として リチウムイオン電池専門メーカー、UFOPOWERと開発者が協力 AUV電池, ROV電池および世界各地の水中ロボット動力システム。バッテリシステムは、船体や推進システムが最終的に決定された後に選択されるコンポーネントではなく、水中ロボットを開発する際に考慮すべき最初のシステムの1つです。蓄電池の電圧は推進システムと電力電子機器に影響を与える。容量はタスク時間、重量、浮力に影響します。rsquo；s電気及び機械構造。

ウッズホール海洋研究所は、より強い圧力ケーシングは重量を増加させ、より大きな浮力を必要とし、車両のエネルギー消費を増加させる可能性があると指摘している。これは、多くのAUV、バッテリに電力を供給するROV、水中推進器、水中設備の開発者が必要とするのは、標準的なバッテリパックだけではない理由です。バッテリ選択、電気アーキテクチャ、BMS開発、構造統合、テスト、および生産計画に参加できるバッテリパートナーが必要です。

セルモデルではなくタスクの概要から開始

バッテリ項目は問題から始めるべきではありません。ldquo；18650個の電池を使うべきですか、21700個の電池を使うべきですか。&；rdquo；水中ロボットから始めなければなりませんrsquo；という使命があります。エンジニアリングチームは、まず次のことを理解する必要があります。

• 車両タイプとアプリケーション

• ターゲットタスク期間

• 巡航と最高速度

• 公称および最大システム電圧

• へいきんうんてんでんりょく

• 連続電流とピーク電流

• 内部電池セルサイズ

• 動作温度と充電温度

• 目標深さと圧力シェル設計

• 充電、ドッキング、バッテリ交換方法

• 通信プロトコル

• 基地への帰還または緊急路面備蓄の要求

構築された研究車両では、エネルギーとタスク性能との関係が見られる。ウッズホール海洋研究所、rsquo；ABE自主水中航行器は5キロワット時のリチウムイオン電池システムを携帯し、任務に応じて約210-300ワットを消費し、20-40キロの作業範囲と14-20時間の任務継続時間をサポートする。車両と、rsquo；ldquo；ホテル負荷と、rdquo；これはエネルギー予算に含めなければならない。

したがって、同じ公称電圧を使用する2つの水中ロボットは、非常に異なる電池を必要とする可能性があります。次の表では、一般的な車両タイプのバッテリ優先度を比較します。

円筒型電池または袋型電池：どのフォーマットがこのプロジェクトに適していますか？

18650や21700などの円筒電池は標準化されており、モジュール化された組み立てが容易で、広く利用可能である。これらの固定サイズは購入を簡単にすることができますが、高容量バッテリパックには多くのバッテリ、溶接、電流経路、機械的支持が必要になる場合があります。袋型電池は、使用可能な空間の周りで容量、厚さ、幅、長さを調整することができます。これらは、狭いモジュール、セグメントパック、または円筒形圧力シェル内の大容量単電池部分に配列することができる。

Cell-format research (University of Bologna) shows that cylindrical, prismatic, and pouch formats create different tradeoffs in packaging efficiency, thermal behavior, mechanical support, manufacturing, and system-level energy density. No format is automatically best for every vehicle:

UFOPOWER’s main advantage is not commodity cylindrical-cell supply. It is the ability to develop high-energy and high-power pouch solutions. The company’s semi-solid-state portfolio covers selected energy-density platforms from 300 to 380 Wh/kg, while its broader cell portfolio includes high-discharge-rate, LiHV, low-temperature, custom-shaped, and LiFePO4 options. The final value at pack level will be lower after adding the BMS, connector, wiring, enclosure, and mechanical protection.

LiFePO4 may be considered when thermal stability and service life are more important than minimum weight. Tests presented at the NASA Aerospace Battery Workshop found lower maximum temperatures for the evaluated LFP batteries than for the evaluated NMC batteries under thermal-runaway conditions, while also showing that module layout and heat-transfer paths strongly influence the complete pack response.

How Series and Parallel Configuration Affects the Robot

Series and parallel configuration connects cell characteristics to vehicle-level voltage, capacity, and power. Cells connected in series increase pack voltage while retaining the capacity of one series string. Cells connected in parallel increase amp-hour capacity and distribute current across multiple cells. Research on lithium-ion module configurations (U.S. Department of Energy) shows that series-parallel architecture affects current distribution, voltage spread, energy throughput, and degradation behavior, especially when cells are not perfectly matched.

For example:

• A 6S standard lithium battery has a nominal voltage of approximately 22.2 V.

• A 12S standard lithium battery has a nominal voltage of approximately 44.4 V.

• Two 30 Ah strings connected in parallel provide a nominal capacity of 60 Ah, provided the cells and current paths are properly matched.

Electrical power follows P = V × I. For the same required power, a higher-voltage system can operate at a lower current. This can reduce resistive losses in cables and connectors, because those losses increase with the square of current (P loss = I²R). Higher voltage is not automatically better — it may require a higher-voltage motor controller, charger, BMS, insulation system, contactor, and connector. More parallel cells can increase capacity and output capability, but they also add weight, volume, interconnections, and cell-consistency requirements. The correct architecture should be determined together with the propulsion system, control electronics, charger, connector, and available housing space.

Capacity Is Not the Same as Mission Endurance

Battery capacity is normally stated in amp-hours, but underwater robot energy should also be evaluated in watt-hours: Energy (Wh) = Nominal Voltage (V) × Capacity (Ah). Mission time depends on usable energy, not Ah alone. The energy model must include propulsion, onboard computers, cameras, lights, sonar, communications, manipulators, pumps, and other auxiliary loads. Vehicle speed, water current, hydrodynamic drag, motor efficiency, temperature, aging, and the required recovery reserve also affect the result.

A practical preliminary estimate is: Required Energy = (Average Power × Mission Time) ÷ (Usable Depth of Discharge × System Efficiency). An engineering reserve should then be added for return, surfacing, unexpected currents, route changes, and battery aging. Long-range AUV research (NOAA Institutional Repository) treats endurance, route planning, navigation, and data transfer as connected system-level constraints rather than independent specifications.

Cold water must also be included in the calculation. Lithium-ion batteries can lose available capacity and power at low temperatures because ion transport slows and internal resistance increases. Laboratory research supported by Purdue University and the U.S. Department of Energy documented substantial capacity reductions as test temperature decreased, showing why room-temperature capacity cannot be used as the only basis for cold-water mission planning.

Design for Continuous Power, Peak Current, and Voltage Sag

An underwater robot rarely operates at one constant current. Cruising may create a moderate load, while thruster startup, rapid maneuvering, station keeping in strong currents, manipulator movement, or simultaneous tool operation can produce short power peaks. The battery specification should distinguish:

• Average current

• Continuous current

• Peak current

• Peak duration

• Minimum acceptable system voltage

• Maximum BMS and connector temperature

A battery may have sufficient nominal capacity but still fail to support the propulsion system if its internal resistance is too high. A large current pulse can pull the terminal voltage down far enough to reduce thruster performance, trigger BMS protection, or restart vehicle electronics. Research on underwater thruster control has specifically identified battery voltage sag as a factor that can limit available thruster output. Power capability must therefore be checked across the complete current path: cell, busbar, weld, fuse, BMS, cable, connector, and motor controller. Charge rate, discharge rate, temperature, and calendar time also affect battery degradation, which is why DNV recommends controlled and transparent cell-testing methods when comparing battery performance (DNV-RP-0577).

UFOPOWER’s high-rate pouch-cell and industrial UAV experience provides a useful engineering base for underwater thrusters and battery-powered ROVs. Both applications involve motor loads, high current, voltage stability, connector heating, and limited weight. The actual discharge rate still needs to be confirmed from the robot’s measured or simulated load profile.

PACK Structure, Waterproofing, and Mechanical Protection

The cell is only one part of an underwater battery system. The pack also needs mechanical support, insulation, wiring control, BMS placement, thermal paths, sealing interfaces, and protection against vibration and impact. Cylindrical pressure housings are common because their geometry distributes external pressure efficiently. At an average seafloor depth of 3,800 meters, hydrostatic pressure is roughly 380 times atmospheric pressure at sea level. Housings for batteries and electronics must therefore be engineered around the target depth rather than treated as ordinary waterproof enclosures.

UFOPOWER has developed rugged smart battery packs for agricultural and industrial UAVs. Existing products combine BMS functions, thermal design, structured enclosures, high-current interfaces, and water-resistant construction for demanding outdoor operations. Several of these practices transfer directly to underwater projects:

• Sealing around screws and enclosure joints

• Waterproof power and data connectors

• Sealing rings around buttons and service interfaces

• Sealed cable exits with strain relief

• Internal insulation and moisture barriers

• Controlled placement of gaskets and sealing plugs

• Shock-absorbing supports around cells and circuit boards

Water resistance is not the same as deep-water qualification. Agricultural and cleaning drones primarily face rain, spray, cleaning liquids, vibration, and repeated field handling. An underwater robot must also withstand continuous immersion, hydrostatic pressure, pressure cycling, saltwater corrosion, seal compression, and long-term material aging. Waterproofing and pressure resistance should therefore be validated at the complete battery enclosure or vehicle level. The same rule applies to vibration and impact performance: experience from UAV and high-power battery packs can guide material selection and structural design, but the final underwater configuration requires project-specific testing.

Connector Design Is Part of the Power System

An underwater battery connector must be selected by more than pin count. Engineers need to consider voltage, continuous and peak current, contact resistance, wire gauge, locking method, mating cycles, corrosion resistance, sealing, and communication requirements. Power, charging, and data may use separate interfaces or a combined connector. Some systems are connected only in a dry environment, while subsea docking or service systems may require wet-mate technology. IEEE research on subsea power and data transmission treats wet-mate connection as a dedicated underwater engineering problem, not a standard extension of an exposed electrical plug.

UFOPOWER works with XT90S, AS150, AS150U, EC-series, Molex, and customized smart interfaces in UAV and industrial battery systems. These provide experience in high-current delivery, anti-spark design, locking, signal contacts, and BMS communication. A standard UAV connector should not be presented as subsea-ready unless its sealing and pressure performance have been verified for the intended environment.

BMS and Thermal Management Must Be Designed Separately

A BMS monitors and controls the battery, but it is not the complete thermal-management system. Typical BMS functions include cell-voltage monitoring, current measurement, temperature monitoring, overcharge and over-discharge protection, overcurrent and short-circuit protection, balancing, SOC estimation, fault records, and communication. NASA describes cell monitoring, charge balancing, fault detection, and overvoltage or undervoltage protection as core functions of high-voltage battery management.

Thermal management deals with how heat moves through the pack. It includes sensor placement, cell spacing, thermal pads, heat spreaders, insulation, enclosure materials, and the conduction path from the cells to the pressure housing. NASA battery research emphasizes that pack energy, series-parallel layout, charging and discharging behavior, enclosure design, operating environment, and thermal conductivity all affect the thermal solution. There is no single architecture that fits every battery pack.

Cold seawater does not guarantee that a sealed battery pack will remain cool. Heat still needs to travel from the cell through the support structure and enclosure before it can reach the surrounding water. UFOPOWER develops BMS solutions with CAN and SMBus communication, SOC indication, current detection, abnormal-event logs, balancing, temperature alarms, and charge-discharge protection. These capabilities can be adapted to a project-specific underwater robot BMS rather than simply reusing an existing UAV board unchanged.

From EVT to DVT, PVT, and Mass Production

A custom underwater battery should be developed in stages. During concept development, the team defines chemistry, voltage, capacity, power, housing space, connector architecture, BMS functions, and charging strategy. EVT prototypes verify core electrical functions and initial integration. DVT focuses on thermal behavior, vibration, shock, communication, sealing, pressure, and vehicle-level operation. PVT confirms production tooling, assembly processes, traceability, end-of-line testing, and batch consistency.

This staged approach matters because cell-level results do not fully predict module or pack behavior. NASA and UL testing has shown that module configuration and heat-dissipation paths can materially change how a complete battery responds compared with an individual cell. As a factory-direct battery manufacturer, UFOPOWER supports cell development, pack engineering, BMS, assembly, testing, and production in-house. Its R&D organization covers high-energy, high-rate, low-temperature, custom-shaped, and intelligent battery technologies, allowing the company to participate earlier than a supplier focused only on standard finished packs. The goal is a long-term engineering relationship: UFOPOWER works with customers from early platform development through validation and volume production, including projects that begin with a small engineering team and later move into commercial manufacturing.

Testing, Documentation, and Compliance Support

UFOPOWER supports common battery safety testing, transportation documentation, and market compliance requirements based on the selected battery configuration and target market. To begin an engineering evaluation, share the target voltage, capacity or energy, average power, continuous and peak current, available dimensions, operating temperature, target depth, charging method, communication requirements, development schedule, and estimated production volume. UFOPOWER can then evaluate the cell chemistry, series-parallel architecture, BMS, connector, thermal path, and mechanical pack structure as one integrated system.