Description
Product Overview
The TJ-120 is a compact and simple-structure turbojet engine featuring low fuel consumption and reliable operation, designed for aircraft propulsion applications. It offers excellent high-altitude and high-speed adaptability, rapid start capability, and outstanding overload resistance. A generator module can be integrated according to application requirements. The engine is capable of operating under a wide range of temperature and starting altitude conditions, uses dedicated jet fuel without the need for lubricating oil, and features optimized dimensions and weight with a qualified service life.
Key Features
- Maximum thrust ≥115 daN (sea level standard atmosphere) for aircraft propulsion
- Low specific fuel consumption ≤1.25 kg/(daN·h)
- Operates at altitudes ≥12,000 m with start altitude range of 0-5,000 m
- Lightweight design: weight ≤15 kg and diameter ≤238 mm
- Service life ≥20 h with no lubricating oil required
- Bleed air flow ≥0.12 kg/s for generator module integration
Technical Specifications
| Parameter | Value |
|---|---|
| Maximum Thrust | ≥115 daN (sea level standard atmosphere) |
| Specific Fuel Consumption | ≤1.25 kg/(daN·h) |
| Maximum Operating Altitude | ≥12,000 m |
| Weight | ≤15 kg |
| Diameter | ≤238 mm |
| Service Life | ≥20 h |
| Operating Temperature | -40°C ~ 55°C |
| Start Altitude | 0 – 5,000 m |
| Fuel | No.3 Jet Fuel |
| Bleed Air Flow | ≥0.12 kg/s |
Reviews
There are no reviews yet.