Structural Health Monitoring of Composite Cryogenic Propellant Tanks Using Optical Fiber Sensors
| Project/Area Number |
15360447
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | The University of Tokyo |
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Principal Investigator |
TAKEDA Nobuo The University of Tokyo, Graduate School of Frontier Sciences, Professor, 大学院・新領域創成科学研究科, 教授 (10171646)
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| Co-Investigator(Kenkyū-buntansha) |
OKABE Yoji The University of Tokyo, Graduate School of Engineering, Lecturer, 大学院・工学系研究科, 講師 (90313006)
MIZUTANI Tadahito The University of Tokyo, Graduate School of Frontier Sciences, Research Associate, 大学院・新領域創成科学研究科, 助手 (00401232)
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| Project Period (FY) |
2003 – 2005
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| Project Status |
Completed (Fiscal Year 2005)
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| Budget Amount *help |
¥15,300,000 (Direct Cost: ¥15,300,000)
Fiscal Year 2005: ¥3,600,000 (Direct Cost: ¥3,600,000)
Fiscal Year 2004: ¥5,300,000 (Direct Cost: ¥5,300,000)
Fiscal Year 2003: ¥6,400,000 (Direct Cost: ¥6,400,000)
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| Keywords | composite materials / cryogenic temperature / structural health monitoring / optical fiber / FBG sensor / reusable launch vehicle / strain / transverse crack |
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| Research Abstract |
A reusable launch vehicle is attracting much interest as one of promising future space transportation systems. Advanced composite cryogenic tanks are necessary to achieve an affordable light-weight vehicle. It is highly demanded to establish the structural integrity and reliability of such composite tanks because failure mechanisms of composite tanks are very complicated and are not well understood. The purpose of the present study is to establish a real-time health-monitoring technology to continuously monitor the strains and temperatures using optical fiber sensors embedded in composite cryogenic tanks.
First, we adhered FBG (fiber Bragg grating) sensors on CFRP tanks in an experimental reusable launch vehicle, and measured the strains and temperatures in real time using a telemetry system during a launch-return cycle. The validity of the measuring method was proven and some fundamental problems were clarified.
Then, we embedded several FBG sensors in filament-wound CFRP tanks. Small-diameter optical fibers (52 μm in diameter including the coating) were used to avoid the strength reduction due to the embedment. A new FBG temperature sensor was proposed to distinguish the temperature and the mechanical strain. An optimum measurement procedure was studied to obtain reliable strains and temperatures through comparison between experiments and theoretical prediction. Continuous monitoring was conducted during the entire fabrication cycle of filament-wound CFRP tanks. Effects of various fabrication conditions on thermal residual strains were studied. Detection of transverse cracks was also successfully made during the pressuring stage of CFRP tanks through the measurement of FBG reflection spectra.
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Report
(4 results)
Research Products
(25 results)
