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Flight test of V-22 Hover Mission Task Elements in Natural Winds

机译:V-22悬停任务任务元素在自然风中的飞行测试

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The V-22 Osprey tiltrotor low-speed flight envelope was developed primarily on the basis of paced criticalrnazimuth testing, coupled with paced pedal kicks to measure transient control margins. In order torndemonstrate that the low-speed hover flight envelope was acceptable in real-world conditions, a flight testrnprogram was conducted to measure handling qualities ratings (HQR) for 7 mission task elements (MTE) at 4rnwind azimuths in 3 wind bands. Hover MTE tests such as those presented in ADS-33, and in previous flightrntests of the V-22 and other vehicles, were developed and flown in low- or no-wind conditions. On the otherrnhand, shipboard tests in winds typically focus on a limited number of operations in the presence of large,rnthree dimensional air currents caused by the ship that are not translatable to land-based operations. Thisrnpaper explores the approach taken to extend MTE testing to include natural winds up to the highest speedsrnpermitted for operations of the V-22. In addition to the test results, the creation of the MTE tolerances andrnthe design and implementation of the test course are discussed. Because the aircraft mission does not changernas the wind speed increases, the task tolerances were the same as those for no-wind conditions. HQRs werernexpected to drop as wind speed increased and the pilots had more difficulty in performing precision tasks.rnFor both the MTE tolerance and the test course layout, compromises were made to increase the efficiency ofrnthe test, specifically to minimize flight time and to take advantage of wind and weather conditions. The keyrnlesson learned is that defining the V-22 low-speed envelope through paced testing and control marginrninvestigations is adequate, except for vertical landing and takeoff in winds. In addition, a practical andrnefficient test course was designed and used in the tests. However, finding natural winds up to or beyond thernflight envelope limits is difficult and time-consuming. Overall, MTE testing in natural winds was found to bernpractical and added to our knowledge of the V-22, but the test was complex and may not be necessary for allrnaircraft.
机译:V-22 Osprey倾转旋翼低速飞行包络线主要是在有节奏的临界方位角测试的基础上开发的,并结合有节奏的踏板脚蹬来测量瞬态控制裕度。为了证明低速悬停飞行包线在现实条件下是可以接受的,进行了飞行测试程序,以测量3个风带中4个风向上7个任务任务要素(MTE)的处理质量等级(HQR)。悬停的MTE测试(例如ADS-33中提出的测试以及在V-22和其他车辆的先前飞行测试中)是在低风或无风条件下开发和飞行的。另一方面,船上的风中测试通常集中在有限数量的操作上,该操作存在着由船舶引起的无法转换为陆上操作的大,三维气流。本文探讨了扩展MTE测试以将自然风包括到V-22操作所允许的最高速度的方法。除了测试结果,还讨论了MTE公差的创建以及测试过程的设计和实施。由于飞机的任务不会改变风速,因此任务容差与无风条件下的容差相同。 HQRs预计会随着风速的增加而下降,并且飞行员执行精确任务的难度更大。rn对于MTE公差和测试路线的布局,都做出了折衷以提高测试效率,特别是最大程度地减少了飞行时间并利用了风和天气条件。获悉的关键教训是,通过有节奏的测试和控制裕度调查来定义V-22低速包络是足够的,除了垂直着陆和风中起飞外。此外,还设计了实用且效率低下的测试课程,并在测试中使用了该课程。然而,找到达到或超过飞行包络线极限的自然风是困难且耗时的。总体而言,发现自然风中的MTE测试是实用的,并增加了我们对V-22的了解,但是该测试很复杂,对于飞机来说可能不是必需的。

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