岳的又肥又大水多,學生真實初次破初視頻

?
Business area
Other
  • Product Brief

    Tianyi -1 UAV is a light multi-purpose UAV developed by Chengdu aircraft industry group. With two kinds of take-off modes, vehicle parachute and ejection, parachute recovery and real-time information transmission can be widely used for aerial survey, aerial photography, remote sensing, environmental protection and other tasks.

    Design features

    Tianyi -1 UAV system is completed in accordance with the requirements of Chengfei's existing military aircraft development system. From design to material procurement, product development, manufacture, test and flight test, there is a complete quality control system to control it. The structure of the whole machine block is made of carbon fiber composite, which has the characteristics of light weight, high strength and rigidity, long fatigue life and so on. In addition, the aircraft adopts the patented buffer system of Chengfei company, which is flexible and convenient to use. At the same time, parachute recovery has unique and complete flight safety assurance measures. The whole machine system has complete functions, excellent performance, reasonable and concise system configuration, and the highest flying quality in GJB: first class flying quality.

    performance data

    The maximum flat speed is 180KM/H;

    Cruising speed 120KM/H;

    Practical ceiling 4000M;

    TT & C radius 100KM;

    Maximum take-off weight 87KG;

    Task load 20KG;

    Duration 3H.

    General layout and aerodynamic characteristics

    Tianyi -1 UAV adopts the normal layout of high aspect ratio / trapezoid upper and middle wing, streamlined cabin, double tail supporting double vertical tail and propelling propeller. The total length of the aircraft is 2.465M, the height is 0.97M, the fuselage is 1.727M, and the wing wingspan is 4.179M.

  • Product Brief

    The night hawk UAV system is a new generation of small short-range UAV, which is developed by our country. It is mainly used for battlefield surveillance, target location, correction shooting and damage evaluation. The system uses rocket assisted zero length launches, with light weight, large workload, flexible operation and convenient operation.

    performance data

    The maximum take-off weight is less than 90kg.

    Task load 20kg;

    The combat radius is 110km;

    The maximum flat speed is 170km/h;

    Voyage 3H;

    The ceiling is 3500m.

    General layout and aerodynamic characteristics

    The small short range UAV is a single propeller propeller engine with a single wing and all composite structure. Aircraft captain 3.165m, wingspan 3.79M, machine height: 1.26m. Aircraft wing airfoil LS (1) -0417MD, tail V inverted V tail form, inverted V tail angle: 80. Rocket assisted take-off, parachute recovery, fuselage with sled damping system to increase the landing safety of aircraft. The standard weight of the aircraft is 88 kilograms.

  • Product Brief

    The hawk UAV system is a hollow low-speed UAV system developed by China Aviation Industry Guizhou aircraft Co., Ltd. on the basis of the existing unmanned aerial vehicle system, aiming at the market prospect of domestic and international civilian market and the demand of foreign support.

    Design features

    The hawk UAV system consists of four subsystems: the aircraft subsystem, the measurement and control information transmission subsystem, the mission equipment subsystem and the integrated support subsystem. The whole system consists of two to four UAVs and a set of ground stations. The mission equipment is basically configured as UAV in the CCD digital camera and (Falcon) 100 synthetic aperture mirror radar, and the two mission equipment is individually installed. The way of loading can be configured according to the needs of users. In addition, under the premise of ensuring weight, size, work numbers and joints to meet the hawkman UAV, different mission equipment can be loaded according to user requirements. The hawk UAV system wing is a single beam structure with an auxiliary beam connecting aileron and flaps. The wing has two parts. Each wing is composed of the main beam of the connecting wing and the composite skin. The winglet winglet is an integrated composite structure, and the fuselage is a semi hard shell consisting of stiffeners and hard aluminum skin. The size of the machine is 6 meters long, 10 meters in span, 2.2 meters in height, 6 meters in length, 1 meters in height and 2.2 meters in height.

    performance data

    Maximum take-off weight: 700kg;

    Task load: 60-100kg;

    Maximum flat speed: 230km/h;

    Cruising speed: 170km/h;

    Cruising altitude: 500-7000m;

    Practical ceiling: 7500m;

    Duration: >16h (task load 60kg);

    >12h (task load 100kg);

    Take-off and landing mode: wheel run and take-off and landing;

    Take off distance: <400m;

    Landing distance: <350m.

  • Aviation electromechanical services and support

  • Aeronautical electromechanical Civil Aviation

  • Aero electromechanical second power system

  • Airborne electromechanical air drop airborne system

  • Aviation electromechanical protection lifesaving system

    ?

  • Aeronautical electromechanical fire prevention system - anti / de icing system

  • Aviation electromechanical freight system

  • Aero electromechanical high lift system

  • Aeronautic electromechanical seats and cabin equipment

  • Aeronautical electromechanical environment control system

  • Aero electromechanical hydraulic system

  • Aeronautical electromechanical fuel system

  • Aeronautical electromechanical power system

  • Product Brief

    The LS-6 guided glider is a new type of guided weapon with independent intellectual property rights developed in China. Its overall performance is comparable to that of the most advanced fourth generation guided bomb JDAM-ER in the United States.

    System features: the combined guidance method of strapdown inertial navigation and satellite positioning has the characteristics of out of area attack, all-weather use, no matter after launching, long range, high precision, low cost, strong anti-interference ability and strong adaptability of aircraft.

    Combat mission and role: the LS-6 guided glider bomb is a high cost effectiveness weapon between conventional air bombs and air to ground missiles. It can be mounted on bombers, fighter bombers and assault planes with the ability to air bombs, and is used to attack fixed points on the ground (SEA).

    Loaders: trainers, UAVs, fighters.

    main parameter

    Guidance system: strapdown inertial navigation + satellite positioning;

    Maximum attack distance: 60km;

    Guidance accuracy: 15m (CEP).

    ?

    ?

    ?

    ?

    ?

    ?

    ?

  • Product Brief

    TY-90 is a multi-purpose infrared tactical missile. It can intercept low altitude, ultra-low altitude flying helicopters, fixed wing aircraft or cruise missiles and other targets.

    System features: multiple infrared guidance; anti-jamming capability; automatic interception and tracking; zero height and zero initial velocity launching capability; digital information processing system; small size and light weight.

    Carrier platform: as the TY90 missile is light in weight and small in size, it can be flexibly arranged on various carrier platforms.

    main parameter

    Projectile diameter: 90mm;

    Length: 1862 mm;

    Quality: 20kg;

    Range: 6 km.

    ?

    ?

    ?

    ?

    ?

    ?

  • Product Brief

    The PL5E-II air-to-air missile is an enhanced third generation close combat air to air missile. It uses two color multi detector, missile borne computer and laser fuze technology. It has excellent anti-interference ability, omnidirectional attack ability and better detection ability. System features: with the ability to transmit, laser proximity fuze; infrared multi color seeker; high-energy fragment warhead. Carrier platform: Xiaolong, annihilate series, annihilate FII, FBC-1, L-15 and so on.

    main parameter

    Aerodynamic layout: duck type;

    Maximum detection distance: 16 Km;

    Maximum flight speed: 3 M;

    Maximum overload: 35g;

    Projectile diameter: 127mm;

    Projectile length: 2893mm;

    Wingspan: 617mm.

    ?

    ?

    ?

    ?

    ?

    ?

    ?

  • Product Brief

    The PL-9C air-to-air missile is the third generation infrared close range combat missile, which has the ability to resist infrared decoy and omnidirectional attack. It can be used to attack all kinds of manned and unmanned vehicles, mainly for attacking fighters. System features: multiple infrared guidance; anti infrared decoy jamming capability; no matter after launch; radar and helmet follow; excellent maneuverability. Carrier platform: Xiaolong, annihilate series, annihilate FII, FBC-1, L-15 and so on.

    main parameter

    Projectile length: 2992mm;

    Diameter: 157mm;

    Quality: 115KG;

    Wingspan: 856mm;

    Range: 20km.

    ?

    ?

    ?

  • Product Brief

    SD-10A is an advanced fourth generation active radar medium range air-to-air missile. It has high guidance accuracy, large kill probability and strong electronic anti-jamming capability. It has all-weather, full height, all directional attack capability, and beyond the horizon launch and launch capability. It can not only intercept and shoot, but also close combat. It can attack large maneuvering targets and low altitude targets in electronic warfare environment. Stealth targets, multi-target and group targets.

    System characteristics: over the horizon attack capability; all-around, all-weather attack capability; multi-target attack; no matter after launch. Guidance: strapdown inertial navigation plus radio correction + active radar terminal guidance. Propulsion: solid rocket motor. Launch mode: guideway and ejection.

    main parameter

    Length: 3930mm;

    Diameter: 203mm;

    Wingspan: 674mm;

    Rudder Exhibition: 754mm;

    Weight: 198kg;

    Maximum maneuverability: 38g;

    Operational height: 0 ~ 21km;

    Range: 70km.

    ?

Related videos
?
http://www.gdgsbao.com/ http://www.baidu.com/ https://m.baidu.com/ https://www.sogou.com/ https://www.iqiyi.com/ https://www.qq.com/ https://v.qq.com/channel/choice http://paper.people.com.cn/rmrb/html/2020-04/04/nbs.D110000renmrb_01.htm http://www.xinhuanet.com/ https://www.weibo.com/ https://m.sohu.com/limit/ https://news.china.com/ http://www.bjnews.com.cn/ http://www.infzm.com/ http://www.ifeng.com/ https://www.huanqiu.com/ http://www.bookbao8.com/ http://book.qidian.com/ https://www.aizhan.com/ 山东快乐扑克3豹子遗漏