Thruster Power System Segmentation and Energy Storage

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Solution Overview

Problem

Conventional offshore drilling rig systems face challenges in managing transient and steady-state electric loads, requiring significant excess thruster capacity and complex testing to ensure reliability, which increases costs and complexity due to the need for multiple combustion generators and complex electrical coupling.

Innovation Solution

The thruster electric power system includes a DC electric power bus, DC-to-AC converters, energy storage units such as kinetic generators, batteries, and supercapacitors, which allow for independent operation of thrusters and auxiliary loads during power failures, reducing the need for excess capacity and simplifying testing by enabling thruster operation from energy storage during emergencies.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple combustion generators with complex electrical coupling are used to ensure reliability during transient loads, then system reliability is improved, but device complexity and cost increase

Engineering Contradiction:
Improvepower system reliabilityVSAvoidelectrical coupling complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent segments the power system into separate DC and AC domains with independent power paths. The DC electric power bus serves thrusters independently from the AC bus that serves auxiliary loads, eliminating complex electrical coupling between combustion generators and reducing system complexity while maintaining reliability

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces energy storage units as intermediaries between the AC power bus and DC thruster bus. These energy storage units decouple the thruster power path from the combustion generators, simplifying the electrical coupling architecture while ensuring reliable power delivery during transient conditions

Inventive Principle:
Principle #24Intermediary (Mediator)

2Power

If excess thruster capacity is installed to handle transient loads, then power delivery capability is improved, but device complexity and cost increase

Engineering Contradiction:
Improvethruster power capacityVSAvoidsystem configuration complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The patent implements energy storage units that are pre-charged during normal operation to store energy in advance. During transient load conditions, these pre-charged energy storage units immediately discharge to supplement thruster power, eliminating the need for excess thruster capacity while maintaining power delivery capability

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent changes the operational parameters of the power system by introducing a DC electric power bus that operates independently from the AC bus. This parameter change allows thrusters to draw power directly from energy storage units during transients, reducing the required thruster capacity while simplifying system configuration

Inventive Principle:
Principle #35Parameter changes

3Reliability

If complex testing procedures are implemented to ensure thruster reliability, then system reliability is improved, but loss of time and cost increase

Engineering Contradiction:
Improvethruster operation reliabilityVSAvoidtesting time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent designs the power system with inherent reliability features through the DC bus architecture and energy storage integration. The system's modular design and independent power paths provide natural fault isolation and continued operation capability, reducing the need for extensive external testing while maintaining high reliability

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This solution reduces the number of thrusters disabled by a single failure, decreases the required excess thruster capacity, and simplifies testing by allowing thruster operation from energy storage units, enhancing reliability and reducing costs.

Implementation Method 1

one or more energy storage units electrically coupled to the thruster DC electric power bus

Methodology Applied
Scientific EffectBattery energy storage: Battery (electricity)

Implementation Method 2

the one or more energy storage units include at least one of a battery storage subsystem and a supercapacitor

Methodology Applied
Scientific EffectSupercapacitor energy storage: Capacitance

Implementation Method 3

one or more thruster direct current to alternating current (DC-to-AC) converters configured to electrically couple a respective electric thruster to the thruster DC electric power bus

Methodology Applied
Scientific EffectPower conversion:

Implementation Method 4

a first transformer electrically coupled to a first alternating current (AC) electric power bus

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Data Source

PatentUS11682907B2Thruster electric power systems and associated methods
Publication Date: 2023.06.20 NOBLE DRILLING AS
  • US11682907B2 patent drawing
  • US11682907B2 patent drawing
  • US11682907B2 patent drawing

AI summary

A mobile offshore drilling unit includes a plurality of electric thrusters to dynamically position the drilling unit, and a microgrid electric power generation system for providing power to the plurality of electric thrusters, the microgrid electric power generation system including at least one combustion generator electrically coupled to a main electric power bus and at least one thruster electric power system, the thruster electric power system including a thruster electric power bus, an additional electric power bus connected to the thruster electric power bus via an interface device, and a circuit breaker electrically coupling the additional electric power bus to a main electric power bus for isolating the thruster electric power bus from the main electric power bus in case of loss of power on the main electric power bus.