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AC311直升機基本性能
Presentation of AC311 Helicopter
AC311直升機是一款2噸級單發單旋翼、帶尾槳式多用途民用直升機，該機采用高橇式起落架，裝有一臺美國Honeywell公司LTS101-700D-2低油耗發動機，配置高度集成化綜合航空電子系統，可供多種選擇的精致內飾和座椅，整機大量使用復合材料。采用全數字化設計和制造技術，充分體現了“安全性”、“經濟性”、“舒適性”、“可靠性”設計理念。應用廣泛，可滿足高原、高寒氣候的使用條件。
AC311 is a 2-ton-class multi-purpose civil helicopter of single-main-rotor plus tail rotor configuration. With heavy use of composite materials, it is installed with high skid landing gear, a low-fuel-consumption engine LTS101-700D-2 from American Honeywell Company, highly Integrated Avionics System (IAS) and multiple optional delicate interiors and seats. Its adoption of all-digital design and manufacturing technologies fully demonstrates the design concept of “safety”, “affordability”, “comfort” and “reliable”. It can be used in wide applications and can satisfy the operation conditions of plateau and extremely cold climate.
適航規范
Airworthiness Certification Standards
符合CCAR27部的要求
Complies with CCAR 27
運行類型
Operation type
晝夜目視飛行
Day and Night VFR
應用領域
Application Area
AC311直升機可廣泛用于客貨運輸、飛行訓練、公務飛行，經加裝任務設備后可執行多種任務，如醫療救護、電力巡檢、空中執法、航拍攝影、飛播滅蟲、護林防火等多個領域。
AC311 helicopter can be widely used for transportation of personnel and cargo, flight training and business flight. After installation of mission equipment, it can carry out multiple missions in a variety of areas, such as EMS, power-line patrol inspection, aerial law enforcement, aerial photography, aerial seeding and pesticide spraying, fire protection, etc.
技術特點
Technical features
u 構型：單旋翼帶尾槳式常規布局輕型直升機；
Configuration: light helicopter with conventional layout of single-main-rotor plus tail rotor;
u 發動機：一臺霍尼韋爾LTS101-700D-2低油耗發動機；
Engine: a low-fuel-consumption Honeywell engine LTS101-700D-2;
u 旋翼：3片復合材料主槳葉，長壽命星型柔性槳榖；
Rotor: three main rotor blades of composite, long-life star-flex rotor hub;
u 尾槳：2片復合材料尾槳葉，采用蹺蹺板結構形式；
Tail rotor: two composite tail rotor blades of see-saw type;
u 起落架：采用加拿大DART公司帶阻尼器的滑橇和板彈簧尾撐型式的高姿起落裝置；
Undercarriage: high landing gear, the skid with damper and spring plate style of tail support, supplied by Canadian DART;
u 航電系統：2臺多功能顯示器和1臺綜合顯示處理機，集成了發動機監視和告警系統（帶聲音告警）；
Avionics system: two MFDs and one Intergraded display processor, integrating engine monitoring and warning system (with audio warning);
u 左側艙門采用滑軌式設計；
Left door adopts sliding rail-type design;
u 駕駛艙門采用拋放式結構設計
The cockpit is of jettison structure.
u 座艙地板為整體平面式
The cabin floor is of whole place- surface.
u 機艙可用容積4.756m3
Available volume of the cockpit and cabin: 4.756m3
u 客貨艙布局：
Layout of cabin/cargo hold:
客艙
Cabin
座艙后部可安裝二組可折疊的雙人座椅；
The rear part of the cabin can be installed with two couples of foldable double seats;
2名駕駛員+2名乘員
2 pilots+2 passengers
2名駕駛員+4名乘員
2 pilots+4 passengers
1名駕駛員+5名乘員
1 pilot+5 passengers
1名駕駛員+1副擔架和2名醫務人員
1 pilots+1 stretcher and 2 medical persons
貨艙：
Cargo hold:
配有左、右、后三個體積和約1立方米的行李艙
Three luggage holds of about 1 cubic meter total are respectively installed in the left, right and rear part.
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基本性能：
Performance:
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飛行性能
Flight performance
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不可逾越速度 ：
Never Exceed Speed :
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有動力
Power-on
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270Km/h
270Km/h
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無動力
Power-off
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219Km/h
219Km/h
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最大巡航速度
Maximum Cruising Speed
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236 Km/h
236Km/h
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最大斜爬升率
Maximum Inclined Climb Rate
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8.3m/s
8.3m/s
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無地效靜升限
OGE (out of ground effect) Hovering
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2250m
2250m
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有地效靜升限
IGE (in ground effect) Hovering
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2950m
2950m
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最大續航時間
Maximum Endurance
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4.0h
4.0h
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最大使用高度
Max Service Attitude
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6000m
6000m
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最大航程
Max Range
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670Km
670Km
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重量
Weight
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最大起飛重量
Max Take-off Weight
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2200kg
2200kg
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動力
Powerplant
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美國Honeywell公司LTS101-700D-2低油耗發動機
Low-fuel-consumption engine LTS101-700D-2 supplied by American Honeywell Company
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最大連續功率
Max Continuous Power
最大起飛功率
Max Take-off Power
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484.7Kw
484.7Kw
545.9Kw
545.9Kw
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燃油
Fuel
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最大燃油重量
Max Fuel Weight
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423Kg
423Kg
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外形尺寸
External Dimensions
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總長
Overall Length
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13.083m
13.083m
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總高（至槳榖頂點）
Overall Height (to the top of main rotor hub)
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3.299m
3.299m
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機身寬
Fuselage Width
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1.828m
1.828m
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旋翼直徑
Rotor Diameter
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10.69m
10.69m
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尾槳直徑
Tail Rotor Diameter
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1.86m
1.86m
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產品優勢：
Product Advantages:
技術優點
Technical Advantages
u 滑軌式艙門設計便于航拍和醫療救護；
Sliding door design is convenient for aerial photography and medical aid;
u 高姿滑橇和平面開放式地板，可快速、便捷地加裝各類作業設備；
High skid and open plane-surface floor, which are convenient for the installation of various optional mission equipments;
u 行李艙容量大，行李攜帶方便；
Baggage compartment with large volume, which is convenient for baggage carrying;
u 高度集成化綜合航電系統，大大減輕了飛行員的飛行負擔；
Highly Integrated Avionics System (IAS) greatly reduces the workload of pilots;
u 采用低油耗、高可靠性發動機，環保、經濟；
Low-fuel-consumption and highly-reliable engine, green and affordable;
u 雙駕駛操縱設計，方便正副駕駛；
Double control sticks are convenient for pilot and co-pilot’s control.
u 采用開闊大玻璃設計的機頭，駕駛艙寬敞，視野開闊；
Nose of large-open-glass design can provide a spacious cockpit and wide vision;
u 復合材料機身和旋翼系統，飛行重量輕，使用壽命長；
Composite fuselage and rotor system, light flight weight and long operation life cycle;
u 優秀的飛機性能，完美的飛行品質，優良的可控制性和機動性；
Excellent helicopter performance, perfect flight quality, good controllability and maneuverability;
u 座艙采用多功能設計，寬敞、舒適，可配置多種精致內飾和座椅，使用靈活性強，改裝迅速、簡便；
Spacious and comfortable cockpit adopts multi-functional design, which can be equipped with various delicate interiors and seats with strong flexibility as well as quick and easy modification;
u 維護簡單，使用成本低；
Easy maintenance and low operation cost;
u 具有本土化優勢和完善的用戶管理服務體系，可提供快速響應、飛行和機務培訓、工程技術支持等服務，支持快速的維修、備件支援、通航托管等。
Indigenous advantage and complete service system for customer management are available. The services such as quick-response, flight and maintenance training as well as engineering and technical support may be provided and quick repair, spare support, general aviation commissioning may also be supported.
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