平易近机系列
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  • AC311直升机简介 
    Presentation of AC311 Helicopter 
     

        

    AC311直升机是一款2吨级单发单旋翼、带尾桨式多用途民用直升机,该机接纳高橇式起落架,装有一台美国Honeywell公司LTS101-700D-2低油耗发动机,设置高度集成化综合航空电子系统,可供多种挑选的细腻内饰和座椅,整机大量运用复合材料。接纳齐数字化设想和制造手艺,充分体现了“安全性”、“经济性”、“温馨性”、“环保性”设想理念。运用普遍,可知足高原、高寒天气的运用前提。 
    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 “green”. It can be used in wide applications and can satisfy the operation conditions of plateau and extremely cold climate.-j158com金沙

    适航范例   
    Airworthiness Certification Standards  
      
    相符CCAR27部的要求 
    Comply with CCAR 27

    运转范例 
    Operation type
    日夜目视航行 
    Day and Night VFR 
    应用领域     
    Application Area 
    AC311直升机可普遍用于客货运输、航行练习、公事航行,经加装义务装备后可执行多种义务,如医疗救护、电力巡检、空中执法、航拍拍照、飞播灭虫、护林防火等多个范畴。 
    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.

    手艺特性    
    Technical features 

    ◆ 构型:单旋翼带尾桨式通例结构轻型直升机;

    Configuration: light helicopter with conventional layout of single-main-rotor plus tail rotor;

    ◆ 发动机:一台霍尼韦尔LTS101-700D-2低油耗发动机;

    Engine: a low-fuel-consumption Honeywell engine LTS101-700D-2;

    ◆ 旋翼:3片复合材料主桨叶,少寿命星型柔性桨榖;

    Rotor: three main rotor blades of composite, long-life star-flex rotor hub;

    ◆ 尾桨:2片复合材料尾桨叶,接纳跷跷板构造情势;

    Tail rotor: two composite tail rotor blades of see-saw type;

    ◆ 起落架:接纳加拿大DART公司带阻尼器的滑橇和板弹簧尾撑型式的下姿升降装配;

    Undercarriage: high landing gear, the skid with damper and spring plate style of tail support, supplied by Canadian DART;

    ◆ 航电体系:2台多功能显示器和1台综合显现处理机,集成了发动机看管和告警体系(带声音告警);

    Avionics system: two MFDs and one Intergraded display processor, integrating engine monitoring and warning system (with audio warning);

    ◆ 左边舱门接纳滑轨式设想;

    Left door adopts sliding rail-type design;

    ◆ 客货舱结构:

    Layout of cabin/cargo hold:
    客舱 
    Cabin
    座舱后部可安装二组可折叠的双人座椅; 
    The rear part of the cabin can be installed with two couples of foldable double seats;
    2 驾驶员+3乘员 
    2 pilots+3 passengers
    2驾驶员+4乘员 
    2 pilots+4 passengers
    1驾驶员+5乘员  
    1 pilot+5 passengers
    1名飞行员+1副担架和2位医务人员 
    1 pilots+1 stretcher and 2 medical persons
    货舱: 
    Cargo hold:
    配有左、左、后三个体积和约1立方米的行李舱 
    Three luggage holds of about 1 cubic meter total are respectively installed in the left, right and rear part.

    根基机能: 
    Performance:

    航行机能 
    Flight performance

    不可逾越速度 :

    270Km/h

    Never Exceed Speed :

    270Km/h

    最大巡航速度 
    Maximum cruising speed

    236千米/小时(Km/h) 
    236Km/h

    最大斜爬升率 
    Maximum inclined climb rate

    8.3米/秒(m/s) 
    8.3m/s

    无天效静升限 
    OGE (out of ground effect) Hovering

    2250米(m) 
    2250m

    有天效静升限 
    IGE (in ground effect)  Hovering

    2950米(m) 
    2950m

    最大续航工夫   
    Maximum endurance

    4.0h
    4.0h

    最大航程 
    Max. Range

    630Km
    630Km

    重量 
    Weight

    最大腾飞重量 
    Max Take-off Weight

    2200公斤(kg) 
    2200kg

    动力 
    Powerplant

    美国Honeywell公司LTS101-700D-2低油耗发动机 
    Low-fuel-consumption engine LTS101-700D-2 supplied by American Honeywell Company

    最大一连功率 
    Max Continuous Power

    484.7Kw
    484.7Kw

    燃油 
    Fuel

    最大燃油重量  
    Max Fuel Weight  

    423Kg
    423Kg

    外形尺寸 
    External Dimensions 

    总长 
    Overall length

    13.083m
    13.083m

    总下(至桨榖极点) 
    Overall height (to the top of main rotor hub)

    3.299m
    3.299m

    机身宽 
    Fuselage width

    1.828m
    1.828m

    旋翼直径 
    Rotor diameter

    10.69m
    10.69m

    尾桨直径 
    Tail rotor diameter

    1.86m
    1.86m

    产物上风: 
    Product Advantages:
    手艺长处 
    Technical advantages

    ◆ 滑轨式舱门设想便于航拍和医疗救护;

    Sliding door design is convenient for aerial photography and medical aid; 

    ◆ 高度集成化综合航电体系,大大减轻了飞行员的航行肩负;

    Highly Integrated Avionics System (IAS) greatly reduces the workload of pilots;

    ◆ 接纳低油耗、下可靠性发动机,环保、经济;

    Low-fuel-consumption and highly-reliable engine, green and affordable;

    ◆ 接纳坦荡大玻璃设想的机头,驾驶舱宽阔,视野坦荡;

    Nose of large-open-glass design can provide a spacious cockpit and wide vision;

    ◆ 复合材料机身和旋翼体系,航行重量沉,使用寿命少;

    Composite fuselage and rotor system, light flight weight and long operation life cycle;

    ◆ 水滴形气动形状机身和总体布局,线条流通,表面漂亮;

    Water-drop shaped aerodynamic configuration and overall layout, smooth lines and beautiful appearance;

    ◆ 优异的飞机机能,完善的航行品格,优秀的可控制性和机动性;

    Excellent helicopter performance, perfect flight quality, good controllability and maneuverability;

    ◆ 座舱接纳多功能设想,宽阔、温馨,可设置多种细腻内饰和座椅,运用灵活性强,改装敏捷、轻便;

    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;

    ◆ 保护简朴,运用本钱低;

    Easy maintenance and low operation cost;

    ◆ 具有本土化上风和完美的用户管理服务体系,可供应快速相应、航行和机务培训、工程技术支持等效劳,支撑快速的维修、备件增援、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.


  • AC311A直升机简介 
    Presentation of AC311A Helicopter 
      

      
    AC311A直升机是一款2吨级单发、6座单旋翼、带尾桨式高原轻型直升机,该机接纳单/单驾驶设置及高橇式起落架,装有一台微弱的法国透博梅卡公司ARRIEL 2B1A发动机,设置国产高度集成化综合航空电子系统,加装数字化删稳体系及语音告警体系,并预留了多种选装义务装备接口,具有很强的义务拓展才能。同时,整机大量运用复合材料,并提供多种挑选的细腻内饰和座椅。运用普遍,可知足我国大部分地区的运用要求,尤其是高原地区,功课局限可掩盖85%的国土面积。 
    AC311A, a 2-ton-class light civil helicopter with one engine and 6 seats, is of single-main-rotor plus tail rotor, which is especially for high land operation. The helicopter is configured with single/double pilot system and high skid landing gear, a powerful engine ARRIEL 2 B1A from Turbomeca Company, highly Integrated Avionics System (IAS) and digital SAS system and audio warning system. And interfaces for much optional mission equipment are reserved. The helicopter has strong capability of mission extension. At the same time, composite materials are heavily used for the whole aircraft and multiple optional delicate interiors and seats are provided for your option. Its extensive application can meet the operating requirement in the most areas of our country, especially in the high land area. It is applicable to 85% of the territory of China.

    ◆加装一台入口大功率发动机,进步整机高原机能和情况适应性; 
    An imported powerful engine is equipped to improve the plateau performance and environment adaptability of the whole aircraft; 
    ◆安装的一台大功率发动机,功率储备大,高温高原机能佳,灵活机能好,具有很好的义务效能和高原情况适应性; 
    A powerful engine with large power storage is equipped so that the helicopter has excellent high-temperature performance for plateau, good maneuverability and creditable mission efficiency and adaptability to plateau environment. 
    ◆接纳高度集成化的先辈国产化综合航电体系,低落航行肩负; 
    Advanced, highly integrated domestic avionics system is adopted to reduce pilots' burden. 
    ◆接纳构造预留设想,可加装电动绞车、医疗救护单位(ICU)、扬声器、搜刮灯、图象传输体系、应急漂泊体系、氧气体系、农林喷洒体系等多种义务装备,具有优越的义务和功用扩展性; 
    Structure reservation design is adopted so multiple mission equipment such as electric hoist, ICU, loudspeaker, search light, image transmission system, emergency float system, oxygen system, agriculture and forestry sprinkling system etc. can be optionally installed, which makes the aircraft have good mission & function extensibility.      
    ◆国产化水平下,低落对外洋手艺依赖性,进步加改装自立性和开放性; 
    The localization degree of parts and components is high, which reduces the dependence on foreign technology and improves the independence and openness of helicopter modification. 
    ◆整体手艺成熟、先辈,可靠性下,保护和保障简朴,故障率低; 
    The technology is rather mature, advanced, so the reliability of the aircraft is high and the maintenance is easy and the rate of failures is low.

     

    手艺特性 
    Technical features 

    ◆ 构型:单旋翼带尾桨式通例结构轻型直升机;

    Configuration: light helicopter with conventional layout of single-main-rotor plus tail rotor;

    ◆ 发动机:一台透博梅卡ARRIEL 2B1A下机能发动机;

    Engine: a Turbomeca engine ARRIEL 2B1A with excellent performance

    1. 发动机接纳双通道电调(EECU)加电动应急备份控制系统; The Engine adopts dual channel EEC (EECU) plus electric emergency back-up control system;

    2. 旋翼:3片复合材料主桨叶,少寿命星型柔性桨榖;

    Rotor: three main rotor blades of composite, long-life star-flex rotor hub;

    ◆ 尾桨:2片复合材料尾桨叶,接纳跷跷板构造情势;

    Tail rotor: two composite tail rotor blades of see-saw type;

    ◆ 起落架:接纳加拿大DART公司带阻尼器的滑橇和板弹簧尾撑型式的下姿升降装配;

    Undercarriage: high landing gear, the skid with damper and spring plate style of tail support, supplied by Canadian DART;

    1. 电气体系:装有1台6kw的起动发电机和1块24V/15Ah的蓄电池应急电源; Electric system: a 6 kw starter generator and one 24 V/15Ah emergency supply for accumulator are additionally installed;

    2. 航电体系: 2台多功能显现掌握单元和1台发动机参数显现单位,综合集成显现航行义务历程中所需的航向、姿势、速度、高度、数字地图、发动机参数等根基航行信息,并提供通讯、导航、告警等各项功用;

    Avionics System: 2 Multifunction Display control units and 1 engine parameter display unit which will integrate and display the basic flight information during the flight mission, such as the flight direction, attitude, speed, altitude, digital map, engine parameter etc. and provide communication, navigation, warning and other functions;

    1. 导航系统接纳捷联惯导,可实现正在无GPS旌旗灯号条件下的齐自立导航。The navigation system adopts the strapdown inertial navigation, which can realize the totally self-contained navigation without the GPS signal. 

    2. 接纳单驾驶支配体系、单仪表设置;It adopts the dual-pilot control system and the dual instrument arrangement;

    3. 左边舱门接纳滑轨式设想;

    4. Left door adopts sliding rail-type design;

    根基机能 
    Basic performance


    航行机能(ISA,H=0m,最大腾飞重量2250KG) 
    Flight performance (ISA, H=0m, maximum take-off weight 2250 KG)


    最大巡航速度 
    Maximum cruising speed

    240 Km/h 
    240Km/h

    最大斜爬升率 
    Maximum inclined climb rate

    8.3 m/s(状况8.2)
    8.3m/s(状况8.2)

    无天效静升限 
    OGE (out of ground effect) Ceiling

    3200 m(状况3400) 
    3200m(状况3400)

    有天效静升限 
    IGE (in ground effect) Ceiling
    运用升限 
    Service Ceiling

    3900 m(状况4200) 
    3900m(状况4200) 
    6000m(状况5100) 
    6000m(状况5100)

    最大续航工夫  
    Maximum endurance 
    最大航程 
    Max Range

    4.0h(状况3.0) 
    4.0h(状况3.0) 
    630km(状况550) 
    630km(状况550)



    重量 
    Weight


    最大腾飞重量 
    Max Take-off Weight

    2250kg 
    2250kg

    动力 
    Powerplant


    1台法国透博梅卡公司ARRIEL 2B1A发动机 
    One set of engine ARRIEL 2B1A supplied by French Turbomeca Company


    最大一连功率 
    Max Continuous Power
    最大腾飞功率 
    Max Take-off Power

    543Kw
    543Kw
    632Kw
    632Kw

    燃油 
    Fuel


    最大燃油重量  
    Max Fuel Weight  

    423Kg(535L)
    423Kg(535L)

    外形尺寸 
    External Dimensions 


    总长 
    Overall length

    13.083m 
    13.083m

    总下(至桨榖极点) 
    Overall height (to the top of main rotor hub)

    3.299m 
    3.299m

    机身宽 
    Fuselage width

    1.828m 
    1.828m

    旋翼直径 
    Rotor diameter

    10.69m 
    10.69m

    尾桨直径 
    Tail rotor diameter

    1.86m 
    1.86m

    产物上风: 
    Product Advantages:

    ◆ 
    直升机根蒂根基平台成熟、先辈、牢靠,包管了整机优越的出勤率和完好率;

    Basic platform of helicopter is mature, advanced and reliable, which ensures goods availability rate and readiness rate. 

    ◆ 义务改装天真多样,可凭据差别需求改装成警用型/通航功课型/锻练型/医疗救济型/VIP型及运输型等,并可且于军用,加装多种兵器及侦探装备。

    Flexible to modify for different missions. The aircraft can be modified for combat, reconnaissance, transportation etc. and various weapons on cabin door can be optionally installed.

    ◆ 安装一台大功率发动机,功率储备大,高温高原机能好,灵活机能好,具有很好的整机义务效能和高原情况适应性;

     A powerful engine with large power storage is equipped so that the helicopter has excellent high-temperature performance for plateau, good maneuverability and creditable operational efficiency and adaptability to plateau environment. 

    ◆ 接纳高度集成化的先辈综合航电体系,低落航行肩负;

    Advanced, highly integrated avionics system is adopted to reduce pilots' burden. 

    ◆ 增添预留接口,可选装或增添多种义务装备,进步差别义务情况适应性;

    Interfaces are additionally reserved, and much mission equipment can be optionally installed to improve its adaptability to environment of different missions. 

    ◆ 接纳坦荡大玻璃设想的机头,视野坦荡;

    Nose of large-open-glass design can provide wide vision;

    1. 先辈的复合材料机身和齐复合材料旋翼体系,重量沉,使用寿命少; Advanced composite fuselage and all-composite rotor system, light in weight and long in service life.

    2. 优异的航行机能和航行品格,优秀的可控制性和机动性;

    Excellent helicopter performance, perfect flight quality, good controllability and maneuverability;

    ◆ 具有很下的开放性,可凭据用户的要求停止加改装;

     As it has high degree of openness, modification can be done according to customers' requirements. 

    ◆ 整体手艺成熟、先辈,可靠性下,保护和保障简朴,故障率低;

    The technology is rather mature, advanced, so the reliability of the aircraft is high and the maintenance is easy and the rate of failures is low. 

    ◆ 具有完美的用户管理服务体系,可供应快速相应、航行和机务培训、工程技术支持等效劳,支撑快速的维修、备件增援等。

    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.

     


  • AC313直升机简介
    Presentation of AC313 Helicopter


    AC313直升机是一款13吨级大型三发民用直升机。该机接纳轮式起落架和单驾驶体系体例,装三台PT6B-67A发动机,配有高度集成的航电体系。根据CCAR-29R1划定中实用的适航要求,接纳构造预留、空间预留设想原则,停止客货两用根基型研制,可根据日夜目视航行划定规矩(VFR)和仪表航行划定规矩(IFR),正在陆地和无结冰条件下停止目视和仪表航行,可知足高温、高寒天气和高原等庞大区域对直升机的运用要求。 
    AC313 is a brand new 13-ton class civil helicopter powered by three PT6B-67A engines, which can satisfy the operation requirement for all complicated terrains in hot & high and cold areas. Highly integrated avionics suites are provided. Design criterion for structure reservation and space reservation is used in accordance with airworthiness requirement specified by CCAR-29R1 to develop basic versions of both cargo and passenger transport. Visual flight and instrument flight can be performed to IFR and VFR rules in day and night time over land and under icing free conditions.

    适航范例: 
    Airworthiness Standards 
    相符CCAR29部的要求。 
    Comply with CCAR 29

    运转范例: 
    Operation type

    可日夜目视航行。 
    Day and Night VFR
    仪表航行划定规矩 
    Day and Night IFR

     

    根基运用情况 
    Basic operation environment
    航行高度:海平面~6000 m 
    Flight altitude: sea level ~ 6000m
    运用环境温度:-40℃~ISA+35℃
    Operation ambient temperature: -40℃~ISA+35℃ 
    应用领域: 
    Application fields:
    AC313直升机可普遍的应用于搜刮救济、护林灭火、客货运输、医疗救护、悬挂功课、陆地考查等范畴。 
    AC313 helicopter can be widely used in search and rescue, forest firefighting, passenger and cargo transportation, external sling, maritime survey.

    手艺特性: 
    Technical Features
    ◆ 构型:通例单旋翼带尾桨式;

    Configuration: conventional single rotor with tail rotor;

    ◆ 动力装置:3台PT6B-67A发动机,1台辅佐动力装置(APU);

    Power Plant: 3 PT6B-67A engines, 1 auxiliary power unit (APU);

    ◆ 旋翼: 6片复合材料桨叶,钛合金球柔性桨毂;

    Rotor: 6 composite blades with titanium alloy spheriflex hub 

    ◆ 尾桨:5片复合材料尾桨叶,钛合金球柔性构造型式尾桨榖;

    Tail rotor: five composite tail rotor blades, spheriflex tail rotor hub;

    ◆ 起落架:前三点、双轮、弗成收放式起落架,包管起降安稳、平安牢靠。

    Landing gear: non-retractable tricycle dual-wheel landing gears to ensure stable, safe and reliable takeoff and landing. 

    ◆ 航电体系:运用ARINC429和RS422数据总线为重要数据传输体式格局,并经由过程综合显现体系实现综合掌握和显现。要害的装备及功用接纳余度设想,以进步体系的可靠性。

    Avionics system: ARINC429 and RS422 data buses are used as major data transfer methods and integral control and display are achieved through integral display system. Redundancy design is used for critical equipment and function to improve system reliability. 

    ◆ 支配机构:单套并列式部署,正、副驾驶联动

    Control mechanism: dual parallel layout with the inter-linkage between pilot and copilot controls;

    ◆ 航行控制系统:接纳单余度数字式KJ-15A自动驾驶仪,实现四轴掌握

    Flight control system: dual-redundancy digital KJ-15 autopilot is used to realize 4-axis control;

    ◆ 灭火体系:能正在统一动力舱内可一连停止两次灭火,也可正在两个差别的动力舱内离别停止一次灭火;

    Fire extinguishing system: two fire extinguishments can be consecutively performed in the same power compartment and one fire extinguishment can be separately performed in two different power compartments too.

    ◆ 防护装配:尾梁后下段部署有尾撑,防备正在着陆时尾梁和尾桨叶不测撞击空中;

    Protection device: tail support is arranged under the lower aft part of tail boom to prevent tail boom and tail rotor blades striking against the ground during landing. 

    ◆ 座舱结构:2名飞行员+18名搭客;

    Cabin layout: 2 pilots + 18 passengers;
    根基机能:Performance 
    航行机能: 
    Flight Performance
    最大速度/巡航速度                  244 Km/Hr
    Max Speed/Max Cruise Speed   244 Km/Hr
    最大续航工夫                       5.3Hrs
    Max Endurance                       5.3Hrs
    最大航行高度                      6000m
    Max. Flight Altitude                6000m
    有/无天效悬停升限             2800/100m
    HIGE/HOGE                         2800/100m
    最大航程                             1050Km 
    Max. Range                          1050Km 
    最大爬升率                          7.6m/s
    Max Rate-of-Climb                7.6m/s

    重量:Weight  
    空重                     7560 Kg 
    Empty Weight             7560 Kg 
    最大腾飞重量             13000 Kg
    Max Take-off Weight        13000 Kg
    有用载重                 4000 Kg
    Max Payload              4000 Kg
    最大吊运重量             5000Kg
    Max. Sling Load           5000Kg

    动力:Powerplant 
    三台加普惠PT6B-67A发动机, 
    3 P&WC PT6B-67A engines
    最大空中起动高度  4500m, 
    Max. Ground Starting Altitude: 4500m
    最大空中起动高度   6000m, 
    Max. Aerial Starting Altitude: 6000m
    腾飞功率  1447kw  
    Take-off Power: 1447Kw
    最大一连功率  1249kw 
    Max. Continuous Power: 1249Kw

    燃油:Fuel
    有用总的燃油量:3800 Kg 
    Total Effective Fuel Volume:  3800Kg
    20min可用余油量:390 Kg; 
    Useful Reserve for 20min: 390Kg;
    尺度油箱容量     4740L 
    Standard Tank Volume: 4740L 
    外形尺寸 
    External Dimensions
    全长(旋翼扭转)                           23.045 m
    Overall Length (Rotors turning)         23.045 m
    齐下(空重,尾桨扭转)                    6.741 m
    Overall Height (empty weight, tail rotor turning)
    6.741 m
    齐宽(旋翼迁移转变时)                 18.900 m
    Width (Rotors turning)                 18.900 m
    旋翼直径                           18.900 m
    Rotor Diameter                       18.900 m
    尾桨直径                           4.000 m
    Tail Rotor Diameter                  4.000 m 
    产物上风: 
    Product Advantage:

    ◆ 
    载重量大,悬挂能力强

    Large payload carrying capability as well as strong external sling load capability;

    ◆ 精彩的航程和续航才能

    Excellent range and endurance capability;

    ◆ 大量运用复合材料,延伸使用寿命

    Composite material is widely used to extend service life cycle 

    ◆ 综合显现控制系统为飞行员供应航行状况信息、导航信息、电机管理体系的备份显现及其它机载信息的综合显现,进步人机工效。

    Integral display and control system provides flight status information, navigation information, standby display of electromechanical management system as well as integral display of other airborne information to the pilots to improve man-machine ergonomics. 

    ◆ 正、副驾驶联动,平安牢靠

    Inter-linkage between pilot and copilot controls makes it safe and reliable.

    ◆ KJ-15A自动驾驶仪,减轻驾驶肩负

    KJ-15 autopilot reduces the workload of the pilot.

    ◆ 抗坠毁座椅、告警体系使直升机更平安、牢靠

    Crashworthy seats and warning system make the helicopter safer and more reliable;

    ◆ 机中照明体系供应直升机的航向和方位信息和防撞告警旌旗灯号,并正在着陆时照亮四周园地,使飞行员能清楚目视直升机着陆时的位置和高度。

    External lighting system provides the heading and position information of the helicopter as well as anti-collision signal and illuminates the surrounding areas during landing to make the pilot be able to legibly visually see the position and altitude during helicopter landing. 

    ◆ 机舱容量大,座椅柔嫩,温馨性好

    Spacious cabin and soft seats with excellent comfort;

    ◆ 运用本钱低,便于保护

    Low operation cost and easy of maintenance, 

    ◆ 具有本土化上风和完美的用户管理服务体系,可供应快速相应、航行和机务培训、工程技术支持等效劳,支撑快速的维修、备件增援、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

     

  • AC311A直升机简介
    Presentation of AC311A Helicopter
      

     
    AC311A直升机是一款2吨级单发、6座单旋翼、带尾桨式高原轻型直升机,该机接纳单/单驾驶设置及高橇式起落架,装有一台微弱的法国透博梅卡公司ARRIEL 2B1A发动机,设置国产高度集成化综合航空电子系统,加装数字化删稳体系及语音告警体系,并预留了多种选装义务装备接口,具有很强的义务拓展才能。同时,整机大量运用复合材料,并提供多种挑选的细腻内饰和座椅。运用普遍,可知足我国大部分地区的运用要求,尤其是高原地区,功课局限可掩盖85%的国土面积。
    AC311A, a 2-ton-class light civil helicopter with one engine and 6 seats, is of single-main-rotor plus tail rotor, which is especially for high land operation. The helicopter is configured with single/double pilot system and high skid landing gear, a powerful engine ARRIEL 2 B1A from Turbomeca Company, highly Integrated Avionics System (IAS) and digital SAS system and audio warning system. And interfaces for much optional mission equipment are reserved. The helicopter has strong capability of mission extension. At the same time, composite materials are heavily used for the whole aircraft and multiple optional delicate interiors and seats are provided for your option. Its extensive application can meet the operating requirement in the most areas of our country, especially in the high land area. It is applicable to 85% of the territory of China.

    ◆加装一台入口大功率发动机,进步整机高原机能和情况适应性;
    An imported powerful engine is equipped to improve the plateau performance and environment adaptability of the whole aircraft;
    ◆安装的一台大功率发动机,功率储备大,高温高原机能佳,灵活机能好,具有很好的义务效能和高原情况适应性;
    A powerful engine with large power storage is equipped so that the helicopter has excellent high-temperature performance for plateau, good maneuverability and creditable mission efficiency and adaptability to plateau environment.
    ◆接纳高度集成化的先辈国产化综合航电体系,低落航行肩负;
    Advanced, highly integrated domestic avionics system is adopted to reduce pilots' burden.
    ◆接纳构造预留设想,可加装电动绞车、医疗救护单位(ICU)、扬声器、搜刮灯、图象传输体系、应急漂泊体系、氧气体系、农林喷洒体系等多种义务装备,具有优越的义务和功用扩展性;
    Structure reservation design is adopted so multiple mission equipment such as electric hoist, ICU, loudspeaker, search light, image transmission system, emergency float system, oxygen system, agriculture and forestry sprinkling system etc. can be optionally installed, which makes the aircraft have good mission & function extensibility.     
    ◆国产化水平下,低落对外洋手艺依赖性,进步加改装自立性和开放性;
    The localization degree of parts and components is high, which reduces the dependence on foreign technology and improves the independence and openness of helicopter modification.
    ◆整体手艺成熟、先辈,可靠性下,保护和保障简朴,故障率低;
    The technology is rather mature, advanced, so the reliability of the aircraft is high and the maintenance is easy and the rate of failures is low.

     

    手艺特性
    Technical features

    ◆ 构型:单旋翼带尾桨式通例结构轻型直升机;

    Configuration: light helicopter with conventional layout of single-main-rotor plus tail rotor;

    ◆ 发动机:一台透博梅卡ARRIEL 2B1A下机能发动机;

    Engine: a Turbomeca engine ARRIEL 2B1A with excellent performance

    1. 发动机接纳双通道电调(EECU)加电动应急备份控制系统; The Engine adopts dual channel EEC (EECU) plus electric emergency back-up control system;
    2. 旋翼:3片复合材料主桨叶,少寿命星型柔性桨榖;

    Rotor: three main rotor blades of composite, long-life star-flex rotor hub;

    ◆ 尾桨:2片复合材料尾桨叶,接纳跷跷板构造情势;

    Tail rotor: two composite tail rotor blades of see-saw type;

    ◆ 起落架:接纳加拿大DART公司带阻尼器的滑橇和板弹簧尾撑型式的下姿升降装配;

    Undercarriage: high landing gear, the skid with damper and spring plate style of tail support, supplied by Canadian DART;

    1. 电气体系:装有1台6kw的起动发电机和1块24V/15Ah的蓄电池应急电源; Electric system: a 6 kw starter generator and one 24 V/15Ah emergency supply for accumulator are additionally installed;
    2. 航电体系: 2台多功能显现掌握单元和1台发动机参数显现单位,综合集成显现航行义务历程中所需的航向、姿势、速度、高度、数字地图、发动机参数等根基航行信息,并提供通讯、导航、告警等各项功用;

    Avionics System: 2 Multifunction Display control units and 1 engine parameter display unit which will integrate and display the basic flight information during the flight mission, such as the flight direction, attitude, speed, altitude, digital map, engine parameter etc. and provide communication, navigation, warning and other functions;

    1. 导航系统接纳捷联惯导,可实现正在无GPS旌旗灯号条件下的齐自立导航。The navigation system adopts the strapdown inertial navigation, which can realize the totally self-contained navigation without the GPS signal. 
    2. 接纳单驾驶支配体系、单仪表设置;It adopts the dual-pilot control system and the dual instrument arrangement;
    3. 左边舱门接纳滑轨式设想;
    4. Left door adopts sliding rail-type design;

    根基机能
    Basic performance

     

    航行机能(ISA,H=0m,最大腾飞重量2250KG)
    Flight performance (ISA, H=0m, maximum take-off weight 2250 KG)

     

    最大巡航速度
    Maximum cruising speed

    240 Km/h
    240Km/h

    最大斜爬升率
    Maximum inclined climb rate

    8.3 m/s(状况8.2)
    8.3m/s(状况8.2)

    无天效静升限
    OGE (out of ground effect) Ceiling

    3200 m(状况3400)
    3200m(状况3400)

    有天效静升限
    IGE (in ground effect) Ceiling
    运用升限
    Service Ceiling

    3900 m(状况4200)
    3900m(状况4200)
    6000m(状况5100)
    6000m(状况5100)

    最大续航工夫 
    Maximum endurance
    最大航程
    Max Range

    4.0h(状况3.0)
    4.0h(状况3.0)
    630km(状况550)
    630km(状况550)

     

     

    重量
    Weight

     

    最大腾飞重量
    Max Take-off Weight

    2250kg
    2250kg

    动力
    Powerplant

     

    1台法国透博梅卡公司ARRIEL 2B1A发动机
    One set of engine ARRIEL 2B1A supplied by French Turbomeca Company

     

    最大一连功率
    Max Continuous Power
    最大腾飞功率
    Max Take-off Power

    543Kw
    543Kw
    632Kw
    632Kw

    燃油
    Fuel

     

    最大燃油重量 
    Max Fuel Weight  

    423Kg(535L)
    423Kg(535L)

    外形尺寸
    External Dimensions 

     

    总长
    Overall length

    13.083m
    13.083m

    总下(至桨榖极点)
    Overall height (to the top of main rotor hub)

    3.299m
    3.299m

    机身宽
    Fuselage width

    1.828m
    1.828m

    旋翼直径
    Rotor diameter

    10.69m
    10.69m

    尾桨直径
    Tail rotor diameter

    1.86m
    1.86m

    产物上风:
    Product Advantages:

    直升机根蒂根基平台成熟、先辈、牢靠,包管了整机优越的出勤率和完好率;

    Basic platform of helicopter is mature, advanced and reliable, which ensures goods availability rate and readiness rate.

    ◆ 义务改装天真多样,可凭据差别需求改装成警用型/通航功课型/锻练型/医疗救济型/VIP型及运输型等,并可且于军用,加装多种兵器及侦探装备。

    Flexible to modify for different missions. The aircraft can be modified for combat, reconnaissance, transportation etc. and various weapons on cabin door can be optionally installed.

    ◆ 安装一台大功率发动机,功率储备大,高温高原机能好,灵活机能好,具有很好的整机义务效能和高原情况适应性;

     A powerful engine with large power storage is equipped so that the helicopter has excellent high-temperature performance for plateau, good maneuverability and creditable operational efficiency and adaptability to plateau environment.

    ◆ 接纳高度集成化的先辈综合航电体系,低落航行肩负;

    Advanced, highly integrated avionics system is adopted to reduce pilots' burden.

    ◆ 增添预留接口,可选装或增添多种义务装备,进步差别义务情况适应性;

    Interfaces are additionally reserved, and much mission equipment can be optionally installed to improve its adaptability to environment of different missions.

    ◆ 接纳坦荡大玻璃设想的机头,视野坦荡;

    Nose of large-open-glass design can provide wide vision;

    1. 先辈的复合材料机身和齐复合材料旋翼体系,重量沉,使用寿命少; Advanced composite fuselage and all-composite rotor system, light in weight and long in service life.
    2. 优异的航行机能和航行品格,优秀的可控制性和机动性;

    Excellent helicopter performance, perfect flight quality, good controllability and maneuverability;

    ◆ 具有很下的开放性,可凭据用户的要求停止加改装;

     As it has high degree of openness, modification can be done according to customers' requirements.

    ◆ 整体手艺成熟、先辈,可靠性下,保护和保障简朴,故障率低;

    The technology is rather mature, advanced, so the reliability of the aircraft is high and the maintenance is easy and the rate of failures is low.

    ◆ 具有完美的用户管理服务体系,可供应快速相应、航行和机务培训、工程技术支持等效劳,支撑快速的维修、备件增援等。

    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.

     

  • AC313直升机简介
    Presentation of AC313 Helicopter


    AC313直升机是一款13吨级大型三发民用直升机。该机接纳轮式起落架和单驾驶体系体例,装三台PT6B-67A发动机,配有高度集成的航电体系。根据CCAR-29R1划定中实用的适航要求,接纳构造预留、空间预留设想原则,停止客货两用根基型研制,可根据日夜目视航行划定规矩(VFR)和仪表航行划定规矩(IFR),正在陆地和无结冰条件下停止目视和仪表航行,可知足高温、高寒天气和高原等庞大区域对直升机的运用要求。
    AC313 is a brand new 13-ton class civil helicopter powered by three PT6B-67A engines, which can satisfy the operation requirement for all complicated terrains in hot & high and cold areas. Highly integrated avionics suites are provided. Design criterion for structure reservation and space reservation is used in accordance with airworthiness requirement specified by CCAR-29R1 to develop basic versions of both cargo and passenger transport. Visual flight and instrument flight can be performed to IFR and VFR rules in day and night time over land and under icing free conditions.

    适航范例:
    Airworthiness Standards
    相符CCAR29部的要求。
    Comply with CCAR 29

    运转范例:
    Operation type

    可日夜目视航行。
    Day and Night VFR
    仪表航行划定规矩
    Day and Night IFR

     

    根基运用情况
    Basic operation environment
    航行高度:海平面~6000 m
    Flight altitude: sea level ~ 6000m
    运用环境温度:-40℃~ISA+35℃
    Operation ambient temperature: -40℃~ISA+35℃
    应用领域:
    Application fields:
    AC313直升机可普遍的应用于搜刮救济、护林灭火、客货运输、医疗救护、悬挂功课、陆地考查等范畴。
    AC313 helicopter can be widely used in search and rescue, forest firefighting, passenger and cargo transportation, external sling, maritime survey.

    手艺特性:
    Technical Features
    ◆ 构型:通例单旋翼带尾桨式;

    Configuration: conventional single rotor with tail rotor;

    ◆ 动力装置:3台PT6B-67A发动机,1台辅佐动力装置(APU);

    Power Plant: 3 PT6B-67A engines, 1 auxiliary power unit (APU);

    ◆ 旋翼: 6片复合材料桨叶,钛合金球柔性桨毂;

    Rotor: 6 composite blades with titanium alloy spheriflex hub

    ◆ 尾桨:5片复合材料尾桨叶,钛合金球柔性构造型式尾桨榖;

    Tail rotor: five composite tail rotor blades, spheriflex tail rotor hub;

    ◆ 起落架:前三点、双轮、弗成收放式起落架,包管起降安稳、平安牢靠。

    Landing gear: non-retractable tricycle dual-wheel landing gears to ensure stable, safe and reliable takeoff and landing.

    ◆ 航电体系:运用ARINC429和RS422数据总线为重要数据传输体式格局,并经由过程综合显现体系实现综合掌握和显现。要害的装备及功用接纳余度设想,以进步体系的可靠性。

    Avionics system: ARINC429 and RS422 data buses are used as major data transfer methods and integral control and display are achieved through integral display system. Redundancy design is used for critical equipment and function to improve system reliability.

    ◆ 支配机构:单套并列式部署,正、副驾驶联动

    Control mechanism: dual parallel layout with the inter-linkage between pilot and copilot controls;

    ◆ 航行控制系统:接纳单余度数字式KJ-15A自动驾驶仪,实现四轴掌握

    Flight control system: dual-redundancy digital KJ-15 autopilot is used to realize 4-axis control;

    ◆ 灭火体系:能正在统一动力舱内可一连停止两次灭火,也可正在两个差别的动力舱内离别停止一次灭火;

    Fire extinguishing system: two fire extinguishments can be consecutively performed in the same power compartment and one fire extinguishment can be separately performed in two different power compartments too.

    ◆ 防护装配:尾梁后下段部署有尾撑,防备正在着陆时尾梁和尾桨叶不测撞击空中;

    Protection device: tail support is arranged under the lower aft part of tail boom to prevent tail boom and tail rotor blades striking against the ground during landing.

    ◆ 座舱结构:2名飞行员+18名搭客;

    Cabin layout: 2 pilots + 18 passengers;
    根基机能:Performance
    航行机能:
    Flight Performance
    最大速度/巡航速度                  244 Km/Hr
    Max Speed/Max Cruise Speed   244 Km/Hr
    最大续航工夫                       5.3Hrs
    Max Endurance                       5.3Hrs
    最大航行高度                      6000m
    Max. Flight Altitude                6000m
    有/无天效悬停升限             2800/100m
    HIGE/HOGE                         2800/100m
    最大航程                             1050Km
    Max. Range                          1050Km
    最大爬升率                          7.6m/s
    Max Rate-of-Climb                7.6m/s

    重量:Weight 
    空重                     7560 Kg
    Empty Weight             7560 Kg
    最大腾飞重量             13000 Kg
    Max Take-off Weight        13000 Kg
    有用载重                 4000 Kg
    Max Payload              4000 Kg
    最大吊运重量             5000Kg
    Max. Sling Load           5000Kg

    动力:Powerplant
    三台加普惠PT6B-67A发动机,
    3 P&WC PT6B-67A engines
    最大空中起动高度  4500m,
    Max. Ground Starting Altitude: 4500m
    最大空中起动高度   6000m,
    Max. Aerial Starting Altitude: 6000m
    腾飞功率  1447kw 
    Take-off Power: 1447Kw
    最大一连功率  1249kw
    Max. Continuous Power: 1249Kw

    燃油:Fuel
    有用总的燃油量:3800 Kg
    Total Effective Fuel Volume:  3800Kg
    20min可用余油量:390 Kg;
    Useful Reserve for 20min: 390Kg;
    尺度油箱容量     4740L
    Standard Tank Volume: 4740L
    外形尺寸
    External Dimensions
    全长(旋翼扭转)                           23.045 m
    Overall Length (Rotors turning)         23.045 m
    齐下(空重,尾桨扭转)                    6.741 m
    Overall Height (empty weight, tail rotor turning)
    6.741 m
    齐宽(旋翼迁移转变时)                 18.900 m
    Width (Rotors turning)                 18.900 m
    旋翼直径                           18.900 m
    Rotor Diameter                       18.900 m
    尾桨直径                           4.000 m
    Tail Rotor Diameter                  4.000 m
    产物上风:
    Product Advantage:

    载重量大,悬挂能力强

    Large payload carrying capability as well as strong external sling load capability;

    ◆ 精彩的航程和续航才能

    Excellent range and endurance capability;

    ◆ 大量运用复合材料,延伸使用寿命

    Composite material is widely used to extend service life cycle

    ◆ 综合显现控制系统为飞行员供应航行状况信息、导航信息、电机管理体系的备份显现及其它机载信息的综合显现,进步人机工效。

    Integral display and control system provides flight status information, navigation information, standby display of electromechanical management system as well as integral display of other airborne information to the pilots to improve man-machine ergonomics.

    ◆ 正、副驾驶联动,平安牢靠

    Inter-linkage between pilot and copilot controls makes it safe and reliable.

    ◆ KJ-15A自动驾驶仪,减轻驾驶肩负

    KJ-15 autopilot reduces the workload of the pilot.

    ◆ 抗坠毁座椅、告警体系使直升机更平安、牢靠

    Crashworthy seats and warning system make the helicopter safer and more reliable;

    ◆ 机中照明体系供应直升机的航向和方位信息和防撞告警旌旗灯号,并正在着陆时照亮四周园地,使飞行员能清楚目视直升机着陆时的位置和高度。

    External lighting system provides the heading and position information of the helicopter as well as anti-collision signal and illuminates the surrounding areas during landing to make the pilot be able to legibly visually see the position and altitude during helicopter landing.

    ◆ 机舱容量大,座椅柔嫩,温馨性好

    Spacious cabin and soft seats with excellent comfort;

    ◆ 运用本钱低,便于保护

    Low operation cost and easy of maintenance,

    ◆ 具有本土化上风和完美的用户管理服务体系,可供应快速相应、航行和机务培训、工程技术支持等效劳,支撑快速的维修、备件增援、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