Tianyi UAV
Tianyi UAVs are Chinese UAVs developed by Nanjing Tianyi (meaning Sky One) Unmanned Aerial Vehicles Co., Ltd. (Tianyi, 南京天一无人飞行器有限公司) Some of its UAVs are jointly developed with Nanjing University of Science and Technology.
Flying Fox 1
Flying Fox 1 (Fei-Hu Yi-Hao or Feihu Yihao, 飞狐一号) UAV is an experimental UAV developed by Tianyi to gain experience in carrier landing. Flying Fox 1 UAV is a fixed-wing UAV with a twin-boom layout, inverted v-tail, and tricycle landing gear. Propulsion is provided by a twin-blade pusher propeller driven by a gasoline engine mounted in the rear end of the fuselage. The Flying Fox 1 gained attention when it won the 500000 ¥ prize during the AVIC Cup International UAV Innovation Grand Price Competition (Zhong-Hai Gong-Ye Bei Guo-Ji Wu-Ren Fei-Xing-Qi Chuang-Xin Da-Jiang-Sai中航工业杯国际无人飞行器创新大奖赛) held in Beijing in February 2011. Specification:[1][2]
- Speed: 90–100 km/h
- Weight: < 20 kg
- Take-off distance: < 40 m
- Landing speed: 70 km/h
- Take-off: taxiing
- Landing: taxiing + arresting wiring
- Unit cost: 200000 ¥
Training UAV Flying Sky
The training UAV Flying Sky (Fei-Tian or Feitian, 飞天) is a UAV of conventional layout with high-wing configuration and tricycle landing gear. The nose wheel has a fairing to reduce drag. Propulsion is provided by a two-blade propeller driven by a tractor engine mounted in the nose.[3] The training UAV Flying Sky is intended to be used as a lower cost training UAV for future UAV crews operating more expensive UAVs, such as the TY-HC series. Externally, this training UAV Flying Sky visually resembles a miniature version of the Cessna 152.[4] The training UAV Flying Sky has also been used in the development of the Flying Fox 1 experimental aircraft, designed to gain experience in carrier landing.[5]
TY-DB3
TY-DB3 is an UAV in conventional layout with high wing configuration and tricycle landing gear system. Propulsion is provided by a three-blade propeller driven by a tractor engine mounted in the nose, powered by a Komatsu Limited 80 cc gasoline engine.[6] Specification:[7]
- Wingspan: 2.93 m
- Height: 0.5 m
- Max take-off weight: 35 kg
- Payload: 3 kg
- Control radius: 50 km
- Max speed: 130 km/h
- Cruise speed: 110 km/h
- Ceiling: 1 km
- Endurance: 3 h
- Take-off: taxiing
- Landing: taxiing and parachute
TY-HC30
TY-HC30 is a fixed-wing UAV in twin-boom layout with tricycle landing gear. Propulsion is provided by a two-blade propeller driven by a pusher gasoline engine mounted in the rear end of the fuselage.[8][9]
- Wingspan: 2.98 m
- Height: 0.68 m
- Max take-off weight: 28 kg
- Payload: 5 kg
- Control radius: 50 km
- Max speed: 140 km/h
- Cruise speed: 110 km/h
- Ceiling: 3.5 km
- Endurance: 2–3 h
- Take-off: taxiing
- Landing: taxiing or parachute
TY-HC40 Sky Eye
TY-HC40 is a fixed-wing UAV in twin-boom layout with inverted v-tail. Propulsion is provided by a two-blade propeller driven by a pusher gasoline engine mounted in the rear end of the fuselage, and it has a tricycle landing gear system.[10] Specification:[11]
- Wingspan: approximately 4 m
TY-HC75
TY-HC-75 UAV is a fixed-wing UAV in twin-boom layout with winglets and tricycle landing gear. Propulsion is provided by a three-blade propeller driven by a pusher engine mounted in the rear end of the fuselage, powered by a Limbach Flugmotoren 275 twin cylinder gasoline engine.[12] Specification:[13]
- Wingspan: 4.8 m
- Height: 0.9 m
- Max take-off weight: 75 kg
- Payload: 25 kg
- Control radius: 50–100 km
- Max speed: 180 km/h
- Cruise speed: 125 km/h
- Ceiling: 6 km
- Endurance: 4 h
- Take-off: taxiing
- Landing: taxiing or parachute
TY-Z10
TY-Z10 UAV is a fixed-wing UAV in twin-boom layout with inverted v-tail. Landing gear system consists of a pair of skids and propulsion is provided by a two-blade propeller driven by a pusher engine mounted in the rear end of the fuselage, powered by DL55 engine.[14] Specification:[15]
- Wingspan: 3.902 m
- Wing area: 1.2 m2
- Length: 2.211 m
- Height: 0.68 m
- Empty weight: 24 kg
- Max take-off weight: 40 kg
- Payload: 10 kg
- Fuel: 5.6 kg
- Max speed: 140 km/h
- Cruise speed: 85 km/h
- Ceiling: 2 km
- Endurance: 2–3 h
- Take-off: catapult
- Landing: parachute