第二代大型民用倾转旋翼机的变转速动力／传动技术发展被引量：1

Observation on the LCTR2＇s Variable Speed Power/Transmission System Technologies

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摘要突破旋翼机飞行速度限制是旋翼机发展最主要的目标之一，而航程和载荷也是两个限制旋翼机更广泛应用的重要因素。为了提高直升机的速度、航程和载荷等性能水平，研究人员将改变旋翼转速视为提升旋翼机性能的突破口，并对此展开多项研究。

作者李昊

机构地区中国航空工业发展研究中心

出处《国际航空》 2013年第8期40-42,共3页 International Aviation

关键词倾转旋翼机传动技术第二代速动民用速度限制研究人员直升机

同被引文献9

1ACREE C W, YEO H, SINSAY J D. Performance optimization of the NASA large civil tiltrotor[R]. NASA/TM-2008-215359, 2008.
2MARK R, JOSEPH W, ROBERT M, et al. The effect of rotor cruise tip speed, enginetechnology and engine/drive system RPM on the NASA large civil tiltrotor (LCTR2) size and performance[R]. N ASA/TM-2013-0014739, 2013.
3WAYNE J, GLORIA K Y, MICHAEL E. NASA heavy lift rotorcraft systems investigation[C]. Proceedings of the 2nd International Basic Research Conference on Rotorcraft Technology, Nanjing, 2005.
4STEVENS M A, LEWICKI D G, HANDSCHUH R F. Concepts for multi-speed rotorcraft drive system-status of design and testing at NASA GRC[C]. The AHS 71st Annual Forum, Virginia, 2015.
5LAPPOS N D, KAREDES E, VINAYAK H, et al. Variable speed gearbox with an independently variable speed tail rotor system for a rotary wing aircraft: US, US7651050[P]. 2010.
6GARCIA T, GMIRYA Y, PALCIC P X. Variable speed transmission for a rotary wing aircrafl: US, US7296767 B2[P]. 2007.
7EHINGER R T, FENNY C A, KILMAIN C J, et al. Multi-ratio rotorcraft drive system and a method of changing gear ratios thereof: US, US 8449432 B2[P]. 2013.
8CHRISTOPHER A S, CECIL W A. Preliminary assessment of variable speed power turbine technology on civil tiltrotor size and performance[R]. N ASA/TM-2012-0014256, 2012.
9CHRISTOPHER A S, MARK R, JOSEPH W, et al. Summary of the large civil tihrotor (LCTR2) engine gearbox study[R]. NASA/ TM-20100042405, 2010.

国际航空

2013年第8期

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