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Preliminary design of a tip-jet-driven heavy lift helicopter incorporating circulation control

机译:带有循环控制的尖端喷气式重型直升机的初步设计

摘要

This report describes a preliminary design study for a Very Heavy Lift Helicopter (VHLH) that is powered by jets at the blade tips and is controlled by circulation control applied to the main rotor blades. The main thrust of the program was to integrate a tip-jet-powered helicopter design computer program developed by Hughes Helicopters, Inc. (HHI) with circulation control data generated by the David Taylor Naval Ship Research and Development Center (DTNSRDC). This work combined the computer program integration work with an air vehicle preliminary design study to size the helicopter and describe its features. The result of this study is the sizing of a four-engined helicopter with a 185 foot diameter, two-bladed main rotor that is designed to carry the XM-1 Main Battle Tank 100 nautical miles in a ship-to-shore Marine Corps assault mission.
机译:本报告介绍了一种非常重型升力直升机(VHLH)的初步设计研究,该直升机由叶尖的射流提供动力,并通过应用于主旋翼叶片的循环控制进行控制。该计划的主要目的是将由休斯直升机公司(HHIes)开发的尖端喷气动力直升机设计计算机程序与戴维·泰勒海军舰船研究与发展中心(DTNSRDC)生成的循环控制数据相集成。这项工作将计算机程序集成工作与飞机的初步设计研究相结合,以确定直升机的尺寸并描述其功能。这项研究的结果是确定一架直径为185英尺,两叶主旋翼的四引擎直升机的大小,该直升机的设计目的是将XM-1主战坦克在船对岸海军陆战队的攻击中承载100海里。任务。

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  • 年度 1981
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