飞机蒙皮
- 网络Aircraft skin;aircraft envelope
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为提高飞机蒙皮的维修质量,研究了飞机蒙皮表面铈转化膜表面改性技术。
The surface modification of LY12 Al-alloy based aircraft envelope by cerium conversion coating was studied , aiming at improving the repairing quality of the aircraft envelope .
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飞机蒙皮修理补片气动力的计算
Aerodynamic - Force Calculation for Repaired Patch of Aircraft Envelope
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本文对高平均功率高重复率TEACO2激光器应用于飞机蒙皮激光脱漆进行了较为系统的研究。
Research is carried out for paint stripping of aircraft using high power high repetition rate TEA CO_2 laser in this paper .
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介绍了飞机蒙皮拉形过程有限元分析软件的前后置处理系统POPPS。
In this paper , the pre and post process system ( POPPS ) for stretch forming simulation with FEM is presented .
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飞机蒙皮拉形过程的有限元数值模拟
Finite Element Numerical Simulation of Stretch Forming Processes of Aircraft Skin
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氟化改性丙烯酸树脂的合成及在飞机蒙皮涂料中的应用
Synthesis of Fluorocarbon Modified Acrylic Resin and Its Application in Dope
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飞机蒙皮局部腐蚀的原位快速修复工艺
In-Situ rapid renovation process for local corrosion area of aircraft skin
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对1411铝锂合金作飞机蒙皮的可行性研究
A Study of Application Feasibility of AI-Li Alloy 1441 for Fuselage
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基于回弹的飞机蒙皮拉形模型面修模技术研究
Surface Improvement Based on Springback Compensation for Aircraft Skin Stretching Tool
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加载轨迹是决定飞机蒙皮拉伸成形质量的关键因素。
Loading trajectory is the key factor for aircraft skin stretch forming .
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胶补飞机蒙皮补片形状优化研究
Research on optimizations of patch shape for bonding repair of aircraft skin
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光固化复合材料补片在飞机蒙皮修复中的应用
Application of Ultraviolet Curing Composite Patch in Aircraft Skin Repair
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飞机蒙皮表面预处理的研究进展
The Research Progress of Pretreatment of the Airplane Surface
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目前2524铝合金是飞机蒙皮的主流材料。
Currently 2524 aluminum alloy has become the main material of aircraft skin .
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基于红外锁相法的飞机蒙皮损伤检测试验研究
Experimental Research on Damage in the Airplane Skin by Means of Lock-In Thermography
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目前铆接技术仍然是飞机蒙皮连接的主流技术。
Currently , the riveting is the main connection technologies of aircraft skin .
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求解飞机蒙皮耦合热效应的壁面热流函数法
The wall heat flux function for solving coupled heat transfer of aircraft skin
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飞机蒙皮拉形计算机辅助工程系统ASSFCAE
Computer aided engineering system for aircraft stretch forming
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飞机蒙皮激光脱漆技术研究
Study on Laser Paint Stripping of Aircraft Surface
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双曲度飞机蒙皮拉伸成形轨迹优化与验证
Optimization and Validation of Loading Trajectory for Double Curve Aircraft Skin Stretch Forming Process
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飞机蒙皮裂纹的数学形态学识别方法
Morphological Recognition Method of Aircraft Skin Cracks
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搅拌摩擦焊接技术成为飞机蒙皮连接的重要发展方向。
Friction stir welding technology has become the most important development trend of aircraft skin connection .
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飞机蒙皮包覆拉伸成形加载轨迹设计优化方法皮带拉幅机,带式拉幅机
Design and optimization of the loading trajectory in aircraft skin drape forming process belt stretching machine
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氟碳飞机蒙皮涂料的研制
Development of Fluorocarbon Aircraft Dope
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研究了飞机蒙皮检查机器人的系统结构及相关关键技术。
The system structure and related key technologies of the robot used to inspect the aircraft skin defects are studied .
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国外已经将其应用于飞机蒙皮、汽车发动机箱体等零部件的加工制造中。
It have been applied to aircraft skin , car engine parts abroad , such as the box in the processing .
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前飞状态倾转旋翼机气弹稳定性建模基于回弹的飞机蒙皮拉形模型面修模技术研究
Modeling study on tilt-rotor 's aeroelastic stability in cruise flight Surface Improvement Based on Springback Compensation for Aircraft Skin Stretching Tool
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数字化成形制造技术在航空制造领域的不断推广和应用,使飞机蒙皮从传统的经验型向科学型制造模式转变。
The increasing application of numerical forming technology to aircraft manufacturing propels the shift of manufacturing from experiential mode to scientific mode .
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成果将可应用于检测飞机蒙皮或其他部件深处的细小缺损,对保障飞机安全,提高飞行可靠性和延长飞机寿命等方面有重要意义。
The achievements can be applied to detect small defects in aircraft skin and other components , which is meaningful for aircraft safety .
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飞机蒙皮温度场是形成飞机红外图像的基本因素,掌握其瞬态分布特性与控制机制对于飞机相关的红外技术有重要帮助。
The aircraft skin temperature is a basic factor determining the infrared image of aircraft , so the knowledge on the transient temperature is important .