高速直升机运输效能评估

doi:10.7527/S1000-6893.2024.30182

Abstract

Abstract:

The transport effectiveness evaluation of high-speed helicopters is studied by providing transport task profiles with practical needs. The X3 compound helicopter and V-22 tiltrotor aircraft are selected as the research objects. After selecting some typical mission profiles， flight performance parameters are calculated， mainly including the required power， range and fuel consumption rate. A high-speed helicopter transport effectiveness evaluation model is established， and the calculation results of the performance parameters of the flight profile are substituted into the model for effectiveness evaluation， and the factors affecting the effectiveness are analyzed. The sensitivity of the parameters is analyzed. Finally， the transport effectiveness between different aircraft configurations is compared and analyzed， and suitable aircraft configurations for different transport tasks are proposed. Suggestions for improving transport effectiveness are also given.

Key words: compound-helicopter, tiltrotor aircraft, aircraft overall performance, transport effectiveness evaluation, high-speed helicopter

CLC Number:

V212.13

Changhao LIU, Yihua CAO, Xiaomeng MEI, Maosheng WANG, Guanglin ZHANG. Transport effectiveness evaluation of high⁃speed helicopters[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 530182-530182.

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References 23

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倾转旋翼机	年代	复合直升机
	20世纪30年代	Fl185
XV-3验证机 XV-15	20世纪50年代
XV-3验证机 XV-15	20世纪60年代	XH-51A 16H-1“探路者” AH-56“夏延”
	20世纪70年代	XH-59A
V-22	20世纪80年代
AW609 V-280，NGCTR	21世纪	X2， S-97， CCH，卡-92 X3， RACER

性能参数	数据
最大速度/（km·h^-1）	472
旋翼直径/m	12.6
机身	AS365N3机身
旋翼桨叶	5片EC155桨叶
发动机	2台Rolls-Royce Turbomeca RTM322

性能参数	数据
空机重量/kg	15 030
旋翼直径/m	11.6
实用升限/m	7 925
机组/乘员人数	4/24
正常航程/km	2 224
正常载油量/kg	6 215
转场航程/km	3 892
转场载油量/kg	11 970
发动机	2台Rolls-Royce AE1107C

飞行阶段	高度/m	时间/min	距离/km
预留	25 min续航时间或10%油箱容量
地面滑行	200	5	0
垂直起飞	200	3	0
悬停	205	1	0
爬升	1 000		5
巡航	1 000		515
下降	15		520
悬停	15	2	520
降落	10	4	520
地面待命	10	5	520
垂直起飞	10	3	520
悬停	15	1	520
爬升	1 000		525
巡航	1 000		1 035
下降	205		1 040
悬停	205	2	1 040
降落	200	4	1 040

飞行阶段	高度/m	时间/min	距离/km
预留	25 min续航时间或10%油箱容量
地面滑行	800	5	0
垂直起飞	800	2	0
悬停	805	1	0
爬升	4 300		40
巡航	4 300		150
下降	1 065		190
悬停	1 065	2	190
降落	1 060	4	190
地面待命	1 060	5	190
垂直起飞	1 060	2	190
悬停	1 065	1	190
爬升	4 300		230
巡航	4 300		340
下降	805		380
悬停	805	2	380
降落	800	4	380

Transport effectiveness evaluation of high⁃speed helicopters

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