軍(jun)機系列
  














  • 直-8型機簡介

    直8型機是亞洲最(zui)大噸位的(de)多用途直升機,也(ye)是我國(guo)交付部隊(dui)使(shi)用的(de)第一種直升機。該機采(cai)用單旋翼帶尾槳常(chang)規氣動布局,配裝三台發動機,裝有前(qian)三點式兩棲起(qi)落架。該機具有安全性(xing)好、三防能力強和功能全等優勢(shi),可(ke)廣泛適shi)糜誥jun)用、通用航空(kong)和準軍(jun)事領(ling)域的(de)需求,可(ke)執行武器裝備/人員(yuan)/貨qiao)鐫聳洹? 址闌稹?老站仍幀 馱撕槳唷 攪liao)救護、搜索救援、物資運輸、地(di)質勘探、地(di)理測繪、建築施(shi)工、海洋考察(cha)、旅游觀光(guang)、公務飛行和反恐維穩(wen)等任務。


  • 直-10型機簡介

    直-10型機是我國(guo)自主(zhu)研(yan)制(zhi)的(de)第一種專用武裝直升機,該機采(cai)用單旋翼帶尾槳構型ting)  澩chuan)列式駕駛(shi)艙、後三點式起(qi)落架布局。具有優良(liang)的(de)飛行性(xing)能、較(jiao)高的(de)戰場生存力、多機空(kong)地(di)信息化協同、連續、快(kuai)速攻(gong)擊多目標能力,可(ke)在(zai)全天候、復雜戰場環境(jing)和野外保障條件(jian)下遂行多種作戰任務。綜(zong)合作戰效能與國(guo)外現役先進武裝直升機相當。

  • 直-11型機簡介

    直11型直升機是由航空(kong)工業昌(chang)飛和中國(guo)直升機設計研(yan)究所共同研(yan)制(zhi)生產的(de)多用途輕(qing)型直升機,是我國(guo)自行設計研(yan)制(zhi)的(de)第一個具有自主(zhu)知識產權的(de)直升機機種,也(ye)是部隊(dui)服役出勤(qin)率最(zui)高的(de)直升機機種。該機已取(qu)得中國(guo)民航總局頒發的(de)型號合格證(zheng)和生產許(xu)可(ke)證(zheng),可(ke)廣泛用于空(kong)中巡邏、空(kong)中指揮、通訊(xun)聯絡、公務運輸、交通監(jian)理、消(xiao)防滅火、緊急救援、緝私緝毒、防爆反恐、火力支(zhi)援和邊境(jing)巡邏等領(ling)域。

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    直-11WB型機簡介

     

           直11WB“”偵察(cha)攻(gong)擊直升機是qie)豢罹哂泄guo)際先進水平的(de)2噸級輕(qing)型直升機,該機采(cai)用全數字(zi)化設計和制(zhi)造技術,不僅配備了紅(hong)外激光(guang)干擾吊(diao)艙,而且(qie)機槍、火箭發射器、反坦克導彈等應(ying)有盡有,能夠執行對(dui)地(di)攻(gong)擊、戰場偵察(cha)、武裝反恐等多種任務,是“信息融合、網絡中心戰、空(kong)地(di)一體戰”的(de)攻(gong)擊偵察(cha)作戰利器。

            

    一張圖了解直11WB ?


    直11WB性(xing)能展gu)臼shi)頻 ?

           

     

     

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

    ?
    AC311A直升機是qie)豢噸級單發、6座單旋翼、帶尾槳式高原輕(qing)型直升機,該機采(cai)用單/雙(shuang)駕駛(shi)配置及高橇式起(qi)落架,裝有xing)惶ㄇ烤 de)法國(guo)透博梅卡(ka)公司ARRIEL 2B1A發動機,配置國(guo)產高度ran) cheng)化綜(zong)合航空(kong)電子系統chang) 幼笆zi)化增穩(wen)系統及語音(yin)告警系統chang)  ?裊碩嘀盅 叭撾襠璞附涌冢 弒負(fu)芮康de)任務拓展能力。同時,整(zheng)機大量使(shi)用復合材料,並提供(gong)多種選擇的(de)精致內飾和座椅。應(ying)用廣泛,可(ke)滿足我國(guo)大部分地(di)區(qu)的(de)使(shi)用要(yao)求,尤其是高原區(qu)域,作業範圍可(ke)覆蓋85%的(de)國(guo)土(tu)面(mian)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.

    ◆加裝一台進口大功率發動機,提高整(zheng)機高原性(xing)能和環境(jing)適shi)ying)性(xing);
    An imported powerful engine is equipped to improve the plateau performance and environment adaptability of the whole aircraft;
    ◆安裝的(de)一台大功率發動機,功率貯(zhu)備大,高溫高原性(xing)能佳,機動性(xing)能好,具有很好的(de)任務效能和高原環境(jing)適shi)ying)性(xing);
    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(cai)用高度ran) cheng)化的(de)先進國(guo)產化綜(zong)合航電系統chang) 檔頭尚懈fu)擔;
    Advanced, highly integrated domestic avionics system is adopted to reduce pilots' burden.
    ◆采(cai)用結構預留設計,可(ke)加裝電動絞車、醫療(liao)救護單元(ICU)、揚聲器、搜索燈、圖像傳輸系統、應(ying)急漂浮系統、氧氣系統、農林噴灑(sa)系統等多種任務設備,具有良(liang)好的(de)任務和功能擴(kuo)展性(xing);
    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(guo)產化程度高,降低對(dui)國(guo)外技術依賴(lai)性(xing),提高加改裝自主(zhu)性(xing)和開放性(xing);
    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(zheng)體技術成(cheng)熟、先進,可(ke)靠性(xing)高,維護和保障簡單,故(gu)障率低ting)
    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ting)旱?澩步笆匠chang)規布局輕(qing)型直升機;

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

    ◆ 發動機︰一台透博梅卡(ka)ARRIEL 2B1A高性(xing)能發動機;

    Engine: a Turbomeca engine ARRIEL 2B1A with excellent performance

    1. 發動機采(cai)用雙(shuang)通道(dao)lai)緄鰨ECU)加電動應(ying)急備份控(kong)制(zhi)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(zhu)槳葉,長壽(shou)命星型柔(rou)性(xing)槳?b;

    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(cai)用蹺(qiao)蹺(qiao)板(ban)結構形式;

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

    ◆ 起(qi)落架︰采(cai)用加拿(na)大DART公司帶阻尼器的(de)滑橇和板(ban)彈簧尾撐型式的(de)高姿起(qi)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chang)鶴壩台6kw的(de)起(qi)動發電機和1塊24V/15Ah的(de)蓄(xu)電池應(ying)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chang)2台多功能顯示控(kong)制(zhi)單元和1台發動機參數顯示單元,綜(zong)合集(ji)成(cheng)顯示飛行任務過(guo)程中所需的(de)航jiao)頡 頌 ?俁取(qu) 叨取(qu)?zi)地(di)圖、發動機參數等基本飛行信息,並提供(gong)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jiao)低巢cai)用捷聯慣導,可(ke)實現在(zai)無GPS信號條件(jian)下的(de)全自主(zhu)導航。The navigation system adopts the strapdown inertial navigation, which can realize the totally self-contained navigation without the GPS signal.?
    2. 采(cai)用雙(shuang)駕駛(shi)操縱(zong)系統、雙(shuang)儀(yi)表配置;It adopts the dual-pilot control system and the dual instrument arrangement;
    3. 左側(ce)艙門采(cai)用滑軌式設計;
    4. Left door adopts sliding rail-type design;

    基本性(xing)能
    Basic performance

     

    飛行性(xing)能(ISA,H=0m,最(zui)大起(qi)飛重量2250KG)
    Flight performance (ISA, H=0m, maximum take-off weight 2250 KG)

     

    最(zui)大巡航速度
    Maximum cruising speed

    240 Km/h
    240Km/h

    最(zui)大斜(xie)爬升率
    Maximum inclined climb rate

    8.3 m/s(狀態8.2)
    8.3m/s(狀態8.2)

    無地(di)效靜(jing)cai)xian)
    OGE (out of ground effect) Ceiling

    3200 m(狀態3400)
    3200m(狀態3400)

    有地(di)效靜(jing)cai)xian)
    IGE (in ground effect) Ceiling
    使(shi)用升限(xian)
    Service Ceiling

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

    最(zui)大續航時間?
    Maximum endurance
    最(zui)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(zui)大起(qi)飛重量
    Max Take-off Weight

    2250kg
    2250kg

    動力
    Powerplant

     

    1台法國(guo)透博梅卡(ka)公司ARRIEL 2B1A發動機
    One set of engine ARRIEL 2B1A supplied by French Turbomeca Company

     

    最(zui)大連續功率
    Max Continuous Power
    最(zui)大起(qi)飛功率
    Max Take-off Power

    543Kw
    543Kw
    632Kw
    632Kw

    燃(ran)油
    Fuel

     

    最(zui)大燃(ran)油重量?
    Max Fuel Weight ?

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

    外形尺寸(cun)
    External Dimensions?

     

    總長
    Overall length

    13.083m
    13.083m

    總高(至槳?b頂(ding)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(shi)︰
    Product Advantages:

    直升機基礎(chu)平jiao) cheng)熟、先進、可(ke)靠,保證(zheng)了整(zheng)機良(liang)好的(de)出勤(qin)率和完(wan)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(huo)多樣,可(ke)根據不同需要(yao)改裝成(cheng)警用型/通航作業型/教(jiao)練型/醫療(liao)救援型/VIP型及運輸型等,並可(ke)且(qie)于軍(jun)用,加裝多種武器及偵察(cha)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.

    ◆ 安裝一台大功率發動機,功率貯(zhu)備大,高溫高原性(xing)能好,機動性(xing)能好,具有很好的(de)整(zheng)機任務效能和高原環境(jing)適shi)ying)性(xing);

    ?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(cai)用高度ran) cheng)化的(de)先進綜(zong)合航電系統chang) 檔頭尚懈fu)擔;

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

    ◆ 增加預留接口,可(ke)選裝或增加多種任務設備,提高不同任務環境(jing)適shi)ying)性(xing);

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

    ◆ 采(cai)用開闊大玻(bo)璃(li)設計的(de)機頭,視(shi)野開闊;

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

    1. 先進的(de)復合材料機身和全復合材料旋翼系統chang) 亓殼qing),使(shi)用壽(shou)命長; Advanced composite fuselage and all-composite rotor system, light in weight and long in service life.
    2. 優秀的(de)飛行性(xing)能和飛行品質,優良(liang)的(de)可(ke)控(kong)制(zhi)性(xing)和機動性(xing);

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

    ◆ 具有很高的(de)開放性(xing),可(ke)根據用戶的(de)要(yao)求進行加改裝;

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

    ◆ 整(zheng)體技術成(cheng)熟、先進,可(ke)靠性(xing)高,維護和保障簡單,故(gu)障率低ting)

    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(wan)善的(de)用戶管理服務體系,可(ke)提供(gong)快(kuai)速響應(ying)、飛行和機務培訓、工程技術支(zhi)持等服務,支(zhi)持快(kuai)速的(de)維修(xiu)、備件(jian)支(zhi)援等qu)

    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qie)豢3噸級大型三發民用直升機。該機采(cai)用輪(lun)式起(qi)落架和雙(shuang)駕駛(shi)體制(zhi),裝三台PT6B-67A發動機,配有高度ran) cheng)的(de)航電系統。依據CCAR-29R1規定(ding)中適shi)玫de)適航要(yao)求,采(cai)用結構預留、空(kong)間預留設計準則,進行客貨兩用基本型研(yan)制(zhi),可(ke)按照晝夜目視(shi)飛行規則(VFR)和儀(yi)表飛行規則(IFR),在(zai)陸地(di)和無結冰條件(jian)下進行目視(shi)和儀(yi)表飛行,可(ke)滿足高溫、高寒氣候和高原等復雜地(di)區(qu)對(dui)直升機的(de)使(shi)用要(yao)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.

    適航規範︰
    Airworthiness Standards
    符合CCAR29部的(de)要(yao)求。
    Comply with CCAR 29

    運行類型ting)/strong>
    Operation type

    可(ke)晝夜目視(shi)飛行。
    Day and Night VFR
    儀(yi)表飛行規則
    Day and Night IFR

     

    基本使(shi)用環境(jing)
    Basic operation environment
    飛行高度︰海平面(mian)~6000 m
    Flight altitude: sea level ~ 6000m
    使(shi)用環境(jing)溫度︰-40℃~ISA+35℃
    Operation ambient temperature: -40℃~ISA+35℃
    應(ying)用領(ling)域︰
    Application fields:
    AC313直升機可(ke)廣泛的(de)應(ying)用于搜索救援、護林滅火、客貨運輸、醫療(liao)救護、吊(diao)掛作業、海洋考察(cha)等領(ling)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ting)撼chang)規單旋翼帶尾槳式;

    Configuration: conventional single rotor with tail rotor;

    ◆ 動力裝置︰3台PT6B-67A發動機,1台輔助動力裝置(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(jin)球柔(rou)性(xing)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(jin)球柔(rou)性(xing)結構型式尾槳?b;

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

    ◆ 起(qi)落架︰前(qian)三點、雙(shuang)輪(lun)、不可(ke)收放式起(qi)落架,保證(zheng)起(qi)降平穩(wen)qu) 踩 ke)靠。

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

    ◆ 航電系統chang)河ying)用ARINC429和RS422數據總線為主(zhu)要(yao)數據傳輸方式,並通過(guo)綜(zong)合顯示系統實現綜(zong)合控(kong)制(zhi)和顯示。關鍵的(de)設備及功能采(cai)用余(yu)度設計,以(yi)提高系統的(de)可(ke)靠性(xing)。

    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(zong)機構︰雙(shuang)套(tao)並列式布置,正、副駕駛(shi)聯動

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

    ◆ 飛行控(kong)制(zhi)系統chang)翰cai)用雙(shuang)余(yu)度數字(zi)式KJ-15A自動駕駛(shi)儀(yi),實現四(si)軸控(kong)制(zhi)

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

    ◆ 滅火系統chang)耗茉zai)同一動力艙內可(ke)連續進行兩次(ci)滅火,也(ye)可(ke)在(zai)兩個不同的(de)動力艙內分別(bie)進行xing)淮ci)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︰尾梁後下段布置有尾撐,防止(zhi)在(zai)著陸時尾梁和尾槳葉意外撞擊地(di)面(mian);

    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xing)yuan)+18名乘客ting)

    Cabin layout: 2 pilots + 18 passengers;
    基本性(xing)能︰Performance
    飛行性(xing)能︰
    Flight Performance
    最(zui)大速度/巡航速度????????????????? 244 Km/Hr
    Max Speed/Max Cruise Speed?? 244 Km/Hr
    最(zui)大續航時間?????????????????????? 5.3Hrs
    Max Endurance???????????????????? ??5.3Hrs
    最(zui)大飛行高度??????????????????????6000m
    Max. Flight Altitude????????????????6000m
    有/無地(di)效懸停(ting)升限(xian) ????????????2800/100m
    HIGE/HOGE????? ???????????????????2800/100m
    最(zui)大航程?????????? ???????????????? ?1050Km
    Max. Range?????????????? ???????????1050Km
    最(zui)大爬升率??????????????????????? ??7.6m/s
    Max Rate-of-Climb????????????????7.6m/s

    重量︰Weight?
    空(kong)重???????????????????? 7560 Kg
    Empty Weight???????????? 7560 Kg
    最(zui)大起(qi)飛重量???????????? 13000 Kg
    Max Take-off Weight???? ???13000 Kg
    有效載重???????????????? 4000 Kg
    Max Payload????????????? 4000 Kg
    最(zui)大吊(diao)運重量???????????? 5000Kg
    Max. Sling Load?????????? 5000Kg

    動力︰Powerplant
    三台加普惠(hui)PT6B-67A發動機,
    3 P&WC PT6B-67A engines
    最(zui)大地(di)面(mian)起(qi)動高度? 4500m,
    Max. Ground Starting Altitude: 4500m
    最(zui)大空(kong)中起(qi)動高度?? 6000m,
    Max. Aerial Starting Altitude: 6000m
    起(qi)飛功率? 1447kw?
    Take-off Power: 1447Kw
    最(zui)大連續功率? 1249kw
    Max. Continuous Power: 1249Kw

    燃(ran)油ting)/strong>Fuel
    有效總的(de)燃(ran)油tu)浚800 Kg
    Total Effective Fuel Volume:? 3800Kg
    20min可(ke)用余(yu)油tu)浚90 Kg;
    Useful Reserve for 20min: 390Kg;
    標準油箱容量???? 4740L
    Standard Tank Volume: 4740L
    外形尺寸(cun)
    External Dimensions
    全長(旋翼旋轉)???????????? ???????? ?? ??23.045 m
    Overall Length (Rotors turning)???????? 23.045 m
    全高(空(kong)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(shi)︰
    Product Advantage:

    載重量大,吊(diao)掛能力強

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

    ◆ 出色的(de)航程和續航能力

    Excellent range and endurance capability;

    ◆ 大量使(shi)用復合材料,延長使(shi)用壽(shou)命

    Composite material is widely used to extend service life cycle

    ◆ 綜(zong)合顯示控(kong)制(zhi)系統為飛行xing)yuan)提供(gong)飛行狀態信息、導航信息、機電管理系統的(de)備份顯示及其它機載信息的(de)綜(zong)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(shi)聯動,安全可(ke)靠

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

    ◆ KJ-15A自動駕駛(shi)儀(yi),減輕(qing)駕駛(shi)負(fu)擔

    KJ-15 autopilot reduces the workload of the pilot.

    ◆ 抗墜(zhui)毀座椅、告警系統使(shi)直升機更安全、可(ke)靠

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

    ◆ 機外照明系統提供(gong)直升機的(de)航jiao)蠔頭轎恍畔 yi)及防撞告警信號,並在(zai)著陸時照亮周圍場地(di),使(shi)飛行xing)yuan)能清晰目視(shi)直升機著陸時的(de)位置和高度qu)

    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wen)rou)軟,舒適性(xing)好

    Spacious cabin and soft seats with excellent comfort;

    ◆ 使(shi)用成(cheng)本低ting) 閿諼 

    Low operation cost and easy of maintenance,

    ◆ 具有xie)就tu)化優勢(shi)和完(wan)善的(de)用戶管理服務體系,可(ke)提供(gong)快(kuai)速響應(ying)、飛行和機務培訓、工程技術支(zhi)持等服務,支(zhi)持快(kuai)速的(de)維修(xiu)、備件(jian)支(zhi)援、通航托管等qu)

    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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