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Impact of Ground Effect on Airplane Lateral Directional Stability during Take-Off and Landing 被引量:2
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作者 M. Sereez N. Abramov M. G. Goman 《Open Journal of Fluid Dynamics》 2018年第1期1-14,共14页
Computational simulations of aerodynamic characteristics of the Common Research Model (CRM), representing a typical transport airliner are conducted using CFD methods in close proximity to the ground. The obtained dep... Computational simulations of aerodynamic characteristics of the Common Research Model (CRM), representing a typical transport airliner are conducted using CFD methods in close proximity to the ground. The obtained dependencies on bank angle for aerodynamic forces and moments are further used in stability and controllability analysis of the lateral-directional aircraft motion. Essential changes in the lateral-directional modes in close proximity to the ground have been identified. For example, with approach to the ground, the roll subsidence and spiral eigenvalues are merging creating the oscillatory Roll-Spiral mode with quite significant frequency. This transformation of the lateral-directional dynamics in piloted simulation may affect the aircraft responses to external crosswind, modify handling quality characteristics and improve realism of crosswind landing. The material of this paper was presented at the Seventh European Conference for Aeronautics and Space Sciences EUCASS-2017. Further work is carried out for evaluation of the ground effect aerodynamics for a high-lift configuration based on a hybrid geometry of DLR F11 and NASA GTM models with fully deployed flaps and slats. Some aspects of grid generation for a high lift configuration using structured blocking approach are discussed. 展开更多
关键词 CFD HIGH-LIFT CONFIGURATION Ground Effect airplane Stability Lateral-Directional MODES
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IAP's Solar-Powered Unmanned Surface Vehicle Actively Passes through the Center of typhoon Sinlaku(2020) 被引量:3
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作者 Hongbin CHEN Jun LI +6 位作者 Wenying HE Shuqing MA Yingzhi WEI Jidong PAN Yu ZHAO Xuefen ZHANG Shuzhen HU 《Advances in Atmospheric Sciences》 SCIE CAS CSCD 2021年第4期538-545,共8页
The solar-powered marine unmanned surface vehicle(USV) developed by the USV team of the Institute of Atmospheric Physics is a rugged, long-duration, and autonomous navigation vessel designed for the collection of long... The solar-powered marine unmanned surface vehicle(USV) developed by the USV team of the Institute of Atmospheric Physics is a rugged, long-duration, and autonomous navigation vessel designed for the collection of longrange, continuous, real-time, meteorological and oceanographic measurements, especially under extreme sea conditions(sea state 6–7). These solar-powered USVs completed a long-term continuous navigation observation test over 26 days.During this time, they coordinated double-USV observations and actively navigated into the path of Typhoon Sinlaku(2020) before collecting data very close to its center during the 2020 USV South China Sea Typhoon Observation Experiment. Detailed high temporal resolution(1 min) real-time observations collected by the USV on the typhoon were used for operational typhoon forecasting and warning for the first time. As a mobile meteorological and oceanographic observation station capable of reliable, automated deployment, data collection, and transmission, such solar-powered USVs can replace traditional observation platforms to provide valuable real-time data for research, forecasting, and early warnings for potential marine meteorological disasters. 展开更多
关键词 solar-powered unmanned surface vehicle TYPHOON meteorological and oceanographic observation
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Compatible Design of the System to Detect Ships and Airplanes with a Ground Wave Over-the-horizon Radar
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作者 沈一鹰 《High Technology Letters》 EI CAS 1997年第2期66-69,共4页
This paper provides a design method based on a time-shared form, which obtains the compatibility of signal and the system for detecting both ships and airplanes. Then, it gives the structure diagram of the system and ... This paper provides a design method based on a time-shared form, which obtains the compatibility of signal and the system for detecting both ships and airplanes. Then, it gives the structure diagram of the system and the chart diagram of signal processing. Finally, the continuity problem of signal modulation for ship detection is discussed. 展开更多
关键词 Compatible DESIGN Ship and airplane detection OVER-THE-HORIZON radar
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Analysis of Airplane Precipitation Operation on Embedded Convective Clouds in Hunan Province
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作者 Zhang Zhongbo Xu Dongying Wang Ling 《Meteorological and Environmental Research》 CAS 2015年第11期9-15,共7页
Based on NCEP 1°×1° reanalysis data, ground encryption houdy precipitation, FY-2E stationary satellite and Doppler radar data, the structural characteristics of precipitation clouds in Hunan Province an... Based on NCEP 1°×1° reanalysis data, ground encryption houdy precipitation, FY-2E stationary satellite and Doppler radar data, the structural characteristics of precipitation clouds in Hunan Province and the effects of airplane precipitation operation were analyzed. The results show that under the effects of low-pressure system and southwest monsoon, Hunan was rich in water vapor, which was beneficial to the maintaining of precipitation clouds. During the process of the artificial precipitation operation over Hunan Province, convection developed vigorously, and precipita- tion was strong in the south of the province; embedded convective clouds were dominant and precipitation was weak in the east of the province. Cloud optical thickness correlated with ground precipitation positively. After catalyzing, echo at high altitudes responded firstly, and the echo intensi- ty increased gradually; the response of low-altitude echo lagged behind that of high-altitude echo. It shows that catalysis could lead to increase of upper precipitation particles in size and quantity. As time goes on, upper precipitation particles descended to low altitudes, so that echo intensity in- creased at low altitudes. It is clearly seen that catalysis could lead to increase of echo intensity and prolong the lifetime of target clouds to improve the area of strong echo zone, showing obvious positive catalytic effect. At the same time, houdy average precipitation in the affected region tended to increase stably and was obviously more than that of the contrast region where hourly average precipitation reduced gradually with time. The changing trend of hourly average precipitation in the affected region correlated positively with the response of radar echo. 展开更多
关键词 Embedded convective clouds airplane precipitation operation Doppler radar Cloud structure Catalytic effect China
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Cost Comparision of Airplane Parking Methods at Apron of Maptuto International Airport
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作者 Jose F.R.Diogo 张华 《Journal of Southwest Jiaotong University(English Edition)》 2007年第1期40-44,共5页
Three known designs for parking, frontal, angled and parallel, were presented. Aircrafts at aprons can be parked either by towing equipment (push-back) or by its own power (serf-powered parking). The costs of thes... Three known designs for parking, frontal, angled and parallel, were presented. Aircrafts at aprons can be parked either by towing equipment (push-back) or by its own power (serf-powered parking). The costs of these two methods for Maputo International Airport were investigated. Based on airplane parking design theory, formulas to calculate the annual maintenance cost at aprons were proposed. Calculation results indicate that self-powered parking is preferable, justified by the fact that this airport has low traffic volume. The system of aircraft parking adopted by this airport saves significantly the cost for purchase and subsequent maintenance of push-back. 展开更多
关键词 airplane parking Push-back equipment Self-powered parking
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Robust Speech Endpoint Detection in Airplane Cockpit Voice Background
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作者 Hongbing CHENG Ming LEI +1 位作者 Guorong HUANG Yan XIA 《Wireless Sensor Network》 2009年第5期489-495,共7页
A method of robust speech endpoint detection in airplane cockpit voice background is presented. Based on the analysis of background noise character, a complex Laplacian distribution model directly aiming at noisy spee... A method of robust speech endpoint detection in airplane cockpit voice background is presented. Based on the analysis of background noise character, a complex Laplacian distribution model directly aiming at noisy speech is established. Then the likelihood ratio test based on binary hypothesis test is carried out. The decision criterion of conventional maximum a posterior incorporating the inter-frame correlation leads to two separate thresholds. Speech endpoint detection decision is finally made depend on the previous frame and the observed spectrum, and the speech endpoint is searched based on the decision. Compared with the typical algorithms, the proposed method operates robust in the airplane cockpit voice background. 展开更多
关键词 Complex LAPLACIAN Model Maximum A POSTERIOR Criterion LIKELIHOOD Ratio Test Speech End- point Detection airplane COCKPIT VOICE
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Asia's Largest Airplane Workshop
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《China's Foreign Trade》 1997年第8期37-37,共1页
The four-airplane repair workshop built and put into operation in May 1996 by the Beijing Airplane Maintenance Engineering Co. Ltd is the largest one in Asia at present. At the 1990s world advanced level, it marks the... The four-airplane repair workshop built and put into operation in May 1996 by the Beijing Airplane Maintenance Engineering Co. Ltd is the largest one in Asia at present. At the 1990s world advanced level, it marks the fact that the maintenance facilities and technology of China’s civil aviation have entered the world’s advanced rank. 展开更多
关键词 Asia’s Largest airplane Workshop CO
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To Understand Why Airships Lost the Sky to Airplanes Take a Look at the Network on the Ground
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作者 Helmut E. Braun 《History Research》 2013年第1期23-30,共8页
关键词 飞艇 飞机 网络 地面 商业竞争 经济损失 成本效益 点对点
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Effect of airplane transport of donor livers on post-liver transplantation survival
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作者 Yi Huang Gerry MacQuillan +7 位作者 Leon A Adams George Garas Megan Collins Albert Nwaba Linjun Mou Max K Bulsara Luc Delriviere Gary P Jeffrey 《World Journal of Gastroenterology》 SCIE CAS 2016年第41期9154-9161,共8页
AIM To evaluate the effect of long haul airplane transport of donor livers on post-transplant outcomes. METHODS A retrospective cohort study of patients who received a liver transplantation was performed in Perth, Aus... AIM To evaluate the effect of long haul airplane transport of donor livers on post-transplant outcomes. METHODS A retrospective cohort study of patients who received a liver transplantation was performed in Perth, Australia from 1992 to 2012. Donor and recipient characteristics information were extracted from Western Australian liver transplantation service database. Patients were followed up for a mean of six years. Patient and graft survival were evaluated and compared between patients who received a local donor liver and those who received an airplane transported donor liver. Predictors of survival were determined by univariate and multivariate analysis using cox regression.RESULTS One hundred and ninety-three patients received alocal donor liver and 93 patients received an airplane transported donor liver. Airplane transported livers had a significantly lower alanine transaminase(mean: 45 U/L vs 84 U/L, P = 0.035), higher donor risk index(mean: 1.88 vs 1.42, P < 0.001) and longer cold ischemic time(CIT)(mean: 10.1 h vs 6.4 h, P < 0.001). There was a weak correlation between CIT and transport distance(r2 = 0.29, P < 0.001). Mean follow up was six years and 93 patients had graft failure. Multivariate analysis found only airplane transport retained significance for graft loss(HR = 1.92, 95%CI: 1.16-3.17). One year graft survival was 0.88 for those with a local liver and was 0.71 for those with an airplane transported liver. One year graft loss was due to primary graft non-function or associated with preservation injury in 20.8% of recipients of an airplane transported liver compared with 4.6% in those with a local liver(P = 0.027). CONCLUSION Airplane transport of donor livers was independently associated with reduced graft survival following liver transplantation. 展开更多
关键词 飞机交通 ischemic 时间 接枝幸存 施主地点 机关损坏
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An Inteduction to the NO.605 Airplane Institute
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作者 XU XIAOYAN 《China Today》 1996年第12期60-61,共2页
AnInteductiontotheNO.605AirplaneInstitute¥XUXIAOYAN(OneoftheleadersinChina'saerospaceindustry.)Bystaffreport... AnInteductiontotheNO.605AirplaneInstitute¥XUXIAOYAN(OneoftheleadersinChina'saerospaceindustry.)BystaffreporterXUXIAOYANTHEMIN... 展开更多
关键词 NO An Inteduction to the NO.605 airplane Institute
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A Novel Airplane Detection Algorithm Based on Deep CNN
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作者 Ying Wang Aili Wang Changyu Hu 《国际计算机前沿大会会议论文集》 2018年第1期60-60,共1页
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基于变刚度复杂曲面模糊路径策略的飞机座舱自动化磨抛
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作者 刘其广 孙晓楠 +2 位作者 魏锦辉 李论 赵吉宾 《工具技术》 北大核心 2024年第7期97-102,共6页
飞机座舱罩作为典型的复杂曲面弱刚性薄壁零件,是军用与民用飞机的重要部件,其安全与否直接关系到飞机和飞行员的安全。针对飞机座舱盖研磨抛光过程的曲面形状复杂以及刚性弱等问题,本文基于机器人自动化磨抛系统提出了一种基于自适应... 飞机座舱罩作为典型的复杂曲面弱刚性薄壁零件,是军用与民用飞机的重要部件,其安全与否直接关系到飞机和飞行员的安全。针对飞机座舱盖研磨抛光过程的曲面形状复杂以及刚性弱等问题,本文基于机器人自动化磨抛系统提出了一种基于自适应阻抗控制策略的复杂曲面模糊路径的生成方法,并对磨抛过程的接触力进行建模与分析,引进主被动相结合的磨抛方法,对某型飞机座舱盖进行了仿真及磨抛试验分析。试验结果表明,所提出的主被动相结合的磨抛方法结合自适应阻抗控制策略能较好的适应复杂曲面模糊路径的磨抛过程,力控制精度可达±1N;提出的复杂曲面模糊路径能够满足某型飞机座舱罩的自动化磨抛工艺需求,在保证磨抛结果一致性的同时提高了磨抛效率。 展开更多
关键词 飞机座舱盖 研磨抛光 主被动柔顺控制 力控制
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民用飞机发动机舱灭火剂浓度测试研究
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作者 杜含杰 顾俊鸣 寇鸿飞 《民用飞机设计与研究》 2024年第2期120-125,共6页
国际民航史上曾因发动机舱着火而多次发生空难事故,为确保飞行安全,找出对发动机舱灭火剂浓度影响的各种因素、采用精准的改装手段以及建立有效的飞行测试方法就显得尤为重要。分析了通风流量、飞行速度、环境温度等因素对发动机舱灭火... 国际民航史上曾因发动机舱着火而多次发生空难事故,为确保飞行安全,找出对发动机舱灭火剂浓度影响的各种因素、采用精准的改装手段以及建立有效的飞行测试方法就显得尤为重要。分析了通风流量、飞行速度、环境温度等因素对发动机舱灭火剂浓度的影响,给出了测试设备、采样管敷设、采样点布置等改装方法,提出了发动机舱灭火剂浓度测试的飞行试验方法,对试验结果裕度进行了分析,为其它民用飞机发动机舱灭火剂浓度测试合格审定试飞提供了参考。 展开更多
关键词 民用飞机 发动机 灭火剂浓度 测试
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“双碳”目标下竹制航模技术探索
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作者 王烨 田薇 +2 位作者 石衡一 鲁少聪 乔婧 《科学技术创新》 2024年第7期221-224,共4页
“双碳”目标是我国基于推动构建人类命运共同体的责任担当和实现可持续发展的内在要求而作出的重大战略决策,为了实现“双碳”目标,需要国家、社会、个人各个层面从小到大做出具体性措施,作为高校学子,西北工业大学民航学院“航育”团... “双碳”目标是我国基于推动构建人类命运共同体的责任担当和实现可持续发展的内在要求而作出的重大战略决策,为了实现“双碳”目标,需要国家、社会、个人各个层面从小到大做出具体性措施,作为高校学子,西北工业大学民航学院“航育”团队在田薇老师的带领下,结合学校三航特色及学生专业性技能,自主研发制作了一种新型环保型航模,团队取材于西北工业大学定点帮扶地区——广西壮族自治区“毛竹之乡”融水,利用当地丰富的毛竹资源,探讨了竹材料在各向的力学性能,并针对传统型航模的短板,制作出一种更环保更实惠的航模,与当地特色苗族文化进行交融,在乡村振兴战略下为“双碳”目标作出自己的贡献。 展开更多
关键词 “双碳”目标 航模 竹材料 乡村振兴
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某发动机凸轮轴与驱动齿轮的装配方法
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作者 李世东 《内燃机与配件》 2024年第1期32-34,共3页
在航空行业中,飞机发动机上的每个零部件都有重量要求,所以在零部件开发阶段在满足产品性能及其功能前提尽量减轻零部件重量,因此凸轮轴及其驱动齿轮中间处于镂空状态,为了提高产品质量稳定性,设计时在凸轮轴轴径增加定位销,但也因此增... 在航空行业中,飞机发动机上的每个零部件都有重量要求,所以在零部件开发阶段在满足产品性能及其功能前提尽量减轻零部件重量,因此凸轮轴及其驱动齿轮中间处于镂空状态,为了提高产品质量稳定性,设计时在凸轮轴轴径增加定位销,但也因此增加了装配难度。现有技术中,由于驱动齿轮在加热时齿轮表面受热不均匀,以及散热速度快等因素,导致压装力过大而造成凸轮轴轴径切削、定位销变形等异常现象,因此传统的齿轮加热压装方式无法满足产品要求。 展开更多
关键词 飞机发动机 凸轮轴 驱动齿轮
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改进NSGA-Ⅱ对飞机维修性分配的方法
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作者 周瑜哲 彭勃 《内燃机与配件》 2024年第10期110-112,共3页
维护性是指为了便于维护,提高设备系统的效率,降低全寿命周期的使用成本,按照规定的时间、条件、方法和程序对设备进行维护,维修性过程中最不可少的一项工作就是维修性分配。本文将维修性分配问题描述为多目标优化问题,通过建立产品全... 维护性是指为了便于维护,提高设备系统的效率,降低全寿命周期的使用成本,按照规定的时间、条件、方法和程序对设备进行维护,维修性过程中最不可少的一项工作就是维修性分配。本文将维修性分配问题描述为多目标优化问题,通过建立产品全寿命周期维护性相关费用与平均修复时间(MTTR)的多目标综合权衡模型,采用改进的非支配性排序遗传算法,对模型进行求解,获得合理的维修性分配方案,从而为飞机座椅维修提供维修依据。 展开更多
关键词 平均修复时间 维修性分配 改进的NSGA-Ⅱ 飞机座椅
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面向民机复杂航电系统的综合验证平台研究
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作者 张军才 胡林平 《电光与控制》 CSCD 北大核心 2023年第2期71-74,共4页
民机复杂航电系统的高效研制需要各种综合验证平台的有力支持。首先,通过梳理复杂航电系统的工程活动,确认所需综合验证平台的类别;其次,对综合验证平台进行功能分析,提出了通用功能定义;再次,采用维度分析方法分析了综合验证平台的现状... 民机复杂航电系统的高效研制需要各种综合验证平台的有力支持。首先,通过梳理复杂航电系统的工程活动,确认所需综合验证平台的类别;其次,对综合验证平台进行功能分析,提出了通用功能定义;再次,采用维度分析方法分析了综合验证平台的现状,并提出了优化思路;最后,针对用途广泛的设备级综合验证平台进行了顶层规划和统一设计,开发了通用的设计模型,并提出了设计模型的实施规范要求。 展开更多
关键词 民用飞机 航电系统 系统验证 验证平台
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高能激光系统试验机建设关键技术研究
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作者 杜梓冰 《激光与红外》 CAS CSCD 北大核心 2023年第7期979-986,共8页
研究高能激光系统试验机建设中的关键技术,以期推动机载高能激光的发展。研究了试验飞机在航空科技领域的作用和地位,并以美国典型的X试验机、F22和F35航电它机进行说明;阐述了试验机在机载高能激光发展中的重要性和必要性,并分别研究... 研究高能激光系统试验机建设中的关键技术,以期推动机载高能激光的发展。研究了试验飞机在航空科技领域的作用和地位,并以美国典型的X试验机、F22和F35航电它机进行说明;阐述了试验机在机载高能激光发展中的重要性和必要性,并分别研究了美国、前苏联和以色列机载高能激光武器试验机建设特点,包括已试飞的和规划中的;总体分析了试验机建设过程中关键技术识别、技术成熟度分析、试验机设计、试验机改装和测试记录等关键技术点。 展开更多
关键词 机载高能激光武器 试验机设计 飞行试验
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西宁机场飞机地面空调改进方式研究
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作者 周敏 许安琪 杨春方 《暖通空调》 2023年第4期54-57,共4页
飞机地面空调机组(PCA)在国内有近10年的历史,但PCA通常处理的新风温差高达30~40℃,机组能效比通常低于2。高能效、轻便、稳定是未来PCA的发展趋势。本文结合西宁地区气候特点、航站楼冷热源设计特点,在常规机组的基础上进行改进,提出... 飞机地面空调机组(PCA)在国内有近10年的历史,但PCA通常处理的新风温差高达30~40℃,机组能效比通常低于2。高能效、轻便、稳定是未来PCA的发展趋势。本文结合西宁地区气候特点、航站楼冷热源设计特点,在常规机组的基础上进行改进,提出夏季采取一级预冷(预冷水温16℃)、二级深度压缩制冷(冷凝采用水冷)+三级风冷保证过渡季供冷的技术方案。并根据冬季供热形式进一步分为方案1(电加热)、方案2(集中热源预热)、方案3(预热预冷共用表面冷却器)。结果显示:方案1投资及运行费均低于常规机组;方案2、方案3投资高于常规机组,但从长期运行来看,均远优于常规机组;3种方案的运行碳排放相比常规机组,分别减少了1.9、2.8、3.3 kt/a。 展开更多
关键词 飞机地面空调机组 预冷(热)盘管 集中冷(热)源 经济效益 碳排放
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飞机飞越噪声自由场声压级测试方法研究
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作者 朱江辉 《噪声与振动控制》 CSCD 北大核心 2023年第4期280-287,共8页
在飞机飞越噪声地面试验中,噪声测量受地面对声波散射的较大影响。为修正地面对飞越噪声测量的影响,开展飞行试验对飞越噪声自由场声压级测试技术的研究。首先,进行地面对飞机飞越噪声传播的影响分析,推导获取自由场声压级的修正方法,... 在飞机飞越噪声地面试验中,噪声测量受地面对声波散射的较大影响。为修正地面对飞越噪声测量的影响,开展飞行试验对飞越噪声自由场声压级测试技术的研究。首先,进行地面对飞机飞越噪声传播的影响分析,推导获取自由场声压级的修正方法,仿真分析影响因素。随后,设计三类可消除地面影响获得自由场声压级的飞越噪声测试方案,应用于某大型运输类民机的飞越噪声测试飞行试验,分析测试方案的适用性。试验结果表明,地面对飞越噪声测量有不可忽略的影响,提出的噪声测量方案均能在一定的宽频带内取得自由场声压级,其中采用带有声学硬反射面的传声器布置方式,在中低频段的宽频带的自由场声压级修正量约为+6 dB,采用加高布置传声器的方式在中高频段的自由场声压级修正量约为+2.8 dB,据此可简便、可靠地得到飞越噪声的自由场声压级,而针对不同的试验条件,需采用与之相适应的测量方法。 展开更多
关键词 声学 飞机噪声 噪声测试 地面影响 自由场声压级
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