Quanhua UAV

Quanhua UAVs are Chinese UAVs developed by Tianjin Quan-Hua (meaning All China) Times Spaceflight Technology Co., Ltd. (Quanhua, 天津全华时代航天科技发展有限公司), some of which has entered service with Chinese military and law enforcement establishments.

Albatross

Albatross (Xin-Tian-Weng or Xintianweng, 信天翁) UAV is a fixed-wing UAV developed by Quanhua in a twin-boom layout with inverted v-tail and tricycle landing gear. Proplusion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage. Specification:[1]

  • Normal radius (km): 600
  • Length (m): 2.56
  • Wingspan (m): 3.7
  • Height (km): 0.545
  • Ceiling (km): 5
  • Normal operating altitude (m): 200 – 3000
  • Max take-off weight (kg): 21.5
  • Payload (kg): 10
  • Max speed (km/h): 130
  • Cruise speed (km/h): 90
  • Endurance (h): 20
  • Max wind scale allowed for operation: 6
  • Operating temperature (°C): - 15 to 40
  • Storage temperature (°C): - 40 to 55
  • Launch: taxiing, or catapult
  • Recovery: taxiing or parachute

Double-Headed Eagle

Double-Headed Eagle (Shuang-Tou-Ying or Shuangtouying, 双头鹰) UAV is a fixed-wing UAV developed by Quanhua in a twin-boom layout with inverted v-tail and tricycle landing gear. Double-Headed Eagle is a twin-engine UAV with proplusion is provided by a pair of two-blade propellers driven by engines, one mounted at the nose and the other at the rear end of the fuselage. Specification:[2]

  • Normal radius (km): 600
  • Length (m): 2.6
  • Wingspan (m): 5
  • Height (km): 0.915
  • Ceiling (km): 5
  • Normal operating altitude (m): 200 – 3000
  • Max take-off weight (kg): 50
  • Payload (kg): 25
  • Max speed (km/h): 150
  • Cruise speed (km/h): 100
  • Endurance (h): 8
  • Max wind scale allowed for operation: 6
  • Operating temperature (°C): - 15 to 40
  • Storage temperature (°C): - 40 to 55
  • Launch: taxiing
  • Recovery: taxiing

FG20TM0 Mobula

FG20TM0 Mobula (Fu-Fen or Fufen, 蝠鲼) is a gasoline-powered fixed-wing UAV developed by Quanhua in a blended wing body layout without vertical stabilizer, but with winglets. FG20TM0 Mobula can be launched by various means, including vehicle launch where the UAV will become airborne after the vehicle speed reached 80 miles per hour.[3] Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose. FG stands for Fixed-wing, Gasoline-powered. Specification:[4]

  • Normal radius (km): 200 – 240
  • Length (m): 1.28
  • Wingspan (m): 2.3
  • Height (km): 0.39
  • Ceiling (km): 3.5
  • Normal operating altitude (m): 100 – 2000
  • Max take-off weight (kg): 15
  • Payload (kg): 3.5
  • Max speed (km/h): 160
  • Cruise speed (km/h): 120
  • Endurance (h): 4 – 6
  • Operating temperature (°C): - 15 to 40
  • Storage temperature (°C): - 40 to 55
  • Max wind scale allowed for operation: 6
  • Navigation: GPS
  • Launch: vehicle assisted, taxiing, or catapult
  • Recovery: parachute

FG55TM0

FG55TM0 is a miniature UAV developed by Quanhua in conventional layout with high-wing configuration and tricycle landing gear. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose. FG55TM0 is primarily intended for aerial survey / photography applications. Specification:[5]

  • Wingspan (m): 2.46
  • Length (m): 1.9
  • Height (m): 0.55
  • Max take-off weight (kg): 12
  • Payload (kg): 3
  • Ceiling (km): 3
  • Endurance (h): 3
  • Operation radius (km): 60
  • Max speed (km/h): 135
  • Cruise speed (km/h): 100

FG210TM0 Griffin

FG210TM0 Griffin (Shi-Jiu or Shijiu, 狮鹫) UAV is a gasoline-powered fixed-wing UAV developed by Quanhua in conventional layout with Pelikan tail and low wing configuration. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose.[6] Specification:[7]

  • Normal radius (km): 300
  • Length (m): 3
  • Wingspan (m): 5
  • Height (km): 1
  • Ceiling (km): 6
  • Normal operating altitude (m): 300 – 5000
  • Max take-off weight (kg): 75
  • Payload (kg): 25
  • Max speed (km/h): 180
  • Cruise speed (km/h): 120 – 160
  • Endurance (h): 5 – 10
  • Max wind scale allowed for operation: 6
  • Navigation: GPS
  • Launch: vehicle assisted, taxiing, or catapult
  • Recovery: taxiing or parachute

HG26TM0 Silver Dragon

HG26TM0 Silver Dragon (Yin-Long or Yinlong, 银龙) UAV is a gasoline-powered unmanned helicopter in conventional helicopter layout developed by Quanhua, and the landing gear consists of a pair of skids. HG stands for Helicopter, Gasoline-powered, and 26 is for the 26 cc engine used on this unmanned helicopter.[8] Specification:[9]

  • Normal radius (km): 30
  • Main rotor diameter (m): 1.8
  • Tail rotor diameter (m): 0.33
  • Ceiling (km): 3
  • Normal operating altitude (m): 10 – 1000
  • Max take-off weight (kg): 10
  • Max speed (km/h): 80
  • Cruise speed (km/h): 20
  • Endurance (h): 1
  • Operating temperature (°C): - 15 to 40
  • Storage temperature (°C): - 40 to 55
  • Max wind scale allowed for operation: 6
  • Navigation: GPS

HG80TM0 Silver Dragon 2

HG80TM0 Silver Dragon 2 (Yin-Long 2 or Yinlong 2) UAV is a gasoline-powered unmanned helicopter in conventional helicopter layout developed by Quanhua, and the landing gear consists of a pair of skids. HG stands for Helicopter, Gasoline-powered, and 80 is for the 80 cc engine used on this unmanned helicopter. Specification[10]

  • Normal radius (km): 30
  • Main rotor diameter (m): 2.2
  • Tail rotor diameter (m): 0.4
  • Ceiling (km): 3.5
  • Normal operating altitude (m): 10 – 1000
  • Max take-off weight (kg): 32.5
  • Max speed (km/h): 80
  • Cruise speed (km/h): 30
  • Endurance (h): 1
  • Operating temperature (°C): - 15 to 40
  • Storage temperature (°C): - 40 to 55
  • Max wind scale allowed for operation: 6
  • Navigation: GPS

HG400TM0 Thunderbird

HG400TM0 Thunderbird (Lei-Niao or Leiniao, 雷鸟) UAV is an unmanned helicopter in conventional helicopter layout with a pair of skids as landing gear.[11] HG stand for Helicopter, Gasoline-powered. Specification:[12]

  • Normal radius (km): 50
  • Length (m): 3.55
  • Fuselage width (m): 0.64
  • Height (m): 0.9 – 1.6, depending on types of landing gear
  • Ceiling (km): 3
  • Normal operating altitude (m): 10 – 1000
  • Max take-off weight (kg): 135
  • Payload (kg): 65
  • Max speed (km/h): 120
  • Endurance (h): 1

JXN-20 Auspicious Bird

JXN-20 Auspicious Bird (Ji-Xiang-Niao or Jixiangniao, 吉祥鸟) UAV is a fixed wing micro air vehicle (MAV) developed by Quanhua. Externally, JXN-20 looks like Northrop X-4 Bantam without the inlets because it is powered by a two-blade propeller driven by a tractor engine mounted in the nose. There are two models of JXN-20 Auspicious Bird, JXN-20-A and JXN-20-B, one is powered by gasoline, and the other by methanol fuel. Specification:[13]

  • Normal radius (km): 150
  • Length (m): 1.2
  • Wingspan (m): 1.6
  • Height (km): 0.45
  • Ceiling (km): 3.5
  • Normal operating altitude (m): 10 – 1000
  • Max take-off weight (kg): 6.5
  • Max speed (km/h): 180
  • Cruise speed (km/h): 60 – 150
  • Endurance (h): 3 for gasoline-powered, 1.5 for methanol-powered
  • Operating temperature (°C): - 15 to 40
  • Storage temperature (°C): - 40 to 55
  • Max wind scale (speed) allowed for operation: 5 (10.7 m/s)
  • Navigation: GPS
  • Launch: hand or catapult
  • Recovery: parachute

Silver Eagle

Silver Eagle (Yin-Diao or Yindiao, 银雕) is a fixed-wing UAV developed by Quanhua in conventional layout with high-wing configuration and tricycle landing gear. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose. Externally, Quanhua Silver Eagle looks identical to two other Chinese UAVs, Chunyi CY-03 Big White and Iflyer Big White 3, because all three share the same airframe. However, the flight control systems are complete different because each developer separately developed their own indigenous flight control systems. The performance of Silver Eagle is similar to the other two Chinese UAVs due to the same hardware used.[14] Specification:

  • Wingspan: 2.95 m
  • Length: 2.3 m
  • Max speed: 135 km/h
  • Min speed: 65 km/h
  • Empty weight: 22 kg
  • Max takeoff weight: 35 kg
  • Normal payload: 6–8 kg
  • Max payload: 16 kg
  • Fuel: 8 L
  • Cruise speed: 90–110 km/h depending on payload
  • Ceiling: 5 km
  • Endurance: 2–3 h depending on payload
  • Rate of climb: 6–8 m/s depending on payload
  • Max wind scale allowed for operation: 5
  • Launch: catapult or takeoff
  • Takeoff distance: 100 m

See also

List of unmanned aerial vehicles of the People's Republic of China

References

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