Kite Launch System with Propelled Support Frame

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Solution Overview

Problem

Current kite designs for wind power generation systems face challenges in meeting demanding wing load and longevity requirements, affecting efficiency and reliability, particularly in launch and retrieval operations at low wind speeds.

Innovation Solution

The system incorporates a second kite support frame with a propulsion system, including propellers, and a launch and retrieve system with guide apertures for main traction cables, optimizing the launch and retrieval process for improved reliability and efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If structural re-enforcements are added to meet wing load and longevity requirements, then reliability is improved, but weight increases which deteriorates launch ability at low wind speed

Engineering Contradiction:
Improvekite assembly reliabilityVSAvoidkite assembly weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The system divides the launch and retrieval function into two separate support frames: a first support frame for stable ground-based cable guidance, and a second support frame with propulsion system for aerial launch and retrieval operations. This segmentation allows the kite assembly to be lighter while the support infrastructure provides the necessary stability and guidance functions.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The second kite support frame with propulsion system acts as an intermediary device that assists in launching and retrieving the kite assembly. The propulsion system provides the additional force needed for launch without requiring the kite itself to be heavily reinforced, thereby maintaining light weight while improving reliability during critical operations.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Device complexity

If a single support frame is used, then device complexity is reduced, but launch and retrieval reliability deteriorates

Engineering Contradiction:
Improvesupport frame complexityVSAvoidlaunch and retrieval reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The support frame system is segmented into two specialized frames: the first support frame handles ground-based cable guidance with guide apertures, while the second support frame provides aerial positioning with propulsion system. This functional segmentation improves launch and retrieval reliability by distributing tasks across specialized components.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Each support frame is designed with multi-functionality to justify the increased complexity. The first support frame provides stable ground mounting and cable guidance through guide apertures. The second support frame combines aerial positioning, propulsion system operation, and cable guidance capabilities. This multi-functionality ensures that each component contributes to overall system reliability.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Ease of operation

If propulsion system is added to second support frame, then launch ability at low wind speed is improved, but device complexity increases

Engineering Contradiction:
Improvelaunch abilityVSAvoidsupport frame complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The propulsion system is localized to the second kite support frame, which is specifically designed for aerial operations requiring active positioning. The first support frame maintains a simpler ground-based design with guide apertures for cable guidance. This local differentiation of complexity allows the propulsion capability to be added only where needed for launch operations.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The propulsion system on the second support frame performs preliminary actions by positioning the support frame and guiding the cables through guide apertures before the kite assembly is launched. This preliminary positioning and cable guidance setup creates optimal conditions for launch at low wind speeds, reducing the operational complexity during the actual launch event.

Inventive Principle:
Principle #10Preliminary action

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 configuration enhances the launch and retrieval operations, ensuring better efficiency and reliability of the kite assembly, enabling effective power generation even at low wind speeds by providing vertical lift and precise control.

Implementation Method 1

The propulsion system comprises a plurality of propellers attached to the second kite support frame

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Implementation Method 2

The propulsion system comprises a plurality of propellers attached to the second kite support frame for positioning the second kite support frame in combination with the kite assembly in a position remote from the first kite support frame

Methodology Applied
Scientific EffectPropeller thrust: Impeller

Implementation Method 3

a kite assembly connected to the generator via one or more (e.g. two) main traction cables

Methodology Applied
Scientific EffectTension: Tension

Data Source

PatentEP3224472B1Wind power generation system and method of operating the same
Publication Date: 2021.06.30 KITEMILL AS
  • EP3224472B1 patent drawingFigure 1
  • EP3224472B1 patent drawingFigure 2
  • EP3224472B1 patent drawingFigure 3

AI summary

Wind power generation system comprising a ground control unit (2) with a generator (3), a kite assembly (10) connected to the generator (3) via one or more main traction cable (5), and a launch and retrieve system (6). The launch and retrieve system (6) comprises a first kite support frame (7) provided with guide apertures (7a, 7b) for each main traction cable (5), and a second kite support frame (8) provided with guide apertures (8a, 8b) for each traction cable (5). The second kite support frame (8) comprises a propulsion system (9) for positioning the second kite support frame (8) in combination with the kite assembly (10) in a position remote from the first kite support frame (7).