Aircraft Propulsion Power Assessment via Partial Action

The patent applies partial action by testing each propulsion member individually at reduced power levels rather than requiring full take-off power testing. Each member is tested separately with other members adjusted to compensate, allowing assessment of maximum power capacity without subjecting the entire system to extreme stress conditions that would increase uncertainty or risk.

The patent enables the propulsion system to perform self-diagnosis and self-testing through automated monitoring of temperature, rotation speed, and power delivery parameters. The system automatically detects latent failures by comparing actual performance against expected performance characteristics, eliminating the need for complex manual maintenance operations requiring specialized tools and highly qualified staff.

The patent segments the propulsion system into multiple independent members (turbine engines, electric motors, propellers) that can be tested and monitored separately. By testing each member individually at manageable power levels with other members adjusted to compensate, the system can assess maximum power capacity without requiring any single member to operate beyond its rated capacity, thereby avoiding damage while ensuring overall system capability.

The patent applies partial action by distributing the maximum power testing across multiple members sequentially rather than testing all members simultaneously at full power. Each member is tested individually at its maximum capacity while other members are adjusted to compensate, achieving accurate maximum power determination without concentrating excessive stress on any single component, thereby minimizing damage risk.