首页> 外文会议>Annual Vertical Flight Society Forum and Technology Display >Active and Passive Camber Morphing for Helicopter Rotors towards Performance Improvements in Hover and Vertical Flight
【24h】

Active and Passive Camber Morphing for Helicopter Rotors towards Performance Improvements in Hover and Vertical Flight

机译:用于直升机转子的主动和被动弯曲传真对悬停和垂直飞行的性能改进

获取原文

摘要

Rotor morphing has been investigated in the past for improvement of rotor performance, either for reduction of rotor power demand or for vibratory load alleviation. The present study investigates the application of camber morphing for improvement of rotor performance in hover and vertical flight conditions, with a particular focus on the combination of camber morphing systems and variable RPM rotors. Camber morphing utilizes a smooth flap at the trailing edge of the rotor blade to modify the camber of blade airfoil sections without excessive drag penalties. Two different camber morphing systems will be investigated in this study, namely the active and passive systems. Passive camber morphing, which combines camber morphing with the variable speed rotor concept is the unique aspect of camber morphing which will be the primary focus of this study. The active system can be actuated at frequencies higher than 1/rev of the rotor and requires external power input for functioning. The passive system can be controlled only by varying the RPM of the rotor and requires no additional energy input. Therefore, the passive system is expected to show larger net performance benefits. Variable RPM rotors in themselves show potential towards the reduction of rotor power demand but are largely ineffective for low-speed applications. The combination of camber morphing and the variable speed rotor shows larger performance benefits than those obtained from the two technologies independent of each other. The two technologies, when combined in passive camber morphing, can remedy each other's deficiencies and improve the overall rotor performance. The use of camber morphing shows more benefit for operating points at or near the edge of the flight envelope since the rotor blade sections encounter high average angles of attack for these operating points. Vertical climb and hover at high altitude are examples of flight conditions investigated. Overall, passive camber morphing shows a larger performance benefit as compared to the active system.
机译:转子变形在过去改进的转子性能进行了研究,无论是减少转子的功率需求或振动载荷减缓。本研究调查外倾角的变形处于悬停和垂直飞行条件的改善的转子性能的应用,尤其侧重于曲面变形系统和可变RPM转子的组合。外倾角变形利用在转子叶片的后缘的平滑襟翼修改叶片翼型部的弯度而没有过度的阻力处罚。两种不同的外倾角变形系统将在本研究中,即有源和无源系统进行调查。被动弯度变形,它结合了外倾角与可变速度转子概念词态化是曲面变形,这将是本研究的主要焦点的独特的方面。有源系统可在更高的频率被致动比转子的1 /转,并且需要外部电源输入为正常。被动系统只能通过改变转子的转速被控制,并且不需要额外的能量输入。因此,被动系统预计将出现较大的净性能优势。本身可变RPM转子显示出对转子的电力需求的还原电位,但是是用于低速应用很大程度上是无效的。拱变形的和组合中的可变速度显示转子比从两种技术互相独立的所获得的那些更大的性能益处。这两种技术,在被动拱变形组合时,可以弥补对方的不足,提高了整体性能的转子。使用弯变形节目在或接近以来的转子叶片部的飞行包线的边缘工作点多效益的遭遇攻击这些工作点的高平均角度。垂直爬升并悬停在高空的飞行条件的实例调查。总体而言,被动弯度变形示出了更大的性能益处相比,有源系统。

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