CTF-9 Turbofan Engine（400kgf）(TRDD-50 A Turbofan Engine)
SKU: MD-P00591·Spare Parts & Components·受注生産
概要
CTF-9 turbofan engine (TRDD-50 A turbofan engine) is an engine with the thrust of 400kg and dual rotors turbofan independently developed by China, which is used for small high-speed UAV. With the outstanding characteristics of high performance and compact structure, the engine is equipped with advanced electrical, control and health management, and can meet the power needs of small UAV with high elevation and large range. Main performance indicators Flying Mach number: 0~0.9 Maximum take-off thrust of engine: 400kgf (H=0, Ma=0, ISA) Engine fuel rate: 0.65kg/ (kgf. h) (H=0, Ma=0, 1SA) Engine inlet diameter/outer diameter: 279mm/330mm Weight: 82kg (body net weight) Cycle of the first restoration :500h Power supply capacity :8kW
技術仕様
Specifications. 主な仕様： Ceiling 12.5km、Flying Mach number 0~0.9、Maximum take-off thrust of engine 400kgf (H=0, Ma=0, ISA)、Engine fuel rate 0.65kg/ (kgf. h) (H=0, Ma=0, 1SA)、Engine inlet diameter/outer diameter 279mm/330mm、Engine length 855mm、Weight 82kg (body net weight)、Cycle of the first restoration 500h、Power supply capacity 8kW。
技術仕様 — 1 groups
主な仕様： Ceiling 12.5km、Flying Mach number 0~0.9、Maximum take-off thrust of engine 400kgf (H=0, Ma=0, ISA)、Engine fuel rate 0.65kg/ (kgf. h) (H=0, Ma=0, 1SA)、Engine inlet diameter/outer diameter 279mm/330mm、Engine length 855mm、Weight 82kg (body net weight)、Cycle of the first restoration 500h、Power supply capacity 8kW。
技術仕様
Specifications
- Ceiling
- 12.5km
- Flying Mach number
- 0~0.9
- Maximum take-off thrust of engine
- 400kgf (H=0, Ma=0, ISA)
- Engine fuel rate
- 0.65kg/ (kgf. h) (H=0, Ma=0, 1SA)
- Engine inlet diameter/outer diameter
- 279mm/330mm
- Engine length
- 855mm
- Weight
- 82kg (body net weight)
- Cycle of the first restoration
- 500h
- Power supply capacity
- 8kW
対応機体
この部品は以下のプラットフォームに対応します。
適合データの準備中です。機体の型番をお知らせください。