Foldable-Wing Anchor Assembly for Extreme Seabed Loads

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Solution Overview

Problem

Existing anchor assemblies are unable to withstand extreme loads and lack sufficient resistance force, security, and adaptability to varying seabed conditions, with wings often failing to deploy properly due to seabed hardness or becoming damaged.

Innovation Solution

An anchor assembly with foldable wings hinged in recesses, featuring a main support element and additional support elements that lock into position using a disc-shaped locking plate and lock block, reinforced by concrete filling, ensuring wings remain deployed and resistant to extreme loads.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If wings are arranged on the surface of the pile, then the anchor assembly can provide resistance force, but the wings may not deploy properly due to seabed hardness or mass aggregation

Engineering Contradiction:
Improvewing deployment reliabilityVSAvoidseabed resistance to deployment
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The wings are nested inside the hollow pile body during installation, protected from seabed interference. Upon retrieval, the wings are deployed outward from the nested position, ensuring they are not blocked by seabed masses or hardness during the critical deployment phase.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Strength

If the pile is inserted further down into the seabed, then the anchor assembly may achieve better anchoring, but the wings will not deploy due to firm seabed

Engineering Contradiction:
Improveanchoring strengthVSAvoidwing deployment
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The wings are pre-positioned inside the hollow pile body in a compact, protected state before installation. This preliminary positioning ensures they remain undamaged during insertion to any depth. The deployment action is then performed during retrieval when the seabed constraint is removed, allowing wings to expand freely regardless of insertion depth.

Inventive Principle:
Principle #10Preliminary action

3Force

If wings are arranged on the pile surface, then they can provide resistance force, but the fastening point may be damaged during insertion

Engineering Contradiction:
Improveresistance forceVSAvoidfastening point integrity
Core Design Contradiction:
ForceVSStrength

Solution Approach 1:

The wings are nested within the hollow pile body during the high-stress insertion phase, protecting their fastening points from damage. The wings are only deployed after insertion is complete, at which point the fastening points have already withstood the insertion forces without damage.

Inventive Principle:
Principle #7Nested doll (Nesting)

4Shape

If wings are arranged on the surface of the pile, then they can deploy outward, but they cannot exhibit an angle larger than maximum 45 degrees

Engineering Contradiction:
Improvewing angleVSAvoidretention capability
Core Design Contradiction:
ShapeVSStrength

Solution Approach 1:

The wings transition from a constrained single-dimensional arrangement on the pile surface to a multi-dimensional deployment where they can extend outward at various angles and positions. The hollow pile body provides three-dimensional space for the wings to achieve optimal angles greater than 45 degrees relative to the pile axis, significantly increasing retention capability.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Data Source

PatentUS12448749B2Anchor assembly
Publication Date: 2025.10.21 HASSAVARI NADER
  • US12448749B2 patent drawing
  • US12448749B2 patent drawing
  • US12448749B2 patent drawing

AI summary

Anchor assembly for arrangement in seabed comprising a main tube provided with foldable wings movably arranged in recesses of the main tube by being hinged in upper end of the recesses, which wings in initial position is aligned with outer surface of the main tube, where the foldable wings are provided with a centered curved main support element extending in a plane perpendicular to inner surface of the wing and wherein rear part of the main support element is provided with a notch, constriction or recess determining the number of degrees the wing is to exhibit in relation to the main tube in deployed state.