Long Technology Triumph

Long Technology UAVs are Chinese UAVs developed by Beijing Long Technology Co., Ltd. (Long Technology, 北京久久凯旋航测科技有限公司), whose products are marketed under the brand Triumph. Traditionally a flight control system provider to other Chinese aircraft (including UAVs) manufacturers, Long Technology has recently expanded its business by developing its own brand of UAVs, some of which are integrations of commercial off-the-shelf (COTS) products such as airframes and flight control systems/software indigenously developed by Long Technology.

Triumph 1

Triumph 1 (Kai-Xuan Yi-Hao or Kaixuan Yihao, 凯旋1号) is an electrically powered micro air vehicle (MAV) which has a layout almost identical to another Chinese MAV, Weiyujie W-1 Sky Hawk.[1] This MAV is hand held and propulsion is provided by a two-blade pusher engine mounted at the rear end of the empennage. Specification:[2]

Wingspan: 1.1 m
Wing area: 32 dm2
Length: 0.9 m
Take-off weight: 2.2 kg
Payload: 0.5 kg
Cruise speed: 60 km/hr
Ceiling: 2 km
Endurance: 20 – 50 min (depending on batteries)
Max wind scale allowed for operation: 5

Triumph 2

Triumph 2 (Kai-xuan Er-Hao or Kaixuan Erhao, 凯旋2号) is an UAV of conventional layout with high-wing configuration with T-tail. Proplusiong is provided by a two-blade propeller driven by a tractor engine mounted above the fuselage just in front of the wing, and the UAV has a tricycle landing gear system. This UAV is powered by methyl alcohol. Specification:[3]

Wingspan: 2.76 m
Length: 2 m
Take-off weight: 11.6 kg
Empty weight: 9.3 kg
Max speed: 120 km/hr
Cruise speed: 60 – 80 km/hr
Ceiling: 3 km
Endurance: 1 hr
Range: 100 km
Max wind scale allowed for operation: 5

Triumph Goose 1

Triumph Goose 1 (Kai-Yan Yi-Hao or Kaiyan Yihao, 凯雁1号) is an UAV of conventional layout with high-wing configuration. Proplusiong is provided by a two-blade propeller driven by a tractor engine mounted in the nose and the UAV has a tricycle landing gear system. Specification:[4]

Wingspan: 3.16 m
Length: 2.15 m
Take-off weight: 26.5 kg
Payload: 5 kg
Max speed: 150 km/hr
Cruise speed: 100 km/hr
Ceiling: 5 km
Relative operating altitude: 200 – 1100 m
Useful altitude: 200 – 3000 m
Max wind scale allowed for operation: 7 – 9
Navigation: INS with GPS

Triumph Sky Hawk 1

Triumph Sky Hawk 1 (Kai-xuan Tian-Ying Yi-Hao or Kaixuan Tianyin Yihao, 凯旋天鹰1号) is a gasoline-powered UAV that share the same airframe with another Chinese UAV, the Keyuan Type II, but the flight control software is different than that of Keyuan Type II in that Triumph Sky Hawk 1 has flight control system developed by Long Technology. The UAV has twin-boom layout and it has tricycle landing gear. Propulsion is powered by two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage. Specification:[5]

Wingspan: 4.05 m
Length: 2.8 m
Height: 0.9 m
Take-off weight: 60 kg
Empty weight: 20 kg
Length of fuselage: 1.825 m
Fuel: 14 L
Power plant: 150 cc

Triumph Sky Hawk 2

Triumph Sky Hawk 2 (Kai-xuan Tian-Ying Er-Hao or Kaixuan Tianyin Erhao, 凯旋天鹰2号) is the larger cousin of the smaller Triumph Sky Hawk 1 and both share the identical twin-boom layout, and both are gasoline-powered. In addition to larger size, Triumph Sky Hawk 2 has winglets. As with Triumph Sky Hawk 1, it has tricycle landing gear and the propulsion is powered by two-blade propeller driven by a pusher engine mounted at the rear end of the fuselage. Specification:[6]

Wingspan: 4.7 m
Length: 2.6 m
Take-off weight: 70 kg
Empty weight: 50 kg
Wing area: 2.18 m2
Powe plant: 16.6 hp

Triumph Transporter

Triumph Transporter (Kai-Xuan Ban-Yun-Gong or Kaixuan Banyungong, 凯旋搬运工) is a gasoline-powered UAV of conventional layout with high wing configuration. This UAV has a tricycle land gear system and propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose. Specification:[7]

Wingspan: 3.16 m
Length: 2.15 m
Take-off weight: 19 kg
Empty weight: 22.5 kg
Payload: 3.5 kg
Max speed: 150 km/hr
Cruise speed: 100 km/hr
Ceiling: 5 km
Endurance: 3 hr
Range: 3 km
Max wind scale allowed for operation: 6
Navigation: GPS

KX601

KX601 is an unmanned hexacopter developed by Long Technology for rapid deployment for various missions such as aerial surveillance and photography. KX601 is mainly constructed with carbon fiber composite material and the remaining portion is constructed of aluminum. Landing gear consists of four legs. Specification:[8]

Deploymet time (min): 10
Empty weight (kg): 3.5
Max take-off weight (kg): 7
Payload (kg): 3.5
Endurance (min): 30
Max speed (km/hr): 50
Normal operating relative altitude (km): 1
Remote control radius (km): 2 – 5
Max wind scale allowed for operation: 6
Relative humidity allowed for operation: 95%
Temperature allowed for operation (°C): - 20 to + 50
Temperature allowed for storage (°C): - 50 to + 70

References

This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.

[1] Triumph 1 UAV

[2] Tirumph 1

[3] Triumph 2

[4] Triumph Goose 1

[5] Triumph Sky Hawk 1

[6] Triumph Sky Hawk 2

[7] Triumph Transporter

[KX601_UAV-8] "KX601". Retrieved 18 August 2014.