
AgustaWestland AW101 | |
|---|---|
| 国家 | 英国 / 意大利 |
| 作用 | 反潜战、中型运输、搜救和通用直升机 |
| 首次飞行 | 9 十月 1987 |
| 建立 | 未知 |
这 阿古斯塔韦斯特兰AW101 是军用和民用的中型直升机。它于1987年首次飞行,由英国的威士兰直升机公司和意大利的阿古斯塔公司合资开发,以满足国家对现代海军通用直升机的要求。包括英国,丹麦和葡萄牙武装部队在内的一些运营商使用Merlin这个名字来命名他们的AW101飞机。它在英国约维尔和意大利韦尔贾特的工厂生产;在日本和美国也进行了许可的装配工作。
| AgustaWestland AW101 Merlin Walk Around | |
|---|---|
| 摄影师 | 未知 |
| 本地化 | 未知 |
| 照片 | 16 |
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General Characteristics
The AW101 is a medium-lift, multi-role helicopter originally developed by a joint venture between Westland Helicopters (UK) and Agusta (Italy). It is primarily used for naval (ASW/ASuW) and troop transport roles and is known for its size and three-engine reliability.
| Property | Value (Typical Military Variant) |
|---|---|
| 作用 | Naval, Transport, SAR, VIP/Utility |
| 制造商 | AgustaWestland (now Leonardo Helicopters) |
| Maiden Flight | October 9, 1987 |
| 船员 | 3–4 (Pilots, Mission/System Operators) |
| Troop Capacity | Up to 30 seated troops (or 16 stretchers) |
| Maximum Take-Off Weight | 15,600 kg (34,392 lb) |
Powerplant and Design
- Powerplant: Three (3) General Electric CT7-8E or Rolls-Royce Turbomeca RTM322 turboshaft engines.
- Power Output: Approx. 1,566 kW (2,100 shp) per engine.
- Rotor System: Five-blade main rotor and four-blade tail rotor.
- Key Design Feature: The three-engine configuration provides excellent safety margins, redundancy, and performance, particularly in difficult environments (e.g., ship deck operations, hot and high).
- Naval Feature: Main rotor blades can be folded automatically for shipboard storage.
Performance and Service
- Maximum Speed: 309 km/h (192 mph / 167 knots).
- Range: 1,363 km (847 miles) (Internal fuel).
- Service Ceiling: 4,575 m (15,010 ft).
- Key Users/Designations: Royal Navy/RAF (Merlin), Royal Canadian Air Force (CH-149 Cormorant), Italian Navy (EH-101), Japanese Maritime Self-Defense Force.
- Armament (ASW Role): Can carry torpedoes (e.g., Sting Ray), depth charges, and dipping sonar.
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