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 AC301直升机为2吨级单旋翼带尾桨型式多用途民用直升机。装有一台WZ8D型发动机,能够在陆上、跨越小面积水域无结冰条件下,作昼间和夜间目视规则飞行,是民用航空和通用航空需要最广泛的机型之一。

AC301 is a two-ton class multi-purpose helicopter. It is of single rotor system with tail rotor, which is powered by one WZ8D engine. Visual flight rules can be performed in day and night time over land or across a small area of water under icing free conditions. It is one of the most widely used helicopter models in civil aviation and general aviation area.
适航规范:
Airworthiness Standards
符合CCAR27的要求
Comply with CCAR 27
 
运行类型:
Operation type:
        昼夜目视飞行;
Day and Night VFR;
 
应用领域:
Application fields:
可用于人员和货物运输、人员培训、公务及私人飞行,通过客户化改装后可执行警用、航拍、交通指挥、侦察通讯、搜索救援等任务。
AC301A can be used for personal and cargo transport, training, business and private flight. It can also be used implement the missions such as policing, aerial photography, traffic command, Surveillance and communication, search and rescue etc. after customized modifications.
 
基本使用环境:
Basic operation condition:
       飞行高度:海平面~4400m;
       Flight altitude: sea level~4400m;
       使用温度范围:-40℃~+50℃;
       Operation temperature range: -40℃~+50℃
 
 
技术特点:
Technical characteristics:
 
u 构型:常规单旋翼带尾桨式;
Configuration: conventional single rotor with tail rotor;
u 发动机:WZ8D型发动机,具有完整的起动系统、燃油供油系统和调节装置,装有磁性螺塞及金属屑探测器;
Engine: WZ8D engine with complete starting system, fuel supply system and fuel control. It is equipped with magnetic plug and chip detector;
u 旋翼:3片复合材料旋翼系统,星形柔性桨毂,并装有旋翼刹车装置;
Rotor: three-bladed composite rotor system, star-flex hub, rotor brake is provided.
u 尾桨:2片复合材料尾桨叶,采用跷跷板结构形式;
Tail rotor: two composite tail rotor blades, see-saw structure are used;
u 机身:采用金属结构机身,整机大面积使用复合材料;
Fuselage: the fuselage is metallic structure with large area use of composite material in the whole helicopter.
u 起落架:采用加拿大DART公司带阻尼器的滑橇和板弹簧尾撑型式的高姿起落装置;
Undercarriage: high landing gear, the skid with damper and spring plate style of tail support, supplied by Canadian DART;
u 航电系统:2台多功能显示器,集成了发动机监视和告警系统(带声音告警);
Avionics system: two MFDs and one Intergraded display processor, integrating engine monitoring and warning system (with audio warning);
u 货舱:配有约1立方米的行李舱;
Cargo hold: 1 cubic meter of the baggage hold is available;
u 客/货舱布局:
The layout of cabin/cargo hold:
客舱:2个双人后排座椅,可向上折叠,每个座位均配有组合安          全带及肩带;
Cabin: two double rear seats which can fold upwards. Each seat has assembly safety belt and strap;
2驾驶员+3乘员
Two pilots+3 passengers
2驾驶员+4乘员 
Two pilots+4 passengers
1驾驶员+5乘员 
One pilot+5 passengers
1名飞行员+1副担架和2位医务人员
Two pilots+1 stretcher and 2 medical persons
基本性能:Basic performance:
 
飞行性能:Flight performance:
不可逾越速度 :
Never exceed speed:
有动力              278Km/h
Power-on            278Km/h
无动力              225Km/h
Power-off            225Km/h
最大巡航速度               238 Km/h
Maximum cruising speed       238 Km/h
最大斜爬升率               8.8 m/s
Maximum climb rate          8.8 m/s
无地效悬停升限             2000m
Hovering ceiling(OGE)        2000m
有地效悬停升限             2740m
Hovering ceiling(IGE)        2740m
最大续航时间               3.83h
Maximum endurance          3.83h
动升限                    4400m
Dynamic ceiling             4400m
最大使用高度              5000m
Max Service Attitude         5000m
最大航程                  640Km
Max range                 640Km
 
重量:Weight
 
最大起飞重量               2200千克(kg)
Maximum take-off weight      2200千克(kg)
最大燃油重量               423Kg(535L)
Maximum fuel weight         423Kg(535L)
动力:Powerplant
 
WZ8D型发动机
WZ8D engine
最大连续功率                   450Kw
Max Continuous Power            450Kw
最大起飞功率                   510Kw
Max Take-off Power              510Kw
 
燃油:Fuel
标准油箱容量                    423kg    535L
Standard Tank Volume              423kg    535L
 
外形尺寸                
External dimensions
总长                       13.012m
Overall length                13.012m
总高(至桨榖顶点)            3.14m
Overall height (to the top of rotor hub)    3.14m
机身宽                     1.8m
Fuselage width               1.8m
主旋翼直径                 10.69m
Main rotor diameter           10.69m
尾桨直径                   1.86m
Tail rotor diameter            1.86m
 
 
 
产品优势:
Product Advantage:
u 出色的航程和续航能力
Excellent range and endurance capability;
u 左侧门采用滑轨式设计,便于航拍和医疗救护;
The left door adopts sliding rail-type design, convenient for aerial photography and EMS;
u 良好的气动外形和总体布局,外形线条流畅,气动阻力减小;
Nice aerodynamic shape and overall layout, smooth lines, aerodynamic reduced;
u 优良的可操作性及优秀的飞行稳定性和操纵响应特性
Fine maneuverability or outstanding flight stability and response characteristic of control;
u 采用视觉和听觉双重故障告警系统,以便飞行员采取紧急措施,安全性高;
Visual & audio warning system, convenient for pilots to take urgent measures, high safety is provided;
u 客舱采用多功能设计,使用灵活性强,改装迅速、简便;
Cabin adopts multi-function design with strong flexibility and quick and simple modification;
u 大面积使用复合材料结构重量轻,使用寿命长,提高抗腐蚀性;
Composite material is widely used, light weight, long life cycle and improved corrosion resistance;
u 驾驶舱宽敞,视野开阔;
Spacious cockpit and wide vision;
u 多种精致内饰和座椅;
Various dedicate interior and seat;
u 良好的密封性能,舱内噪音低;
Good sealing performance and low noise in the cabin;
u 外场可更换零件,维修简便;
LRU is used and it is easy of maintenance;
u 具有本土化优势和完善的用户管理服务体系,可提供快速响应、飞行和机务培训、工程技术支持等服务,支持快速的维修、备件支援、通航托管等。
Indigenous advantage and complete service system for customer management are available. The service such as quick-response, flight and maintenance training as well as engineering and technical support may be provided and quick repair, spare part, general aviation commissioning may also be supported.
扫描二维码有惊喜
扫描二维码有惊喜