TD220 Unmanned Helicopter
SKU: MD-P00111·UAV Platforms·Sob encomenda
Visão geral
TD220 Unmanned Helicopter drone are Chinese UAVs developed by ZHZ Science and Technology Ltd. A total of two ZHZ UAVs have had developed and both are unmanned helicopters. TD220 Unmanned Helicopter is a coaxial unmanned helicopter developed by ZHZ. The indigenously developed coaxial rotors has only half as many components as that of Kamov coaxial rotors, thanks to the replacement of many mechanical parts with electrical components. TD220 Unmanned Helicopter only needs a space of 5 m x 5 m to take-off or land. Max takeoff weight: 290 kg Power plant: 65 hp engine powered by either gasoline or kerosene TD220 Unmanned Helicopter 【伟大的变革 庆祝改革开放40周年大型展览之二十三】大国 ... TD220共轴双旋翼无人直升机由北京中航智科技有限公司研发，是第一款电控共轴无人机，起飞重量330kg，最大载荷50kg，续航时间达5小时 中航智是我国无人直升机研究的专业企业，已经推出TD220、T15K、T333等多款无人直升机产品，无一例外是共轴双旋翼布局，所以其15吨级直升机 CANopen controls helicopter drone rotor - CAN Newsletter ... 2019年8月22日 - The TD220 unmanned aerial vehicle (UAV) uses Hornet CANopen ... Like fixed-wing aircraft, helicopters can be adjusted in pitch (rotation 2012年，中航智实现了中国第一架电控共轴无人直升机首飞。2015年，成功中标海关总署无人机项目，TD220成为中国海关应用的首款无人直升机 中航智公司的TD220无人机. 【环球无人机报道】11月17日， 尖兵之翼 无人机航展在深圳举行，现场有来自国内外多个厂商参加，在中航智展台前 ZHZ's TD220 VTOL Unmanned Aircraft System makes debut ... 2015年11月9日 - The TD220 co-axial twin-rotor unmanned helicopter is a heavier version of that previously shown, being a 220ME model with twin tailfins and ZHZ tech flies high in high-tech expo - China Daily 2015年5月29日 - The TD 220 unmanned helicopter developed by ZHZ tech received warm response after appearing on the 18th China Beijing International WWW.KEPT.NET.CN-2016年11月3日 中航智研发的TD220共轴双旋翼无人直升机可搭载100kg的有效载荷，飞行速度为100km/h，续航时间为5h，可广泛应用于警用、测绘、巡线、侦察等 . Beijing ZHZ Displays TD220 Unmanned Helicopter | News ... 2014年2月12日 - New Singapore Airshow exhibitor Beijing ZhongHanZhi Technology Co. (ZHZ) is displaying its TD220 unmanned helicopter at Booth U08 in
Especificação técnica
Specifications. Especificações principais: Rotor diameter 3.964 m, Length 2.48 m, Width 0.54 m, Height 1.78 m, Empty weight 140 kg, Max takeoff weight 290 kg, Payload 100 kg, Endurance 5 hr, Cruise speed 100 km/hr, Ceiling 4 km, Power plant 65 hp engine powered by either gasoline or kerosene, 中航智田刚印 抓住军民融合的历史机遇.
Especificação técnica — 1 groups
Especificações principais: Rotor diameter 3.964 m, Length 2.48 m, Width 0.54 m, Height 1.78 m, Empty weight 140 kg, Max takeoff weight 290 kg, Payload 100 kg, Endurance 5 hr, Cruise speed 100 km/hr, Ceiling 4 km, Power plant 65 hp engine powered by either gasoline or kerosene, 中航智田刚印 抓住军民融合的历史机遇.
Especificações técnicas
Specifications
- Rotor diameter
- 3.964 m
- Length
- 2.48 m
- Width
- 0.54 m
- Height
- 1.78 m
- Empty weight
- 140 kg
- Max takeoff weight
- 290 kg
- Payload
- 100 kg
- Endurance
- 5 hr
- Cruise speed
- 100 km/hr
- Ceiling
- 4 km
- Power plant
- 65 hp engine powered by either gasoline or kerosene
- 中航智田刚印
- 抓住军民融合的历史机遇