民機系列
  • AC311直升機簡介 
    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”、“環保性”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 “green”. 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 
    Comply 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 

    ◆ 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;

    ◆ 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;

    ◆ 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;

    ◆ 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;

    ◆ 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;

    ◆ 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);

    ◆ 左側艙門采用滑軌式設計;

    Left door adopts sliding rail-type design;

    ◆ 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 駕駛員+3乘員 
    2 pilots+3 passengers
    2駕駛員+4乘員 
    2 pilots+4 passengers
    1駕駛員+5乘員  
    1 pilot+5 passengers
    1名飛行員+1副擔架和2位醫務人員 
    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.

    基本性能: 
    Performance:

    飛行性能 
    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公里/小時(Km/h) 
    236Km/h

    最大斜爬升率 
    Maximum inclined climb rate

    8.3米/秒(m/s) 
    8.3m/s

    無地效靜升限 
    OGE (out of ground effect) Hovering

    2250米(m) 
    2250m

    有地效靜升限 
    IGE (in ground effect)  Hovering

    2950米(m) 
    2950m

    最大續航時間   
    Maximum endurance

    4.0h
    4.0h

    最大航程 
    Max. Range

    630Km
    630Km

    重量 
    Weight

    最大起飛重量 
    Max Take-off Weight

    2200千克(kg) 
    2200kg

    動力 
    Powerplant

    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

    最大連續功率 
    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 

    總長 
    Overall length

    13.083m
    13.083m

    總高(至槳榖頂點) 
    Overall height (to the top of main rotor hub)

    3.299m
    3.299m

    機身寬 
    Fuselage width

    1.828m
    1.828m

    旋翼直徑 
    Rotor diameter

    10.69m
    10.69m

    尾槳直徑 
    Tail rotor diameter

    1.86m
    1.86m

    產品優勢: 
    Product Advantages:
    技術優點 
    Technical advantages

    ◆ 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; 

    ◆ 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;

    ◆ 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;

    ◆ 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;

    ◆ 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;

    ◆ 水滴形氣動外形機身和總體布局,線條流暢,外觀優美;

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

    ◆ 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;

    ◆ 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;

    ◆ 維護簡單,使用成本低;

    Easy maintenance and low operation cost;

    ◆ 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.


  • AC311A直升機簡介 
    Presentation of AC311A Helicopter 
      

      
    AC311A直升機是一款2噸級單發、6座單旋翼、帶尾槳式高原輕型直升機,該機采用單/雙駕駛配置及高橇式起落架,裝有一臺強勁的法國透博梅卡公司ARRIEL 2B1A發動機,配置國產高度集成化綜合航空電子系統,加裝數字化增穩系統及語音告警系統,并預留了多種選裝任務設備接口,具備很強的任務拓展能力。同時,整機大量使用復合材料,并提供多種選擇的精致內飾和座椅。應用廣泛,可滿足我國大部分地區的使用要求,尤其是高原區域,作業范圍可覆蓋85%的國土面積。 
    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.

    ◆加裝一臺進口大功率發動機,提高整機高原性能和環境適應性; 
    An imported powerful engine is equipped to improve the plateau performance and environment adaptability of the whole aircraft; 
    ◆安裝的一臺大功率發動機,功率貯備大,高溫高原性能佳,機動性能好,具有很好的任務效能和高原環境適應性; 
    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進國產化綜合航電系統,降低飛行負擔; 
    Advanced, highly integrated domestic avionics system is adopted to reduce pilots' burden. 
    ◆采用結構預留設計,可加裝電動絞車、醫療救護單元(ICU)、揚聲器、搜索燈、圖像傳輸系統、應急漂浮系統、氧氣系統、農林噴灑系統等多種任務設備,具有良好的任務和功能擴展性; 
    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.      
    ◆國產化程度高,降低對國外技術依賴性,提高加改裝自主性和開放性; 
    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. 
    ◆整體技術成熟、先進,可靠性高,維護和保障簡單,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.

     

    技術特點 
    Technical features 

    ◆ 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;

    ◆ 發動機:一臺透博梅卡ARRIEL 2B1A高性能發動機;

    Engine: a Turbomeca engine ARRIEL 2B1A with excellent performance

    1. 發動機采用雙通道電調(EECU)加電動應急備份控制系統; The Engine adopts dual channel EEC (EECU) plus electric emergency back-up control system;

    2. 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;

    ◆ 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;

    ◆ 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;

    1. 電氣系統:裝有1臺6kw的起動發電機和1塊24V/15Ah的蓄電池應急電源; Electric system: a 6 kw starter generator and one 24 V/15Ah emergency supply for accumulator are additionally installed;

    2. 航電系統: 2臺多功能顯示控制單元和1臺發動機參數顯示單元,綜合集成顯示飛行任務過程中所需的航向、姿態、速度、高度、數字地圖、發動機參數等基本飛行信息,并提供通信、導航、告警等各項功能;

    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. 導航系統采用捷聯慣導,可實現在無GPS信號條件下的全自主導航。The navigation system adopts the strapdown inertial navigation, which can realize the totally self-contained navigation without the GPS signal. 

    2. 采用雙駕駛操縱系統、雙儀表配置;It adopts the dual-pilot control system and the dual instrument arrangement;

    3. 左側艙門采用滑軌式設計;

    4. Left door adopts sliding rail-type design;

    基本性能 
    Basic performance


    飛行性能(ISA,H=0m,最大起飛重量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(狀態8.2)
    8.3m/s(狀態8.2)

    無地效靜升限 
    OGE (out of ground effect) Ceiling

    3200 m(狀態3400) 
    3200m(狀態3400)

    有地效靜升限 
    IGE (in ground effect) Ceiling
    使用升限 
    Service Ceiling

    3900 m(狀態4200) 
    3900m(狀態4200) 
    6000m(狀態5100) 
    6000m(狀態5100)

    最大續航時間  
    Maximum endurance 
    最大航程 
    Max Range

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



    重量 
    Weight


    最大起飛重量 
    Max Take-off Weight

    2250kg 
    2250kg

    動力 
    Powerplant


    1臺法國透博梅卡公司ARRIEL 2B1A發動機 
    One set of engine ARRIEL 2B1A supplied by French Turbomeca Company


    最大連續功率 
    Max Continuous Power
    最大起飛功率 
    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 


    總長 
    Overall length

    13.083m 
    13.083m

    總高(至槳榖頂點) 
    Overall height (to the top of main rotor hub)

    3.299m 
    3.299m

    機身寬 
    Fuselage width

    1.828m 
    1.828m

    旋翼直徑 
    Rotor diameter

    10.69m 
    10.69m

    尾槳直徑 
    Tail rotor diameter

    1.86m 
    1.86m

    產品優勢: 
    Product Advantages:

    ◆ 
    直升機基礎平臺成熟、先進、可靠,保證了整機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. 

    ◆ 任務改裝靈活多樣,可根據不同需要改裝成警用型/通航作業型/教練型/醫療救援型/VIP型及運輸型等,并可且于軍用,加裝多種武器及偵察設備。

    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.

    ◆ 安裝一臺大功率發動機,功率貯備大,高溫高原性能好,機動性能好,具有很好的整機任務效能和高原環境適應性;

     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進綜合航電系統,降低飛行負擔;

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

    ◆ 增加預留接口,可選裝或增加多種任務設備,提高不同任務環境適應性;

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

    ◆ 采用開闊大玻璃設計的機頭,視野開闊;

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

    1. 先進的復合材料機身和全復合材料旋翼系統,重量輕,使用壽命長; Advanced composite fuselage and all-composite rotor system, light in weight and long in service life.

    2. 優秀的飛行性能和飛行品質,優良的可控制性和機動性;

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

    ◆ 具有很高的開放性,可根據用戶的要求進行加改裝;

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

    ◆ 整體技術成熟、先進,可靠性高,維護和保障簡單,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直升機簡介
    Presentation of AC313 Helicopter


    AC313直升機是一款13噸級大型三發民用直升機。該機采用輪式起落架和雙駕駛體制,裝三臺PT6B-67A發動機,配有高度集成的航電系統。依據CCAR-29R1規定中適用的適航要求,采用結構預留、空間預留設計準則,進行客貨兩用基本型研制,可按照晝夜目視飛行規則(VFR)和儀表飛行規則(IFR),在陸地和無結冰條件下進行目視和儀表飛行,可滿足高溫、高寒氣候和高原等復雜地區對直升機的使用要求。 
    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.

    適航規范: 
    Airworthiness Standards 
    符合CCAR29部的要求。 
    Comply with CCAR 29

    運行類型: 
    Operation type

    可晝夜目視飛行。 
    Day and Night VFR
    儀表飛行規則 
    Day and Night IFR

     

    基本使用環境 
    Basic operation environment
    飛行高度:海平面~6000 m 
    Flight altitude: sea level ~ 6000m
    使用環境溫度:-40℃~ISA+35℃
    Operation ambient temperature: -40℃~ISA+35℃ 
    應用領域: 
    Application fields:
    AC313直升機可廣泛的應用于搜索救援、護林滅火、客貨運輸、醫療救護、吊掛作業、海洋考察等領域。 
    AC313 helicopter can be widely used in search and rescue, forest firefighting, passenger and cargo transportation, external sling, maritime survey.

    技術特點: 
    Technical Features
    ◆ 構型:常規單旋翼帶尾槳式;

    Configuration: conventional single rotor with tail rotor;

    ◆ 動力裝置:3臺PT6B-67A發動機,1臺輔助動力裝置(APU);

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

    ◆ 旋翼: 6片復合材料槳葉,鈦合金球柔性槳轂;

    Rotor: 6 composite blades with titanium alloy spheriflex hub 

    ◆ 尾槳:5片復合材料尾槳葉,鈦合金球柔性結構型式尾槳榖;

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

    ◆ 起落架:前三點、雙輪、不可收放式起落架,保證起降平穩、安全可靠。

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

    ◆ 航電系統:應用ARINC429和RS422數據總線為主要數據傳輸方式,并通過綜合顯示系統實現綜合控制和顯示。關鍵的設備及功能采用余度設計,以提高系統的可靠性。

    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. 

    ◆ 操縱機構:雙套并列式布置,正、副駕駛聯動

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

    ◆ 飛行控制系統:采用雙余度數字式KJ-15A自動駕駛儀,實現四軸控制

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

    ◆ 滅火系統:能在同一動力艙內可連續進行兩次滅火,也可在兩個不同的動力艙內分別進行一次滅火;

    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.

    ◆ 防護裝置:尾梁后下段布置有尾撐,防止在著陸時尾梁和尾槳葉意外撞擊地面;

    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. 

    ◆ 座艙布局:2名飛行員+18名乘客;

    Cabin layout: 2 pilots + 18 passengers;
    基本性能:Performance 
    飛行性能: 
    Flight Performance
    最大速度/巡航速度                  244 Km/Hr
    Max Speed/Max Cruise Speed   244 Km/Hr
    最大續航時間                       5.3Hrs
    Max Endurance                       5.3Hrs
    最大飛行高度                      6000m
    Max. Flight Altitude                6000m
    有/無地效懸停升限             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 
    最大起飛重量             13000 Kg
    Max Take-off Weight        13000 Kg
    有效載重                 4000 Kg
    Max Payload              4000 Kg
    最大吊運重量             5000Kg
    Max. Sling Load           5000Kg

    動力:Powerplant 
    三臺加普惠PT6B-67A發動機, 
    3 P&WC PT6B-67A engines
    最大地面起動高度  4500m, 
    Max. Ground Starting Altitude: 4500m
    最大空中起動高度   6000m, 
    Max. Aerial Starting Altitude: 6000m
    起飛功率  1447kw  
    Take-off Power: 1447Kw
    最大連續功率  1249kw 
    Max. Continuous Power: 1249Kw

    燃油:Fuel
    有效總的燃油量:3800 Kg 
    Total Effective Fuel Volume:  3800Kg
    20min可用余油量:390 Kg; 
    Useful Reserve for 20min: 390Kg;
    標準油箱容量     4740L 
    Standard Tank Volume: 4740L 
    外形尺寸 
    External Dimensions
    全長(旋翼旋轉)                           23.045 m
    Overall Length (Rotors turning)         23.045 m
    全高(空重,尾槳旋轉)                    6.741 m
    Overall Height (empty weight, tail rotor turning)
    6.741 m
    全寬(旋翼轉動時)                 18.900 m
    Width (Rotors turning)                 18.900 m
    旋翼直徑                           18.900 m
    Rotor Diameter                       18.900 m
    尾槳直徑                           4.000 m
    Tail Rotor Diameter                  4.000 m 
    產品優勢: 
    Product Advantage:

    ◆ 
    載重量大,吊掛能力強

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

    ◆ 出色的航程和續航能力

    Excellent range and endurance capability;

    ◆ 大量使用復合材料,延長使用壽命

    Composite material is widely used to extend service life cycle 

    ◆ 綜合顯示控制系統為飛行員提供飛行狀態信息、導航信息、機電管理系統的備份顯示及其它機載信息的綜合顯示,提高人機工效。

    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、副駕駛聯動,安全可靠

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

    ◆ KJ-15A自動駕駛儀,減輕駕駛負擔

    KJ-15 autopilot reduces the workload of the pilot.

    ◆ 抗墜毀座椅、告警系統使直升機更安全、可靠

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

    ◆ 機外照明系統提供直升機的航向和方位信息以及防撞告警信號,并在著陸時照亮周圍場地,使飛行員能清晰目視直升機著陸時的位置和高度。

    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. 

    ◆ 機艙容量大,座椅柔軟,舒適性好

    Spacious cabin and soft seats with excellent comfort;

    ◆ 使用成本低,便于維護

    Low operation cost and easy of maintenance, 

    ◆ 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

     

  • AC311A直升機簡介
    Presentation of AC311A Helicopter
    ??

    ?
    AC311A直升機是一款2噸級單發、6座單旋翼、帶尾槳式高原輕型直升機,該機采用單/雙駕駛配置及高橇式起落架,裝有一臺強勁的法國透博梅卡公司ARRIEL 2B1A發動機,配置國產高度集成化綜合航空電子系統,加裝數字化增穩系統及語音告警系統,并預留了多種選裝任務設備接口,具備很強的任務拓展能力。同時,整機大量使用復合材料,并提供多種選擇的精致內飾和座椅。應用廣泛,可滿足我國大部分地區的使用要求,尤其是高原區域,作業范圍可覆蓋85%的國土面積。
    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.

    ◆加裝一臺進口大功率發動機,提高整機高原性能和環境適應性;
    An imported powerful engine is equipped to improve the plateau performance and environment adaptability of the whole aircraft;
    ◆安裝的一臺大功率發動機,功率貯備大,高溫高原性能佳,機動性能好,具有很好的任務效能和高原環境適應性;
    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進國產化綜合航電系統,降低飛行負擔;
    Advanced, highly integrated domestic avionics system is adopted to reduce pilots' burden.
    ◆采用結構預留設計,可加裝電動絞車、醫療救護單元(ICU)、揚聲器、搜索燈、圖像傳輸系統、應急漂浮系統、氧氣系統、農林噴灑系統等多種任務設備,具有良好的任務和功能擴展性;
    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.?????
    ◆國產化程度高,降低對國外技術依賴性,提高加改裝自主性和開放性;
    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.
    ◆整體技術成熟、先進,可靠性高,維護和保障簡單,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.

     

    技術特點
    Technical features

    ◆ 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;

    ◆ 發動機:一臺透博梅卡ARRIEL 2B1A高性能發動機;

    Engine: a Turbomeca engine ARRIEL 2B1A with excellent performance

    1. 發動機采用雙通道電調(EECU)加電動應急備份控制系統; The Engine adopts dual channel EEC (EECU) plus electric emergency back-up control system;
    2. 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;

    ◆ 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;

    ◆ 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;

    1. 電氣系統:裝有1臺6kw的起動發電機和1塊24V/15Ah的蓄電池應急電源; Electric system: a 6 kw starter generator and one 24 V/15Ah emergency supply for accumulator are additionally installed;
    2. 航電系統: 2臺多功能顯示控制單元和1臺發動機參數顯示單元,綜合集成顯示飛行任務過程中所需的航向、姿態、速度、高度、數字地圖、發動機參數等基本飛行信息,并提供通信、導航、告警等各項功能;

    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. 導航系統采用捷聯慣導,可實現在無GPS信號條件下的全自主導航。The navigation system adopts the strapdown inertial navigation, which can realize the totally self-contained navigation without the GPS signal.?
    2. 采用雙駕駛操縱系統、雙儀表配置;It adopts the dual-pilot control system and the dual instrument arrangement;
    3. 左側艙門采用滑軌式設計;
    4. Left door adopts sliding rail-type design;

    基本性能
    Basic performance

     

    飛行性能(ISA,H=0m,最大起飛重量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(狀態8.2)
    8.3m/s(狀態8.2)

    無地效靜升限
    OGE (out of ground effect) Ceiling

    3200 m(狀態3400)
    3200m(狀態3400)

    有地效靜升限
    IGE (in ground effect) Ceiling
    使用升限
    Service Ceiling

    3900 m(狀態4200)
    3900m(狀態4200)
    6000m(狀態5100)
    6000m(狀態5100)

    最大續航時間?
    Maximum endurance
    最大航程
    Max Range

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

     

     

    重量
    Weight

     

    最大起飛重量
    Max Take-off Weight

    2250kg
    2250kg

    動力
    Powerplant

     

    1臺法國透博梅卡公司ARRIEL 2B1A發動機
    One set of engine ARRIEL 2B1A supplied by French Turbomeca Company

     

    最大連續功率
    Max Continuous Power
    最大起飛功率
    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?

     

    總長
    Overall length

    13.083m
    13.083m

    總高(至槳榖頂點)
    Overall height (to the top of main rotor hub)

    3.299m
    3.299m

    機身寬
    Fuselage width

    1.828m
    1.828m

    旋翼直徑
    Rotor diameter

    10.69m
    10.69m

    尾槳直徑
    Tail rotor diameter

    1.86m
    1.86m

    產品優勢:
    Product Advantages:

    直升機基礎平臺成熟、先進、可靠,保證了整機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.

    ◆ 任務改裝靈活多樣,可根據不同需要改裝成警用型/通航作業型/教練型/醫療救援型/VIP型及運輸型等,并可且于軍用,加裝多種武器及偵察設備。

    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.

    ◆ 安裝一臺大功率發動機,功率貯備大,高溫高原性能好,機動性能好,具有很好的整機任務效能和高原環境適應性;

    ?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進綜合航電系統,降低飛行負擔;

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

    ◆ 增加預留接口,可選裝或增加多種任務設備,提高不同任務環境適應性;

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

    ◆ 采用開闊大玻璃設計的機頭,視野開闊;

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

    1. 先進的復合材料機身和全復合材料旋翼系統,重量輕,使用壽命長; Advanced composite fuselage and all-composite rotor system, light in weight and long in service life.
    2. 優秀的飛行性能和飛行品質,優良的可控制性和機動性;

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

    ◆ 具有很高的開放性,可根據用戶的要求進行加改裝;

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

    ◆ 整體技術成熟、先進,可靠性高,維護和保障簡單,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直升機簡介
    Presentation of AC313 Helicopter


    AC313直升機是一款13噸級大型三發民用直升機。該機采用輪式起落架和雙駕駛體制,裝三臺PT6B-67A發動機,配有高度集成的航電系統。依據CCAR-29R1規定中適用的適航要求,采用結構預留、空間預留設計準則,進行客貨兩用基本型研制,可按照晝夜目視飛行規則(VFR)和儀表飛行規則(IFR),在陸地和無結冰條件下進行目視和儀表飛行,可滿足高溫、高寒氣候和高原等復雜地區對直升機的使用要求。
    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.

    適航規范:
    Airworthiness Standards
    符合CCAR29部的要求。
    Comply with CCAR 29

    運行類型:
    Operation type

    可晝夜目視飛行。
    Day and Night VFR
    儀表飛行規則
    Day and Night IFR

     

    基本使用環境
    Basic operation environment
    飛行高度:海平面~6000 m
    Flight altitude: sea level ~ 6000m
    使用環境溫度:-40℃~ISA+35℃
    Operation ambient temperature: -40℃~ISA+35℃
    應用領域:
    Application fields:
    AC313直升機可廣泛的應用于搜索救援、護林滅火、客貨運輸、醫療救護、吊掛作業、海洋考察等領域。
    AC313 helicopter can be widely used in search and rescue, forest firefighting, passenger and cargo transportation, external sling, maritime survey.

    技術特點:
    Technical Features
    ◆ 構型:常規單旋翼帶尾槳式;

    Configuration: conventional single rotor with tail rotor;

    ◆ 動力裝置:3臺PT6B-67A發動機,1臺輔助動力裝置(APU);

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

    ◆ 旋翼: 6片復合材料槳葉,鈦合金球柔性槳轂;

    Rotor: 6 composite blades with titanium alloy spheriflex hub

    ◆ 尾槳:5片復合材料尾槳葉,鈦合金球柔性結構型式尾槳榖;

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

    ◆ 起落架:前三點、雙輪、不可收放式起落架,保證起降平穩、安全可靠。

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

    ◆ 航電系統:應用ARINC429和RS422數據總線為主要數據傳輸方式,并通過綜合顯示系統實現綜合控制和顯示。關鍵的設備及功能采用余度設計,以提高系統的可靠性。

    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.

    ◆ 操縱機構:雙套并列式布置,正、副駕駛聯動

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

    ◆ 飛行控制系統:采用雙余度數字式KJ-15A自動駕駛儀,實現四軸控制

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

    ◆ 滅火系統:能在同一動力艙內可連續進行兩次滅火,也可在兩個不同的動力艙內分別進行一次滅火;

    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.

    ◆ 防護裝置:尾梁后下段布置有尾撐,防止在著陸時尾梁和尾槳葉意外撞擊地面;

    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.

    ◆ 座艙布局:2名飛行員+18名乘客;

    Cabin layout: 2 pilots + 18 passengers;
    基本性能:Performance
    飛行性能:
    Flight Performance
    最大速度/巡航速度????????????????? 244 Km/Hr
    Max Speed/Max Cruise Speed?? 244 Km/Hr
    最大續航時間?????????????????????? 5.3Hrs
    Max Endurance???????????????????? ??5.3Hrs
    最大飛行高度??????????????????????6000m
    Max. Flight Altitude????????????????6000m
    有/無地效懸停升限 ????????????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
    最大起飛重量???????????? 13000 Kg
    Max Take-off Weight???? ???13000 Kg
    有效載重???????????????? 4000 Kg
    Max Payload????????????? 4000 Kg
    最大吊運重量???????????? 5000Kg
    Max. Sling Load?????????? 5000Kg

    動力:Powerplant
    三臺加普惠PT6B-67A發動機,
    3 P&WC PT6B-67A engines
    最大地面起動高度? 4500m,
    Max. Ground Starting Altitude: 4500m
    最大空中起動高度?? 6000m,
    Max. Aerial Starting Altitude: 6000m
    起飛功率? 1447kw?
    Take-off Power: 1447Kw
    最大連續功率? 1249kw
    Max. Continuous Power: 1249Kw

    燃油:Fuel
    有效總的燃油量:3800 Kg
    Total Effective Fuel Volume:? 3800Kg
    20min可用余油量:390 Kg;
    Useful Reserve for 20min: 390Kg;
    標準油箱容量???? 4740L
    Standard Tank Volume: 4740L
    外形尺寸
    External Dimensions
    全長(旋翼旋轉)???????????? ???????? ?? ??23.045 m
    Overall Length (Rotors turning)???????? 23.045 m
    全高(空重,尾槳旋轉) ???????????? ??????6.741 m
    Overall Height (empty weight, tail rotor turning)
    6.741 m
    全寬(旋翼轉動時)???????????????? 18.900 m
    Width (Rotors turning)???????????????? 18.900 m
    旋翼直徑?????????????????????????? 18.900 m
    Rotor Diameter?????????????????????? 18.900 m
    尾槳直徑?????????????????????????? 4.000 m
    Tail Rotor Diameter???? ?????????????4.000 m
    產品優勢:
    Product Advantage:

    載重量大,吊掛能力強

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

    ◆ 出色的航程和續航能力

    Excellent range and endurance capability;

    ◆ 大量使用復合材料,延長使用壽命

    Composite material is widely used to extend service life cycle

    ◆ 綜合顯示控制系統為飛行員提供飛行狀態信息、導航信息、機電管理系統的備份顯示及其它機載信息的綜合顯示,提高人機工效。

    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、副駕駛聯動,安全可靠

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

    ◆ KJ-15A自動駕駛儀,減輕駕駛負擔

    KJ-15 autopilot reduces the workload of the pilot.

    ◆ 抗墜毀座椅、告警系統使直升機更安全、可靠

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

    ◆ 機外照明系統提供直升機的航向和方位信息以及防撞告警信號,并在著陸時照亮周圍場地,使飛行員能清晰目視直升機著陸時的位置和高度。

    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.

    ◆ 機艙容量大,座椅柔軟,舒適性好

    Spacious cabin and soft seats with excellent comfort;

    ◆ 使用成本低,便于維護

    Low operation cost and easy of maintenance,

    ◆ 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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