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電子光学式変位計による航空機用耐熱材料の熱変形の測定
https://jaxa.repo.nii.ac.jp/records/45068
https://jaxa.repo.nii.ac.jp/records/45068f92dc6c6-0d54-4f4b-99e2-28595d4e9609
名前 / ファイル | ライセンス | アクション |
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naltr00810.pdf (1.7 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 電子光学式変位計による航空機用耐熱材料の熱変形の測定 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Thermal Deformation Measurements of Heat-Resistant Structural Materials for Aircraft by Electro Optical Displacement Transducer | |||||
著者 |
青木, 由雄
× 青木, 由雄× 多田, 保夫× AOKI, Yoshio× TADA, Yasuo |
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著者所属 | ||||||
航空宇宙技術研究所機体第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所機体第二部 | ||||||
著者所属(英) | ||||||
en | ||||||
Second Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Airframe Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-810 巻 810, p. 11, 発行日 1984-05 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | ポリイミド樹脂複合材の高温環境での材料特性データを得るために,電子光学式変位計を用いて熱膨張試験を室温~300度Cで行った。この変位計を高温変形測定に用いるためには,標点となる白,黒のターゲットを耐熱性の材質で作る必要がある。ここでは耐熱塗料を用いてターゲットを改良し,各繊維方向(0度,45度,90度)の熱膨張特性と温度の関係ならびに積層構成と熱による面外変形の関係を求めた。また,この手法をチタニウム合金(Ti-6A1-4V)材に適用し,室温~500度Cの温度において熱膨張試験,高温引張試験を行い,その有効性を立証した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Using an Electro Optical Displacement Transducer (EODT), thermal expansion tests ranging from room temperature up to 300C were conducted with sheet specimens of Glass/Polyimide composite laminates. The relations between thermal expansion properties and temperatures in fiber directions 0, 45 and 90 degree as well as those of stacking sequence of layers and out-of-plane deformation in heating were obtained by employing heat-resistant markers as the optical targets of the EODT. The technique was also adapted in thermal expansion and tension tests of Titanium alloy (Ti-6 A1-4V) specimens at temperatures ranging from room temperature to 500C, and the results demonstrated the validity of the present technique. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0810000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-810 |