3.2Kg Tethered Drone Power 6500W 12S Onboard Power Supply 25x6.7x22cm
Tethered Drone Power: 3.2Kg, 25x6.7x22cm, 6500W, 400V d.c., 50V d.c., 130A ±1.5%, 96% Safety
| Parameters | |
| Weight | 3.2Kg |
| Measurement | 25 x 6.7 x 22cm |
| Power | 6500W |
| Input | 400V d.c. |
| Output voltage | 50V d.c. Stable Output |
| Output current | 130A |
| Auto balance | ±1.5% |
| Efficiency | 96% |
Product Specification
Product Model:MY-6.5KW12S
Product Name:6.5kw 12S Onboard Power Supply
Basic parameters
| External dimensions (including heat sink) | 250 x 220 x 60mm (including fan) |
| weights | <3.2kg |
| Housing Material | Aircraft aluminum alloy + plastic |
| rating | 6.5kw normal 7kw max. |
| Rated Input Voltage | 400VDC 420V MAX |
| Rated output | DC 12S QS10 |
| protective function | In tethered power mode, the vehicle can fly and land normally if the power supply is interrupted during flight. |
| Battery pack protection | Yes, it won't charge the pack. |
| Anti-reverse electromotive force |
| Serial number | Item | technical requirement | unit | Remarks |
| 1 | Rated Input Voltage | 400Vdc | Vdc | Fully loaded for work |
| 2 | Maximum Input Current | 18A | A | Vin=400Vdc |
| Serial number | Item | technical requirement | unit | Remarks |
| 1 | Rated output voltage | 50V DC 12S | Vdc | |
| 2 | Output Current Range | 0-130 | A | |
| 3 | Output Voltage Range | 50 | Vdc | |
| 4 | Total output power | 6500 | W | |
| 5 | efficiency | Typical 97 | % | Vin=400Vdc |
| 6 | actual output | 6300 | W |
| Serial number | Item | technical requirement | unit (of measure) | Remarks |
| 1 | Input undervoltage protection | 290 | Vdc | Output shutdown |
| 2 | overpressure protection | 420 | Vdc | Constant Voltage, Recoverable |
| 3 | overtemperature protection | 125 | ℃ | internal temperature |
| 4 | short circuit protection | Yes, recoverable | ||
| 5 | Output anti-reverse connection | Terminal Anti-Dumbing | ||
Protective properties
| Serial number | Item | technical requirement | unit (of measure) | Remarks |
| 1 | Input undervoltage protection | 290 | Vdc | Output shutdown |
| 2 | Output current limiting | 135 | A | Constant Current, Recoverable |
| 3 | overpressure protection | 55 | Vdc | Constant Voltage, Recoverable |
| 4 | overtemperature protection | 125 | ℃ | internal temperature |
| 5 | short circuit protection | Yes, recoverable | ||
| 6 | Output anti-reverse connection | Terminal Anti-Dumbing | ||
Safety Requirements
| Serial number | Item | Standard (or test condition) | Remarks | |
| 1 |
electrically resistant dissociation |
input-to-output | 4242Vdc/10mA/1min | No flying arc, no breakdown |
| Input to earth | 2121Vdc/10mA/1min | |||
| Output to earth | 1050Vdc/5mA/1min | |||
| 2 |
isolate resistive |
input-to-output | ≥100MΩ@500Vdc | Ambient temperature is 28~30℃ and relative humidity is 90%. |
| Input to earth | ≥100MΩ@500Vdc | |||
| Output to earth | ≥100MΩ@500Vdc | |||
connector
|
BAT+ / BAT-: Recommendation AS150 Connect this port to the drone's onboard battery to supply power as a backup. Vo+ / Vo-: Recommendation QS10 12S DC output port for connection to drone inputs Vin+ / Vin-: XT90 400VDC input for cables connected to terrestrial base stations |
interface definition
CON3: Inputs use XT90 connector males
| Pin 1 | VIN- | DC Input Negative |
| Pin 2 | VIN+ | DC Input Positive |
Table 4.1.3.1
CON3: Outputs use QS10 connector female connectors
| Pin 1 | Vo- | negative output |
| Pin 2 | Vo+ | output positive |
Table 4.1.3.2
CON3: Battery input using AS150 connector female connector
| Pin 1 | BAT- | Battery input negative |
| Pin 2 | BAT+ | Battery input positive |
Airborne DC power is chosen for drones for several reasons, depending on the specific requirements of the drone's mission and operational needs:
1. Extended flight times: Airborne DC power systems, such as fuel cells or generators, can provide longer flight times compared to batteries, enabling drones to operate for more extended periods without the need for frequent recharging or battery replacement.
2. Higher efficiency: DC power systems are often more efficient than alternative power sources, allowing drones to maximize their energy usage and achieve better overall performance and endurance.
3. Payload capacity: Airborne DC power solutions can be designed to offer greater power output, enabling drones to carry heavier payloads, specialized sensors, or additional equipment while maintaining adequate flight performance.
4. Rapid refueling or recharging: Some airborne DC power systems, such as fuel cells or hybrid systems, may allow for faster refueling or recharging processes, reducing downtime and increasing operational efficiency for extended missions.
5. Flexibility and scalability: DC power systems offer flexibility in design and scalability, allowing manufacturers to create drones tailored to specific requirements, such as longer flight times, increased payload capacity, or specialized mission capabilities.
6. Enhanced reliability: Compared to batteries, airborne DC power systems may offer improved reliability and reduced maintenance requirements, making them suitable for applications where consistent and high-performance drone operation is critical.
7. Mission-specific requirements: DC power systems can be tailored to meet the unique needs of specific drone applications, such as aerial surveying, industrial inspections, or long-range missions that demand extended endurance and reliable power delivery.
Overall, airborne DC power systems provide a range of performance advantages, longer endurance, and operational capabilities that make them well-suited for various drone applications where extended flight times, higher power output, and increased reliability are essential.
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