GrabCAD 模型信息
VTOL UAV with batteries · 模型 109134
Луна (Luna) - echo in Ukrainian Acknowledgments I thank the GrabCAD members whose models I used in this project Electronic elements of the control system https://grabcad.com/riley.entropy-1/models?page=1 RotoMotor and servo drive https://grabcad.com/felipe.westin-1 Speed controller https://grabcad.com/miyuranga-1 Layout: aircraft with 4 lifting electric motors and a cruise power plant with one engine and a pusher propeller. Takeoff weight is limited to 40 kg, wing loading is no more than 40 kg/m*2, wingspan is ~ 4 m. 3M model – Autodesk Inventor (component designations according to ATA100) Main materials: Carbon fiber composite – outer surfaces of load-bearing planes, box-shaped parts, tubular spars – density ~ 1.43 g/cm*3 Foam plastic – filler for load-bearing planes – density ~ 0.033 g/cm*3 Polypropylene – parts manufactured by 3M printing density ~ 1.32 g/cm*3 Polyethylene, aluminum, etc. … Lifting motors 12S 230 KV MAD M6V68 IPE V1.0 with FLUXER PRO 22x6.6 MFTT propeller were selected https://mad-motor.com/products/mad-components-v68-vtol?VariantsId=10564 T-MOTOR FLAME 100A 12S V2.0 Speed Controller https://store.tmotor.com/product/flame-60a-12s-V2-esc.html?srsltid=AfmBOorp9NEFUCs1gynK-MZQZCJ5frXyQqhpk3-lelJ5u2mzbOVyfNEC Total power plant weight = 4*(378 + 56 +79) = 2052 g For one engine (1 cycle) Takeoff time – 70 s 85% = 46.8V / 49.44A / 7036 RPM / 2.315 kW e-power / 10.09 kG thrust – minimum energy reserve – 0.045 kWh Assumed vertical ascent speed 5 m/s (descent – 2.5 m/s) Vertical acceleration 0.25g – thrust 12.5 kG * time 2 s 100% = 3.444 kW kW e-power 12.8 kG thrust = 0.002 kWh 4 electric motors and minimum 2 takeoff-landing cycles ~ 0.4 kWh Horizontal flight mode Cruising speed 25m/s (90km/h) Required thrust ~ 7.5 kG Electric cruise engine – MAD M6V68 IPE V1.0 70% motor shaft power 1.2 kW electric power 1.5 kW Adjustable (on the ground) pitch propeller 22'' MAD 6S 32Ah Drone Solid State Lithium-ion Battery – https://mad-motor.com/products/6s-32ah-drone-battery 32000 mAh 710.4 Wh 180*95*70mm 2.479 kG 8 batteries = total capacity 5.68 kWh, weight – 19.83 kg Taking into account 2 takeoff – landing cycles (0.4 kWh), horizontal flight time 3.5 h ~ 315 km
- 格式
- STEP / IGES、AutoCAD、Other、Parasolid、Rendering
- 分类
- Aviation、Energy and Power、Machine design
- 标签
- 未标注
- 数据更新
- 2026-10-16T14:54:31Z
