FIELD: transport.
SUBSTANCE: invention relates to power engineering and may be used in power controller 1 design to control aircraft hydride power source. Power controller 1 allows measuring power demand of consuming hardware 2. Said device 1 allows determining first operating characteristic of first power source 3 and second operating characteristic of second power source 4. First power source 1 and second power source 4 serves to generate first and second required portions of necessary demand.
EFFECT: efficient supply of power to consuming hardware.
14 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL CELL SYSTEM FOR SUPPLYING TRANSPORTATION VEHICLE WITH DRINKING WATER AND OXYGEN AND USE THEREOF | 2006 |
|
RU2406186C2 |
| SYSTEM OF FUEL ELEMENTS FOR EMERGENCY POWER SUPPLY | 2006 |
|
RU2393592C2 |
| SYSTEM OF FUEL ELEMENTS AND WATER SUPPLY SYSTEM FOR AIRCRAFT, WHICH CONTAINS IT | 2006 |
|
RU2428770C2 |
| SYSTEM AND METHOD OF FIRE FIGHTING | 2006 |
|
RU2410143C2 |
| SYSTEM AND METHOD OF FIRE PROTECTION | 2006 |
|
RU2411972C2 |
| SYSTEM AND METHOD OF FIRE PROTECTION | 2006 |
|
RU2565493C2 |
| SYSTEM AND METHOD OF AIRCRAFT POWER SUPPLY | 2005 |
|
RU2405720C2 |
| METHOD FOR OPTIMISATION OF TOTAL ENERGY EFFICIENCY OF AIRCRAFT AND MAIN POWER GROUP FOR IMPLEMENTATION | 2011 |
|
RU2585394C2 |
| METHOD AND SYSTEM FOR POWER CONTROL IN CASE OF AT LEAST ONE AIRCRAFT ENGINE FAILURE | 2012 |
|
RU2608784C2 |
| INERT GAS GENERATOR FOR AIRCRAFT FUEL TANK INERTING SYSTEM AND INERTING METHOD | 2019 |
|
RU2800468C2 |
