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飞机外部噪声预计系统在适航测试中的应用
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作者 侯峰 秦浩明 师成梅 《结构强度研究》 2010年第2期19-23,共5页
为满足飞机适航噪声验证试验的需求,根据CCAR-36部中有关飞机适航噪声测试规定,归纳了适航噪声测试的根本目的,采用飞机外部噪声预计系统(AEPN)对某型号飞机发动机进行了外场噪声预计和分析,提出等效航迹和确定地面测试区域的工... 为满足飞机适航噪声验证试验的需求,根据CCAR-36部中有关飞机适航噪声测试规定,归纳了适航噪声测试的根本目的,采用飞机外部噪声预计系统(AEPN)对某型号飞机发动机进行了外场噪声预计和分析,提出等效航迹和确定地面测试区域的工程方法,解决了如何准确和完整记录最大噪声10分贝降区域这一关键的适航噪声测试试验问题。 展开更多
关键词 噪声测试 噪声预计 适航测试
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TEST AND CONTROL SYSTEM DEVELOPMENT AND APPLICATION OF LANDING GEAR DROP TEST RIG 被引量:3
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作者 薛彩军 戚文刚 聂宏 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2011年第2期145-151,共7页
A control and test system of a landing gear drop test rig is developed considering the drop test specifica- tions for the "Seagull 300" multi-functional amphibious airplane. In order to realize the automation of dro... A control and test system of a landing gear drop test rig is developed considering the drop test specifica- tions for the "Seagull 300" multi-functional amphibious airplane. In order to realize the automation of drop test process, a servo system is proposed and programmable logic controller(PLC) technology is used. Several key technologies for measuring the horizontal load, the vertical load and the transient rotational speed are studied. According to the requirements of CCAR-23-R3, the drop test of landing gears of the "Seagull 300" airplane is accomplished. Test results show that the system has a high accuracy of data collection. The system is stable and reliable. The drop test satisfies the requirements of the drop test specifications and the results can be used as the certification of airworthiness for this kind of airplane. 展开更多
关键词 drop test test and control system AIRWORTHINESS landing gears
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机载数字音频系统架构及关键要素符合性研究 被引量:1
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作者 罗斌 李华 +2 位作者 雒嘉 孙淑光 王凯 《长江信息通信》 2021年第2期95-98,共4页
机载音频系统的通话质量直接关系到飞机的飞行安全,话音信号的清晰度及通话时延会影响到飞行员对话音信号的接收及心理感受。根据机载音频系统最小性能标准要求,给出基于AFDX的机载数字音频系统的整体架构方案,并对该架构下的系统信息... 机载音频系统的通话质量直接关系到飞机的飞行安全,话音信号的清晰度及通话时延会影响到飞行员对话音信号的接收及心理感受。根据机载音频系统最小性能标准要求,给出基于AFDX的机载数字音频系统的整体架构方案,并对该架构下的系统信息处理技术的选择及传输时延进行分析计算,分析表明,该架构设计可以满足机载通信系统的性能要求。提供了相应架构下的数字音频系统关键指标的适航符合性测试方案,为机载数字音频系统的设计研发提供依据。 展开更多
关键词 机载数字音频 AFDX 系统架构 传输时延 适航测试
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The Study on the Occupants Protection of the Emergency Landing Condition for Part 23 Airplane
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作者 Hae Sun Lee Yeung Woo Kim Jong Min Yoon 《Journal of Physical Science and Application》 2014年第7期412-419,共8页
The part 23 airworthiness standards for small airplanes states minimal standards of the emergency condition for the occupant protection. Under this regulation, the airplane must be designed and certified about static ... The part 23 airworthiness standards for small airplanes states minimal standards of the emergency condition for the occupant protection. Under this regulation, the airplane must be designed and certified about static strength of the fuselage and seats, horizontal and vertical dynamic strength of seats. Human injuries in dynamic crash tests and the survivability in the turnover condition should be also evaluated. The most important part among injuries of human is a head and the head injury is evaluated by Head Injury Criterion (HIC). KC-100, 4 seats airplane that is manufactured by KAI, was conducted seat dynamic tests. The HIC from tests was well within criteria limits 1,000 and the occupant compartment for head protection provided hazard-free spaces in the occupant's head strike envelope for the frontal-horizontal crash impacts. The airplane also was conducted a turnover static test and analysis to especially show living spaces of the head. The airframe could sustain living spaces for occupants in the turnover condition and occupants could escape and be protected. The results of tests and analysis corresponded to the criteria and proved the retention of survivable space in emergency landing condition. 展开更多
关键词 HIC head injury criterion emergency landing turnover test seat dynamic test.
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Local Path Planning Method of the Self-propelled Model Based on Reinforcement Learning in Complex Conditions
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作者 Yi Yang Yongjie Pang +1 位作者 Hongwei Li Rubo Zhang 《Journal of Marine Science and Application》 2014年第3期333-339,共7页
Conducting hydrodynamic and physical motion simulation tests using a large-scale self-propelled model under actual wave conditions is an important means for researching environmental adaptability of ships. During the ... Conducting hydrodynamic and physical motion simulation tests using a large-scale self-propelled model under actual wave conditions is an important means for researching environmental adaptability of ships. During the navigation test of the self-propelled model, the complex environment including various port facilities, navigation facilities, and the ships nearby must be considered carefully, because in this dense environment the impact of sea waves and winds on the model is particularly significant. In order to improve the security of the self-propelled model, this paper introduces the Q learning based on reinforcement learning combined with chaotic ideas for the model's collision avoidance, in order to improve the reliability of the local path planning. Simulation and sea test results show that this algorithm is a better solution for collision avoidance of the self navigation model under the interference of sea winds and waves with good adaptability. 展开更多
关键词 self-propelled model local path planning Q learning obstacle avoidance reinforcement learning
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