FIELD: measurement and testing.
SUBSTANCE: group of inventions relates to a method and a system for diagnosing the technical state of a hybrid power plant of a light aircraft. In order to diagnose the technical state, certain parameters of the internal combustion engine and parameters of the electric motor, temperature of the storage battery are monitored and compared with preset values using a digital twin. System comprises ground and on-board hardware units connected by means of a telemetric communication channel and equipped with means of creating and operating a digital twin.
EFFECT: enabling increase of functionality and reliability of detecting a malfunction in the hybrid power plant.
6 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CYBER-PHYSICAL SYSTEM FOR RESEARCH OF FLIGHT CHARACTERISTICS OF AIRCRAFT | 2023 |
|
RU2804548C1 |
| HYBRID MULTI-ROTOR FLYING PLATFORM | 2019 |
|
RU2710968C1 |
| CONTROL SYSTEM AND TRANSFER OF ROTARY MOMENT TO SCREW(S) IN UNMANNED AERIAL VEHICLES (UAV), STARTER-GENERATOR, STARTER-GENERATOR CONTROL BOARD AND SHOCK ABSORBER FOR THIS SYSTEM | 2020 |
|
RU2741136C1 |
| CYBER-PHYSICAL SYSTEM FOR STUDYING STRENGTH CHARACTERISTICS OF AIRCRAFT | 2023 |
|
RU2804550C1 |
| CYBERPHYSICAL SYSTEM FOR SYNTHESIS OF DIGITAL TWIN OF AIRCRAFT | 2023 |
|
RU2809462C1 |
| METHOD OF ACCUMULATION AND STABILIZATION OF THE VOLTAGE GENERATED BY A BRUSHLESS GENERATOR AS A PART OF HYBRID SYSTEM | 2018 |
|
RU2708118C1 |
| FLIGHT INFORMATION COLLECTION AND PROCESSING SYSTEM FOR AIRCRAFT DIGITAL TWIN VALIDATION DURING FLIGHT TESTS | 2022 |
|
RU2780244C1 |
| HYBRID JET-TURBINE AIRCRAFT ENGINE | 2012 |
|
RU2511829C2 |
| UNMANNED AERIAL VEHICLE AND THE METHOD OF ITS OPERATION | 2013 |
|
RU2653324C2 |
| SMALL-SIZED ON-BOARD RADIO-ELECTRONIC DEVICE FOR CONTROLLING THE FLIGHT AND NAVIGATION COMPLEX OF AN UNMANNED AERIAL VEHICLE | 2021 |
|
RU2799748C2 |
