural-tensile stress monitoring system for theexisting runway surface structure comprises a plurality of fiber grating sensors installed in line light hoes and grounding strip light holes of the runway, an armored fiber, a main optical cable 4, afiber grating demodulator, a main control terminal, a deconcentrator, fiber jumpers and a temperature compensation grating sensor. The plate bottom flexural-tensile stress monitoring system and method for the existing runway surface structure uses a real plane load to act on the runway surface by means of the fiber grating sensors arranged in airway navigation light holes of an airport runway, and collects the grating refracted light wavelength at the position of the measuring point, so as to realize the measurement of the plate bottom flexural-tensile stress of the airport runway; therefore,not only the monitoring and early warning of airport runway surface damage can be realized, but also the problems such as damage to the existing runway surface and suspending air service for detection can be avoided; and the detection accuracy is high and the speed is fast, which has broad application prospects.

Description

technical field [0001] The invention belongs to the technical field of stress monitoring and pavement structure safety, and in particular relates to a system and method for monitoring bending and tension stress at the bottom of a slab used in an existing pavement structure. Background technique [0002] The runway is the most important infrastructure of the airport, which undertakes the tasks of aircraft takeoff and landing, taxiing and parking, and is the basic platform for the full play of the airport's functions. During the use of the concrete pavement of the airport runway, due to the joint action of the aircraft wheel load and environmental factors, various damage phenomena will often appear on the pavement before the end of its service life, and these damages cannot be predicted, which will bring great harm to the safety of aircraft operation. Very big threat. Therefore, it is particularly important to detect its structural performance and monitor its health. At pres...

Claims

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Application Information

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IPC IPC(8): G01L1/24
CPCG01L1/246
Inventor 蔡靖李岳张恒李少杰
Owner CIVIL AVIATION UNIV OF CHINA
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