FIELD: aviation.
SUBSTANCE: invention relates to a method for determining the thermal mode of operation of aircraft on-board equipment to prevent overheating and subsequent failure of the equipment system of a single-engine aircraft as a whole or its individual units. The method for determining the aircraft heat balance includes collecting data from sensors of the fuel system, air conditioning system, hydraulic circuit, generator oil system, liquid cooling system. The received data is processed in the analysis and calculation unit. In the process of collecting data from systems, failure situations are simulated both in real time and according to predetermined attributes with individual or simultaneous failures of several elements or systems. As a result of processing and software analysis of the obtained data, the algorithms or technical solutions of aircraft systems are corrected, in particular, thermal-hydraulic and design parameters.
EFFECT: removing heat from hydraulic systems, oil systems, air cooling systems, liquid cooling systems, ensuring the heat balance of the aircraft as a whole.
6 cl
Title | Year | Author | Number |
---|---|---|---|
GAS TURBINE ENGINE COMPRESSOR FUEL SUPPLY AND MECHANIZATION SYSTEM | 2023 |
|
RU2821280C1 |
DEVICE TO CONTROL OIL SYSTEM OF GAS-TURBINE | 2004 |
|
RU2287074C2 |
COMPLEX AIR CONDITIONING SYSTEM OF THE AIRCRAFT | 2017 |
|
RU2682758C1 |
INTEGRATED ONBOARD EQUIPMENT SET OF DIFFERENT ARCHITECTURE | 2015 |
|
RU2592193C1 |
AIR CONDITIONING SYSTEM FOR SUPERSONIC CIVIL AIRCRAFT | 2024 |
|
RU2840887C1 |
METHOD OF CONTROLLING A GAS TURBINE ENGINE AT ABORTED TAKEOFF OF AN AIRCRAFT | 2024 |
|
RU2837365C1 |
METHOD OF AND DEVICE FOR OPERATION OF AIRCRAFT EQUIPMENT DEPENDING ON ITS STATE | 2004 |
|
RU2318703C2 |
METHOD OF CONTROLLING AIR BYPASS FROM LOW-PRESSURE COMPRESSOR OF TURBOJET TWO-SHAFT ENGINE WITH HIGH BYPASS RATIO | 2024 |
|
RU2836207C1 |
DEVICE FOR MONITORING AUTOMATIC CONTROL SYSTEM OF FLYING VEHICLE FUEL SYSTEM | 2005 |
|
RU2287457C1 |
METHOD OF PROTECTING GAS TURBINE ENGINE AGAINST SPINNING OF ROTORS IN CASE OF FIRE | 2023 |
|
RU2825767C1 |
Authors
Dates
2023-09-11—Published
2022-12-28—Filed