Inductive Power Transfer for Aerospace Vehicles

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Solution Overview

Problem

Current inductive power transfer technologies are not suited for large aerospace vehicles as they require close proximity between the transmitter and receiver, limiting their efficiency and are primarily designed for battery charging, lacking the capability for operational power transfer, and pose risks during ground operations and in space due to physical connectors.

Innovation Solution

The development of a system that uses retractable skids, landing gear, and door frames to achieve proximity between IPT receivers and transmitters for wireless power transfer, along with the integration of IPT into vehicle fairings and umbilicals for prelaunch and space-based applications, eliminating the need for physical connectors and reducing contamination risks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Use of energy by moving object

If current IPT technologies are used for large aerospace vehicles, then wireless power transfer is achieved, but power efficiency drops significantly due to large distance between transmitter and receiver

Engineering Contradiction:
Improvepower transfer efficiencyVSAvoiddistance between transmitter and receiver
Core Design Contradiction:
Use of energy by moving objectVSLength of stationary object

Solution Approach 1:

The patent employs retractable skids that can extend and retract to dynamically adjust the distance between the IPT receiver on the aircraft and the IPT transmitter on the ground. This dynamic adjustment allows the system to maintain optimal proximity for efficient power transfer while accommodating the large size of aerospace vehicles.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The retractable skid acts as an intermediary mechanism that bridges the gap between the aircraft body and the ground-based transmitter. By providing a movable interface, it enables close proximity contactless power transfer despite the large distance that would otherwise exist between the vehicle and ground equipment.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If physical connectors are used for power transfer, then reliable power transmission is achieved, but risk to ground crew increases during inclement weather and fueling operations

Engineering Contradiction:
Improvepower transmission reliabilityVSAvoidrisk to ground crew
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent replaces mechanical physical connectors with contactless inductive power transfer technology. The IPT system uses electromagnetic fields to transmit power wirelessly between the ground-based transmitter and the aircraft receiver, eliminating the need for physical plug-and-play connections that expose ground crew to electrical hazards during weather events and fueling operations.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Use of energy by moving object

If physical connectors are used for power interfaces, then power transfer is achieved, but contamination risk increases due to dust and physical resistance

Engineering Contradiction:
Improvepower transfer capabilityVSAvoidcontamination risk
Core Design Contradiction:
Use of energy by moving objectVSObject-affected harmful factors

Solution Approach 1:

The IPT system replaces mechanical connectors that are susceptible to dust contamination and physical wear with a contactless electromagnetic power transfer mechanism. This eliminates the physical interfaces where contamination could occur, providing a cleaner and more reliable power transfer solution for aerospace applications.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Use of energy by moving object

If APU is used to generate electricity for aircraft while idling, then power supply is achieved, but fuel consumption and carbon dioxide emissions increase

Engineering Contradiction:
Improvepower supply capabilityVSAvoidfuel consumption and emissions
Core Design Contradiction:
Use of energy by moving objectVSObject-generated harmful factors

Solution Approach 1:

The patent replaces the fuel-driven APU mechanical system with an electrical power transfer system. By using IPT to deliver power wirelessly to the aircraft while idling, the system eliminates the need for combustion-based power generation, thereby removing the associated fuel consumption and carbon dioxide emissions while maintaining the aircraft's power supply capability.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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

Enables efficient wireless power transfer to large aerospace vehicles, reduces environmental impact by minimizing fuel consumption and emissions, enhances safety by eliminating physical connections, and provides reliable and contamination-resistant power interfaces for both ground and space operations.

Implementation Method 1

inductive power transfer (IPT) is currently used on technology from small appliances like electric toothbrushes and cell phones to large diesel-electric locomotives for contactless, high-efficiency battery recharging. Known also as 'resonant magnetic coupling' and 'focused power,' this description refers to IPT for wireless power transfer.

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 2

Known also as 'resonant magnetic coupling' and 'focused power,' this description refers to IPT for wireless power transfer.

Methodology Applied
Scientific EffectResonant magnetic coupling: Resonance

Data Source

PatentUS10298060B2Inductive power transfer for aerospace flight systems
Publication Date: 2019.05.21 UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR NAT AERONAUTICS & SPACE ADMINISTRATION
  • US10298060B2 patent drawing
  • US10298060B2 patent drawing
  • US10298060B2 patent drawing

AI summary

An apparatus and method of wirelessly powering an aerospace vehicle while the vehicle is on the ground is provided to solve a problem of supplying electric power for aircraft while idling on taxiways. Present systems typically require fuel-driven auxiliary power units (APU's) to generate electricity. Running APU's to power aircraft while idling requires over 443 million gallons of jet fuel annually at a cost of $1.3 billion dollars. This results in an estimated 4.7 megatons of carbon dioxide emissions annually. At the gate, shore power is provided via hardline connection.