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无人机快艇通用铝合金30Cc汽油发动机马达

UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en

AI-450C (CM,CD,CP) NBS Aircraf...

Takeoff (S/L static;ISA) Propeller shaft power, hp..........…...........400...49

JRTD-30CC 独特高速汽油发动机风冷遥控无人机飞机模型...

UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en

汽油发动机单缸 30cc 适用于飞机无人机

UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en

模具冲压/旋压+焊接材质：低碳钢/不锈钢/高温合金等

Check at every level: from production to testing one-stop service material selec

无人机铝合金30cc发动机供应商单缸汽油发动机

UAV Drone Gasoline Engine The Drone Gasoline Engine is an internal combustion en

EEJ-20（J70）Micro Jet Engine

Model:EEJ-20 Maximum thrust(daN):19 Maximum speed(rpm):120,000 Specific fuel con

熔模铸造/数控加工材料：GH4169/K418/K424/K...

Turbine Wheels / Shaft & Wheels E&E Turbo can be able to supply an e

W40 turbojet engine

Excellent thrust-to-weight ratio, low fuel consumption, integrated inspiration,

D-436-148FM NBS Aircraft Engin...

Takeoff /Emergency(S/L static;ISA) Thrust, kgf ..........................7,880/8

Sinotruk 615-371 Horsepower Ne...

中国重汽 615-371 马力马达船用发动机

MD550汽油发动机

Twin cylinder horizontally opposed air-cooled, two-stroke gasoline engine with m

MDR208 转子发动机

The MDR208 has the highest power-to-weight ratio compared to other rotary engine

AI-322-30,AI-322-40 NBS Aircra...

Takeoff(S/L static;ISA) Thrust, kgf.................3,000...........3,755 Specif

AI-8 NBS Aircraft Engines

(S/L static;ISA) Generator terminals power, kW ........ 60 Fuel consumption, kg/

AI-28 NBS Aircraft Engines

Specific fuel consumption by 15...20% lower than that of current engines in this

短寿命涡轮喷气发动机 AI-350 NBS 航空发动机

Maximum power rating (S/L static; ISA;=1.0) Thrust, daN ................... ....

AI-322F,AI-322-30F NBS Aircraf...

Check at every level: from production to testing one-stop service material selec

AI-450-2,AI-450C-2(CP-2) NBS A...

AI-450-2 Takeoff(S/L static;ISA) Power, hp ................…....................

W125/110 涡喷发动机

Excellent thrust-to-weight ratio, low fuel consumption, integrated inspiration,

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