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MAKING UH-1N PERFORMANCE CHARTS PREDICT BETTER

机译:更好地预测UH-1N性能图

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This paper highlights the importance of updating aircraft performance charts periodically, especially after modifications are made that could affect power required or power available. With an initial tasking of simply validating some draft performance charts, the test team quickly learned that not only were the draft charts unsafely inaccurate, the published Flight Manual seemed to have significant errors. The Flight Manual under predicted torque required to hover frequently, especially at conditions involving high gross weight and/ or high density altitudes. The test program thus evolved into a four phase project. Phase 1 covered the work done to spot check the draft charts. Phase 2 was intended to check the Flight Manual accuracy with additional test aircraft from operational units, and Phase 3 compared the Flight Manual to the U.S. Navy's UH-1N Flight Manual (with good results). Phase 4 testing found the test team developing completely new hover torque required charts and proving their accuracy under high, hot, and heavy flight conditions.
机译:本文强调了定期更新飞机性能图表的重要性,尤其是在进行了可能影响所需功率或可用功率的修改后。由于最初的任务只是简单地验证一些性能图表草稿,测试团队很快就知道,不仅图表草稿不安全地不准确,而且已出版的《飞行手册》似乎也存在重大错误。 《飞行手册》在经常需要悬停的预期扭矩下,尤其是在涉及高总重和/或高密度高度的情况下。测试程序因此演变为四个阶段的项目。第一阶段涵盖了抽查图表草稿的工作。第2阶段旨在使用操作单元中的其他测试飞机来检查《飞行手册》的准确性,第3阶段将《飞行手册》与美国海军的UH-1N《飞行手册》进行了比较(结果良好)。阶段4的测试发现测试团队开发了全新的悬停扭矩要求图表,并证明了它们在高,热和重飞行条件下的准确性。

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