ロビンソンR44 | |
|---|---|
| 国 | 米国 |
| 役割 | 軽い有用性およびトレーナーのヘリコプター |
| 初飛行 | 1990年3月31日 |
| 構築 | 6400+ |
ザ ロビンソンR44 は、1992年からロビンソンヘリコプターカンパニーによって製造された4人乗りの軽ヘリコプターです。同社の2人乗りロビンソンR22をベースにしたR44は、油圧アシストの飛行制御を備えています。1990年3月31日に初飛行し、1992年12月にFAA認証を取得し、1993年2月に最初の納入を行いました。
ソース： ウィキペディアのロビンソンR44
| ロビンソンR44レイヴンII | |
|---|---|
| カメラマン | 知りません |
| ローカライズ | 知りません |
| 写真 | 100 |
Robinson R44 18
Robinson R44 20
Robinson R44 21
Robinson R44 22
Robinson R44 23
Robinson R44 24
Robinson R44 25
Robinson R44 26
Robinson R44 27
待って、あなたのためにロビンソンR44の写真を検索します...
コーヒーを買って
関連項目:
General Characteristics (Raven II Variant)
The Robinson R44 is a popular four-seat, single-engine piston helicopter, widely recognized for its reliability, efficiency, and relatively low operating costs. It is derived from the smaller, two-seat R22 and is extensively used globally for flight training, corporate transport, tourism, and law enforcement.
| Property | Typical Value (R44 Raven II) |
|---|---|
| 役割 | Light Utility / Trainer / Personal Transport |
| メーカー | Robinson Helicopter Company |
| First Flight | March 31, 1990 |
| 乗組員 | 1 pilot |
| Capacity (Passengers) | 3 passengers |
| Main Rotor Diameter | 10.1 m (33 ft 0 in) |
| Max Takeoff Weight | 1,134 kg (2,500 lb) |
Design and Powerplant
- Engine: One Lycoming IO-540-AE1A5 six-cylinder, fuel-injected piston engine (Raven II). The Raven I uses a carbureted O-540.
- Horsepower: Derated to 245 hp for takeoff and 205 hp continuous (Raven II).
- Rotor System: Semi-rigid two-bladed main rotor and a two-bladed tail rotor.
- Controls: Features hydraulically boosted controls to reduce pilot effort and enhance maneuverability.
- Safety Feature: Equipped with a crashworthy fuel system that includes bladder fuel tanks to mitigate the risk of post-accident fire.
- Variants: Includes the Raven I (carbureted engine), Raven II (fuel-injected engine), Clipper (with floats for water landings), and Cadet (two-seat trainer/utility).
Performance and Capabilities
- Maximum Airspeed (Vne): Up to 241 km/h (130 knots, 150 mph).
- Cruise Speed: Up to 202 km/h (109 knots, 126 mph).
- Service Ceiling: 4,267 m (14,000 ft).
- Maximum Range (No Reserve): Approximately 560 km (300 nautical miles).
- Rate of Climb: Over 1,000 ft/min (5.1 m/s).
- Useful Load: Approximately 451 kg (995 lb) (varies by variant and fuel load).
- Fuel Type: Operates on Aviation Gasoline (AVGAS 100LL).
ビュー : 625
