The compound helicopter — why have we not succeeded before?

Author:

Orchard M. N.,Newman S. J.

Abstract

Abstract Compounding offers a way of advancing the performance of the standard helicopter significantly for a moderate increase in complexity through the addition of wings and/or auxiliary propulsion. The compound helicopter configuration has the potential advantages of increased speed, range, agility, productivity and reduced vibration levels over conventional helicopters. Despite several significant efforts, however, no compound helicopter has ever been put into production. This paper looks at three aircraft that came close to being accepted by operators and examines the reasons why they were not ultimately put into production. The cancellation of these projects appeared to be of a political nature rather than technical. Also addressed are the issues that still face prospective designers of compound helicopters and the lessons that can be extracted and applied to modern day efforts to build and sell an aircraft of this configuration.

Publisher

Cambridge University Press (CUP)

Subject

Aerospace Engineering

Reference6 articles.

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Wind-tunnel experimental investigation on rotor-rotor aerodynamic interaction in compound helicopter configuration;Aerospace Science and Technology;2024-10

2. Maneuverability Assessment of a Compound Helicopter Configuration;Journal of the American Helicopter Society;2016-01-01

3. Performance comparison between a conventional helicopter and compound helicopter configurations;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2015-04-06

4. Flight Dynamics Investigation of Compound Helicopter Configurations;Journal of Aircraft;2015-01

5. The Gyrodyne—A Forgotten High Performer?;Journal of the American Helicopter Society;2007

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