
Agusta-Bell AB.212 | |
|---|---|
| 国家 | 美国 意大利 |
| 作用 | 多用途直升机 |
| 首次飞行 | 1971 |
| 建立 | 未知 |
这 阿古斯塔-贝尔 AB.212 是阿古斯塔在意大利制造的多用途直升机,获得了制造美国贝尔212直升机的许可证。
源: 维基百科上的阿古斯塔-贝尔AB.212
| Agusta-Bell AB.212 | |
|---|---|
| Photographers | Unknow |
| Localisation | Unknow |
| Photos | 110 |
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General Characteristics
The Agusta-Bell AB.212 is the Italian license-built version of the U.S. Bell 212, which is a twin-engine development of the famous single-engine Bell 205 (UH-1 Huey). The dual-engine design provides significantly improved safety and performance, particularly in challenging environments (like “hot and high” conditions) and over water, making it popular for naval and paramilitary roles.
| Property | Typical Value (AB.212) |
|---|---|
| 作用 | Medium Utility / Transport / Anti-Submarine Warfare (ASW) |
| 制造商 | Agusta (now part of Leonardo S.p.A.) |
| First Flight (Bell 212) | April 1968 |
| 船员 | 1 or 2 pilots (2 for IFR operation) |
| Capacity (Passengers) | Up to 14 passengers or 6 stretchers/litters |
| Main Rotor Diameter | 14.63 m (48 ft 0 in) |
| Max Takeoff Weight | 5,080 kg (11,200 lb) |
Design and Powerplant
- Engine: One Pratt & Whitney Canada PT6T-3 Twin-Pac coupled turboshaft engine.
- Power System: The Twin-Pac consists of two power turbines that drive a common gearbox, providing redundancy.
- Thrust Output (Combined): Approximately 1,342 kW (1,800 shp) total, with the ability to maintain 671 kW (900 shp) for 30 minutes in case of a single-engine failure.
- Rotor System: Two-bladed semi-rigid main rotor and a two-bladed tail rotor.
- Cabin: Features a spacious cabin with sliding side doors and a flat floor, easily convertible for troop transport, medevac, or cargo.
- Naval Variant (AB.212ASW): Developed by Agusta, this variant features a large radar dome above the cockpit, corrosion protection, and equipment for anti-submarine warfare (ASW), including dipping sonar and the ability to carry torpedoes.
Performance and Capabilities
- Maximum Speed: Up to 240 km/h (130 knots, 149 mph).
- Cruise Speed: Approximately 185–205 km/h (100–110 knots).
- Service Ceiling: 5,300 m (17,400 ft).
- Max Range: Approximately 420 km (230 nautical miles).
- Internal Cargo Capacity: 6.23 m³ (220 ft³).
- External Load Capacity: The external cargo hook can lift up to 2,268 kg (5,000 lb).
- Operational Use: Widely used by civil operators for offshore transport and logging, and by military forces for utility, SAR (Search and Rescue), and naval operations (especially the ASW variant).
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