Aircraft Turbofan Engine HQ600WS
SKU: MD-P00293·Spare Parts & Components·Auf Bestellung
Übersicht
Low-pressure part: 1-stage Fan+2-stage IPC+2-stage LPT Core part: 1-stage Centrifugal HPC+ Annular reflux combustion chamber+1-stage HPT Exhaust: Mixed exhaust, simply converge nozzle High altitude long endurance UAVs Take-off Thrust ( kgf): 700 Cruising SFC kg/(kgf.h):0.75 Total Pressure Ratio: 11.0 Turbine Inlet Temp K( C)： 1313(1040) Size(diameter/length) （mm）: 472/1450
Technische Daten
Specifications. Wichtige technische Daten: Low-pressure part 1-stage Fan+2-stage IPC+2-stage LPT, Core part 1-stage Centrifugal HPC+ Annular reflux combustion chamber+1-stage HPT, Exhaust Mixed exhaust, simply converge nozzle, Take-off Thrust ( kgf) 700, Cruising SFC kg/(kgf.h) 0.75, Bypass Ratio 2.15, Total Pressure Ratio 11.0, Turbine Inlet Temp K( C) 1313(1040), Dry Weight（kg） 135, Size(diameter/length) （mm） 472/1450.
Technische Daten — 1 groups
Wichtige technische Daten: Low-pressure part 1-stage Fan+2-stage IPC+2-stage LPT, Core part 1-stage Centrifugal HPC+ Annular reflux combustion chamber+1-stage HPT, Exhaust Mixed exhaust, simply converge nozzle, Take-off Thrust ( kgf) 700, Cruising SFC kg/(kgf.h) 0.75, Bypass Ratio 2.15, Total Pressure Ratio 11.0, Turbine Inlet Temp K( C) 1313(1040), Dry Weight（kg） 135, Size(diameter/length) （mm） 472/1450.
Technische Daten
Specifications
- Low-pressure part
- 1-stage Fan+2-stage IPC+2-stage LPT
- Core part
- 1-stage Centrifugal HPC+ Annular reflux combustion chamber+1-stage HPT
- Exhaust
- Mixed exhaust, simply converge nozzle
- Take-off Thrust ( kgf)
- 700
- Cruising SFC kg/(kgf.h)
- 0.75
- Bypass Ratio
- 2.15
- Total Pressure Ratio
- 11.0
- Turbine Inlet Temp K( C)
- 1313(1040)
- Dry Weight（kg）
- 135
- Size(diameter/length) （mm）
- 472/1450
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