军机系列
   














  • 直-8型机简介

    直8型机是亚洲最大吨位的多用途直升机,也是我国交付部队使用的第一种直升机。该机采用单旋翼带尾桨常规气动布局,配装三台发动机,装有前三点式两栖起落架。该机具有安全性好、三防能力强和功能全等优势,可广泛适用于军用、通用航空和准军事领域的需求,可执行武器装备/人员/货物运输、森林防火、抢险救灾、客运航班、医疗救护、搜索救援、物资运输、地质勘探、地理测绘、建筑施工、海洋考察、旅游观光、公务飞行和反恐维稳等任务。


  • 直-10型机简介

    直-10型机是我国自主研制的第一种专用武装直升机,该机采用单旋翼带尾桨构型,窄机身串列式驾驶舱、后三点式起落架布局。具有优良的飞行性能、较高的战场生存力、多机空地信息化协同、连续、快速攻击多目标能力,可在全天候、复杂战场环境和野外保障条件下遂行多种作战任务。综合作战效能与国外现役先进武装直升机相当。

  • 直-11型机简介

    直11型直升机是由中航工业昌飞和中国直升机设计研究所共同研制生产的多用途轻型直升机,是我国自行设计研制的第一个具有自主知识产权的直升机机种,也是部队服役出勤率最高的直升机机种。该机已取得中国民航总局颁发的型号合格证和生产许可证,可广泛用于空中巡逻、空中指挥、通讯联络、公务运输、交通监理、消防灭火、紧急救援、缉私缉毒、防爆反恐、火力支援和边境巡逻等领域。

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    直-11WB型机简介

     

           直11WB“鵟”侦察攻击直升机是一款具有国际先进水平的2吨级轻型直升机,该机采用全数字化设计和制造技术,不仅配备了红外激光干扰吊舱,而且机枪、火箭发射器、反坦克导弹等应有尽有,能够执行对地攻击、战场侦察、武装反恐等多种任务,是“信息融合、网络中心战、空地一体战”的攻击侦察作战利器。

            

    一张图了解直11WB 


    直11WB性能展示视频 

           

     

     

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  • 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,该机采用单/双驾驶配置及高橇式起落架,装有一台强劲的法国透博梅卡公司ARRIEL 2B1A发动机,配置国产高度集成化综合航空电子系统,加装数字化增稳系统及语音告警系统,并预留了多种选装任务设备接口,具备很强的任务拓展能力。同时,整机大量使用复合材料,并提供多种选择的精致内饰和座椅。应用广泛,可满足我国大部分地区的使用要求,尤其是高原区域,作业范围可覆盖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.

    ◆加装一台进口大功率发动机,提高整机高原性能和环境适应性;
    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,功率贮备大,高温高原性能佳,机动性能好,具有很好的任务效能和高原环境适应性;
    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.
    ◆采用高度集成化的先进国产化综合航电系统,降低飞行负担;
    Advanced, highly integrated domestic avionics system is adopted to reduce pilots' burden.
    ◆采用结构预留设计,可加装电动绞车、医疗救护单元(ICU)、扬声器、搜索灯、图像传输系统、应急漂浮系统、氧气系统、农林喷洒系统等多种任务设备,具有良好的任务和功能扩展性;
    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.     
    ◆国产化程度高,降低对国外技术依赖性,提高加改装自主性和开放性;
    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.
    ◆整体技术成熟、先进,可靠性高,维护和保障简单,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.

     

    技术特点
    Technical features

    ◆ 构型:单旋翼带尾桨式常规布局轻型直升机;

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

    ◆ 发动机:一台透博梅卡ARRIEL 2B1A高性能发动机;

    Engine: a Turbomeca engine ARRIEL 2B1A with excellent performance

    1. 发动机采用双通道电调(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,长寿命星型柔性桨榖;

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

    ◆ 尾桨:2片复合材料尾桨叶,采用跷跷板结构形式;

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

    ◆ 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;

    1. 电气系统: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. 航电系统: 2台多功能显示控制单元和1台发动机参数显示单元,综合集成显示飞行任务过程中所需的航向、姿态、速度、高度、数字地图、发动机参数等基本飞行信息,并提供通信、导航、告警等各项功能;

    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. 导航系统采用捷联惯导,可实现在无GPS信号条件下的全自主导航。The navigation system adopts the strapdown inertial navigation, which can realize the totally self-contained navigation without the GPS signal. 
    2. 采用双驾驶操纵系统、双仪表配置;It adopts the dual-pilot control system and the dual instrument arrangement;
    3. 左侧舱门采用滑轨式设计;
    4. Left door adopts sliding rail-type design;

    基本性能
    Basic performance

     

    飞行性能(ISA,H=0m,最大起飞重量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(状态8.2)
    8.3m/s(状态8.2)

    无地效静升限
    OGE (out of ground effect) Ceiling

    3200 m(状态3400)
    3200m(状态3400)

    有地效静升限
    IGE (in ground effect) Ceiling
    使用升限
    Service Ceiling

    3900 m(状态4200)
    3900m(状态4200)
    6000m(状态5100)
    6000m(状态5100)

    最大续航时间 
    Maximum endurance
    最大航程
    Max Range

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

     

     

    重量
    Weight

     

    最大起飞重量
    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

     

    最大连续功率
    Max Continuous Power
    最大起飞功率
    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

    总高(至桨榖顶点)
    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

    产品优势:
    Product Advantages:

    直升机基础平台成熟、先进、可靠,保证了整机良好的出勤率和完好率;

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

    ◆ 任务改装灵活多样,可根据不同需要改装成警用型/通航作业型/教练型/医疗救援型/VIP型及运输型等,并可且于军用,加装多种武器及侦察设备。

    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,功率贮备大,高温高原性能好,机动性能好,具有很好的整机任务效能和高原环境适应性;

     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.

    ◆ 采用高度集成化的先进综合航电系统,降低飞行负担;

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

    ◆ 增加预留接口,可选装或增加多种任务设备,提高不同任务环境适应性;

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

    ◆ 采用开阔大玻璃设计的机头,视野开阔;

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

    1. 先进的复合材料机身和全复合材料旋翼系统,重量轻,使用寿命长; Advanced composite fuselage and all-composite rotor system, light in weight and long in service life.
    2. 优秀的飞行性能和飞行品质,优良的可控制性和机动性;

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

    ◆ 具有很高的开放性,可根据用户的要求进行加改装;

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

    ◆ 整体技术成熟、先进,可靠性高,维护和保障简单,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。该机采用轮式起落架和双驾驶体制,装三台PT6B-67A发动机,配有高度集成的航电系统。依据CCAR-29R1规定中适用的适航要求,采用结构预留、空间预留设计准则,进行客货两用基本型研制,可按照昼夜目视飞行规则(VFR)和仪表飞行规则(IFR),在陆地和无结冰条件下进行目视和仪表飞行,可满足高温、高寒气候和高原等复杂地区对直升机的使用要求。
    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.

    适航规范:
    Airworthiness Standards
    符合CCAR29部的要求。
    Comply with CCAR 29

    运行类型:
    Operation type

    可昼夜目视飞行。
    Day and Night VFR
    仪表飞行规则
    Day and Night IFR

     

    基本使用环境
    Basic operation environment
    飞行高度:海平面~6000 m
    Flight altitude: sea level ~ 6000m
    使用环境温度:-40℃~ISA+35℃
    Operation ambient temperature: -40℃~ISA+35℃
    应用领域:
    Application fields:
    AC313直升机可广泛的应用于搜索救援、护林灭火、客货运输、医疗救护、吊挂作业、海洋考察等领域。
    AC313 helicopter can be widely used in search and rescue, forest firefighting, passenger and cargo transportation, external sling, maritime survey.

    技术特点:
    Technical Features
    ◆ 构型:常规单旋翼带尾桨式;

    Configuration: conventional single rotor with tail rotor;

    ◆ 动力装置:3台PT6B-67A发动机,1台辅助动力装置(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,钛合金球柔性结构型式尾桨榖;

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

    ◆ 起落架:前三点、双轮、不可收放式起落架,保证起降平稳、安全可靠。

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

    ◆ 航电系统:应用ARINC429和RS422数据总线为主要数据传输方式,并通过综合显示系统实现综合控制和显示。关键的设备及功能采用余度设计,以提高系统的可靠性。

    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.

    ◆ 操纵机构:双套并列式布置,正、副驾驶联动

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

    ◆ 飞行控制系统:采用双余度数字式KJ-15A自动驾驶仪,实现四轴控制

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

    ◆ 灭火系统:能在同一动力舱内可连续进行两次灭火,也可在两个不同的动力舱内分别进行一次灭火;

    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.

    ◆ 防护装置:尾梁后下段布置有尾撑,防止在着陆时尾梁和尾桨叶意外撞击地面;

    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.

    ◆ 座舱布局:2名飞行员+18名乘客;

    Cabin layout: 2 pilots + 18 passengers;
    基本性能:Performance
    飞行性能:
    Flight Performance
    最大速度/巡航速度                  244 Km/Hr
    Max Speed/Max Cruise Speed   244 Km/Hr
    最大续航时间                       5.3Hrs
    Max Endurance                       5.3Hrs
    最大飞行高度                      6000m
    Max. Flight Altitude                6000m
    有/无地效悬停升限             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
    最大起飞重量             13000 Kg
    Max Take-off Weight        13000 Kg
    有效载重                 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
    最大地面起动高度  4500m,
    Max. Ground Starting Altitude: 4500m
    最大空中起动高度   6000m,
    Max. Aerial Starting Altitude: 6000m
    起飞功率  1447kw 
    Take-off Power: 1447Kw
    最大连续功率  1249kw
    Max. Continuous Power: 1249Kw

    燃油:Fuel
    有效总的燃油量:3800 Kg
    Total Effective Fuel Volume:  3800Kg
    20min可用余油量:390 Kg;
    Useful Reserve for 20min: 390Kg;
    标准油箱容量     4740L
    Standard Tank Volume: 4740L
    外形尺寸
    External Dimensions
    全长(旋翼旋转)                           23.045 m
    Overall Length (Rotors turning)         23.045 m
    全高(空重,尾桨旋转)                    6.741 m
    Overall Height (empty weight, tail rotor turning)
    6.741 m
    全宽(旋翼转动时)                 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
    产品优势:
    Product Advantage:

    载重量大,吊挂能力强

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

    ◆ 出色的航程和续航能力

    Excellent range and endurance capability;

    ◆ 大量使用复合材料,延长使用寿命

    Composite material is widely used to extend service life cycle

    ◆ 综合显示控制系统为飞行员提供飞行状态信息、导航信息、机电管理系统的备份显示及其它机载信息的综合显示,提高人机工效。

    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,安全可靠

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

    ◆ KJ-15A自动驾驶仪,减轻驾驶负担

    KJ-15 autopilot reduces the workload of the pilot.

    ◆ 抗坠毁座椅、告警系统使直升机更安全、可靠

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

    ◆ 机外照明系统提供直升机的航向和方位信息以及防撞告警信号,并在着陆时照亮周围场地,使飞行员能清晰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,座椅柔软,舒适性好

    Spacious cabin and soft seats with excellent comfort;

    ◆ 使用成本低,便于维护

    Low operation cost and easy of maintenance,

    ◆ 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 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