...
首页> 外文期刊>Aerospace science and technology >Wake vortex encounter severity for rotorcraft in final approach
【24h】

Wake vortex encounter severity for rotorcraft in final approach

机译:尾涡在最后进近时遇到旋翼航空器的严重性

获取原文
获取原文并翻译 | 示例
           

摘要

The Advisory Council for Aeronautics Research in Europe (ACARE) predicts that European air traffic may nearly triple by 2020. The growth in air traffic is already an increasing problem with capacity at some airports becoming limited due to congestion. This could be alleviated by providing additional passenger capacity at hubs through the introduction of rotorcraft using new IFR procedures and operating simultaneously but independently of the fixed-wing traffic. These Simultaneous Non-Interfering Operations (SNIOps) will be enabled by a 'reconfiguration' of the airspace, taking advantage of new navigational and air traffic management systems. SNIOp's raise critical safety questions for rotorcraft wake vortex encounters (WVE's) and will require consideration of the longitudinal and lateral aircraft separation and the locations of the rotorcraft FATO's (Final Approach and Take-Off areas). This paper presents analysis from work carried out as part of the Framework 6 project 'OPTIMAL' including the development of predictive methodology and analysis for rotorcraft WVE's, using a severity rating scale. In particular, scenarios are considered where the rotorcraft is following precision glideslopes of up to 12° in both good and degraded visual conditions. Handling qualities criteria have already been found to be well suited to investigating severity of an encounter. Within this framework, draft boundaries are proposed for assessing the severity of an encounter. Furthermore, the results have shown a pilot may be able to recover from an encounter, but the question of whether the required navigational precision would be compromised and a go-around required is also addressed.
机译:欧洲航空研究咨询委员会(ACARE)预测,到2020年,欧洲的空中交通量可能增长近两倍。空中交通的增长已经成为一个日益严重的问题,由于拥挤,一些机场的运力变得有限。通过采用新的IFR程序引入旋翼航空器并同时但独立于固定翼飞机流量运行,可以在枢纽上增加客运量,从而减轻这一负担。利用新的导航和空中交通管理系统,可以通过对空域进行“重新配置”来实现这些同时无干扰运行(SNIOps)。 SNIOp针对旋翼飞机的尾涡涡流(WVE)提出了关键的安全问题,将需要考虑飞机的纵向和横向间隔以及旋翼飞机FATO的位置(最终进场和起飞区域)。本文介绍了根据框架6项目“ OPTIMAL”进行的工作分析,包括使用严重性等级量表开发了预测方法和旋翼机WVE的分析。特别地,考虑了在良好和退化的视觉条件下旋翼飞机遵循高达12°的精确滑坡的场景。已经发现处理质量标准非常适合调查相遇的严重性。在此框架内,提出了边界草图以评估相遇的严重性。此外,结果表明飞行员可能能够从相遇中恢复过来,但是还解决了所需的导航精度是否会受到损害以及是否需要复飞的问题。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号