FIELD: aircraft engineering.
SUBSTANCE: device for power supply of a tethered unmanned aerial vehicle contains a ground power source, a power cable, two onboard step-down converters, a supervisory PWM controller, and two error signal generators.
EFFECT: increase in the efficiency of the power supply of the aircraft is provided.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR POWER SUPPLY OF TETHERED UNMANNED AERIAL VEHICLES | 2022 |
|
RU2782733C1 |
| ELECTRICAL SUPPLY SYSTEM FOR TETHERED AIRCRAFT | 2022 |
|
RU2782805C1 |
| TETHERED DRONE POWER SUPPLY DEVICE | 2023 |
|
RU2815590C1 |
| DEVICE FOR POWER SUPPLY OF TETHERED AIRCRAFT | 2019 |
|
RU2711325C1 |
| DEVICE FOR USING ENERGY RECOVERY WHEN POWERING ENGINES OF TETHERED HIGH-ALTITUDE UNMANNED AERIAL VEHICLES | 2022 |
|
RU2792311C1 |
| METHOD OF FIXED BALLOON POWER SUPPLY AND DEVICE TO THIS END | 2010 |
|
RU2449927C2 |
| MULTIROTOR UNMANNED AERIAL VEHICLE POWER SUPPLY DEVICE | 2022 |
|
RU2792109C1 |
| AIRCRAFT POWER SUPPLY METHOD AND DEVICE (VERSIONS) | 2013 |
|
RU2554723C2 |
| METHOD FOR REMOTE WIRE POWER SUPPLY OF FACILITIES | 2014 |
|
RU2572822C1 |
| TETHERED MONITORING PLATFORM WITH POWER SUPPLY SYSTEM | 2019 |
|
RU2724509C1 |
