Electronic Ignition
Processor-controlled electronic ignition systems designed for two- and four-stroke engines across aviation, UAV, ULL and specialized aircraft applications. The system architecture prioritizes reliable starting, stable engine operation and predictable behaviour under varying operating conditions.
Product Description
The electronic ignition system is designed for engines ranging from single-cylinder up to multi-cylinder configurations. Reliability, compact form factor and low weight were primary design objectives, making the system suitable for integration into airborne platforms where space, mass and operational stability are critical.
The ignition architecture supports configurable setups based on engine type, application profile and operational requirements. System behaviour is designed to remain predictable across temperature ranges, operating loads and long-term use.
Detailed functions and specifications are available in our documentation.
Functions
Ignition functionality can be configured to meet specific customer and application requirements.
engine start monitoring
safety shutdown in case of unintended engine behaviour
acoustic state indication
automatic system shutdown after defined standby time
internal electronic RC switch
support for partial ignition shutdown in dual-ignition configurations
Technical Parameters
Technical parameters are defined based on engine type and specific application requirements. Each system configuration is optimized to achieve stable ignition performance while minimizing electrical and thermal load.
Input Voltage is typically: 5 - 15V
VN endings for spark plugs
¼-32
CM-6
BMR6F
BMR6A
We offer the following ignition types:
Single-cylinder ignition
Dual single-cylinder ignition
Twin-cylinder ignition
Dual twin-cylinder ignition
Four-cylinder ignition
Dual four-cylinder ignition
Five-cylinder ignition – radial engines
Seven-cylinder ignition – radial engines
