KAMEYAMA Masaki

カメヤママサキ | KAMEYAMA Masaki

Affiliation and department：
Job title： Associate Professor

Research field (3)： Aerospace engineering , Machine materials and mechanics , Mechanics and mechatronics

Research theme for competitive and other funds (28)：

2022 - 2024 熱残留変形レス非対称積層を活用した高性能複合材サンドイッチ構造の一括積層造形
2020 - 2022 Novel Internal-Deformation Control to Bridge Fidelity Gap in Variable-Wing Aircraft Modeling
2019 - 2022 積層複合材構造の実時間衝撃荷重同定の高精度化と高速衝撃荷重同定への応用
2022 - モーターの振動目標仕様の策定
2018 - 2021 Unified Control Theory of Semi-Active Vibration Suppression and Predictive Control to Enable Complete Prediction of Vibration

2018 - 2020 New concept "local joint coordinates" to break down the barrier of flexible deployable wing model between 2-D and 3-D dimensions

2020 - 2020 最適化技術による複合材/粘弾性材サンドイッチ構造の高性能化

2013 - 2015 Powerful power-generation by using in underhanded way aeroelastic instability of growing vibration

2011 - 2014 Smart Sensing and Actuation of CFRP structures with Piezoelectric Materials

2013 - Piezoelectric energy harvesting from structural vibration

2011 - 2012 多入力圧電繊維アクチュエータを用いたスマート複合材構造の損傷モニタリング

2010 - 2011 Non-powered structural health monitoring using piezoelectric sensor and energy harvesting

2009 - 2010 スマート複合材構造の効率的モード別振動計測・制御法の構築と航空宇宙構造への応用

2008 - 2010 Real-time Damage Monitoring of Aerospace CFRP Structures Based on Exper imental Impact Force Identification

2007 - 2009 Research on highly accurate structural health monitoring based on the Lamb wave propagation analysis for composites structures

2008 - 2008 新融合研究領域展開プロジェクトの支援(革新誘電材料を用いた知的構造物の最適設計)

2006 - 2008 飛翔体構造の実時間異物衝突監視システムの構築

2005 - 2007 IMPACT DAMAGE MONITORING OF AIRCRAFT COMPOSITE STRUCTURES WITH PIEZOELECTRIC SENSORS

2004 - 2005 Real-time health monitoring based on identification of impact force for composite structures embedded with piezoelectric sensors

2002 - 2005 Smart-Patch Repair Engineering of Aging Aircraft and Spacecraft Structures

2003 - 2004 REAL-TIME HEALTH MONITORING OF COMPOSITE STRUCTURES BASED ON ACTIVE SENSING

2002 - 2003 圧電アクチュエータ・センサを用いた複合材スマート翼構造のフラッタ抑制法の研究

2001 - 2002 DAMAGE IDENTIFICATION OF SMART COMPOSITE STRUCTURES USlNG PlEZOELECTRlC ACTUATORS AND SENSORS

1999 - Vibration Measurement/Control of Composite Structures

1998 - Health Monitoring of Composite Structures

1997 - Optimum Design of Composite Structures

AI援用積層最適化によるCFRP設計・製造自動化技術の開発

騒音・振動の発生位置検出と要因分析に関する研究

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Papers (30)：

Masaki KAMEYAMA, Atsushi TAKAHASHI, Masahiro ARAI. Damping Optimization of Symmetrically Laminated Plates with Transverse Shear Deformation using Lamination Parameters. Advanced Composite Materials. 2019. 28. 1. 1-26
亀山正樹, 笠原尚哉, 石川皓士, 槙原幹十朗. 平板の超音速パネルフラッタ振動を利用した圧電振動発電における圧電素子最適配置. 日本航空宇宙学会論文集. 2018. 66. 2. 47-52
Masaki KAMEYAMA, Masahiro ARAI. Optimal Design of Symmetrically Laminated Plates for Damping Characteristics using Lamination Parameters. Composite Structures. 2015. 132. 885-897
Masaki Kameyama, Hisao Fukunaga. Single modal vibration control of laminated plates based on the optimal placement of a sensor and an actuator. IFAC Proceedings Volumes (IFAC-PapersOnline). 2010. 18. 1. 235-240
KAMEYAMA Masaki, TAKAYANAGI Nobutaka, FUKUNAGA Hisao. Semi-Active Vibration Control of CFRP Beam Structures Using Piezoelectric Energy Harvesting. JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2010. 58. 683. 340-348

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MISC (13)：

上田政人, 水口周, 横関智弘, 松尾剛, 安岡哲夫, 仲井朝美, 田中基嗣, 山本剛, 亀山正樹, 吉村彰記, et al. 第22回国際複合材料会議報告. 日本複合材料学会誌. 2020. 46. 2. 68-78
YAMADA Takayuki, SUGENO Mitsutoshi, KAMEYAMA Masaki, FUKUNAGA Hisao. 1502 Semi-Active Vibration Control of CFRP Plates Using Piezoelectric Devices. The Computational Mechanics Conference. 2010. 2010. 23. 582-584
MIYAMOTO Yuji, KAMEYAMA Masaki, FUKUNAGA Hisao. 170 Vibration Control of Plates based on the Optimal Placement of Piezoelectric Fiber Actuators. 2010. 2010. 45. 140-141
亀山正樹. 流体・構造の連成効果を利用した構造設計. ながれ. 2009. 28. 4. 291-296
亀山正樹. 圧電材料を用いたCFRP構造の振動制御. 強化プラスチックス. 2009. 55. 6. 222-229

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Lectures and oral presentations (45)：

Optimal Design of Viscoelastic Laminated Sandwich Composite Structures considering Thermally-induced Deformation of Composite Skins using Lamination Parameters
(20th US-Japan Conference on Composite Materials 2024)
Optimal Design of Composite Plate Wings for Aeroelastic Characteristics based on Complex Modulus Approach
(20th International Conference on Flow Dynamics 2023)
Optimal Design of CFRP Laminated Plates with an Interleaved Viscoelastic Damping Layer using Lamination Parameters
(Asian Congress of Structural and Multidisciplinary Optimization 2022 2022)
MultiObjective Optimization of Stacking Sequence Design for Asymmetric Laminated Plates under Several Laminate Configuration Constraints
(Asian Congress of Structural and Multidisciplinary Optimization 2020 2020)
Piezoelectric Energy Harvesting from Panel Flutter Oscillation of Laminated Plates
(Second International Symposium on Flutter and its Application 2020)

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Education (2)：

1995 - 1997 Tohoku University
1991 - 1995 Tohoku University Faculty of Engineering

Professional career (1)：

博士(工学) (東北大学)

Work history (4)：

2010/04 - 現在 Shinshu University Faculty of Engineering
2007/04 - 2010/03 Tohoku University Graduate School of Engineering
2008/08 - 2009/03 ワシントン大学客員研究員
1997/10 - 2007/03 Tohoku University Graduate School of Engineering

Awards (2)：

2011/05/25 - 日本複合材料学会日本複合材料学会論文賞
2005/04/06 - 日本航空宇宙学会日本航空宇宙学会奨励賞

Association Membership(s) (4)：

米国航空宇宙学会 , 日本航空宇宙学会 , 日本複合材料学会 , 日本機械学会

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