Aircraft Float Turbulators and Foam Core Structure

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Solution Overview

Problem

Current seaplane float designs face challenges such as resistance to disengagement from calm water due to suction effects, increased takeoff distance, reduced maximum takeoff weight, and decreased cargo capacity due to heavy float skins, as well as inadequate impact energy absorption during landings and crashes.

Innovation Solution

Integration of turbulators on the water-contacting surface of the float to create turbulence, reducing suction effects and allowing for easier takeoff, and a longitudinally extending support structure to reduce float skin thickness and weight while maintaining structural integrity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a thick float skin is used to maintain hull stiffness and prevent stress fractures, then the structural strength and reliability are improved, but the float weight increases significantly, reducing cargo capacity

Engineering Contradiction:
Improvehull stiffnessVSAvoidfloat weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The float skin is segmented into a thin outer skin and an attached foam core structure. The foam core provides structural stiffness and strength while the thin skin reduces weight. This segmentation allows the float to maintain hull stiffness without requiring a thick solid skin, thereby reducing overall float weight and increasing cargo capacity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The float employs a composite structure combining a thin skin material with a foam core. This composite construction provides the structural integrity and stiffness of a thick skin while maintaining the weight advantages of a thin skin, resolving the contradiction between strength requirements and weight reduction goals.

Inventive Principle:
Principle #40Composite materials

2Ease of manufacture

If conventional smooth float surfaces are used, then manufacturing simplicity is maintained, but suction effects during takeoff increase, making takeoff difficult from calm water

Engineering Contradiction:
Improvefloat surface manufacturingVSAvoidtakeoff performance
Core Design Contradiction:
Ease of manufactureVSEase of operation

Solution Approach 1:

The smooth mechanical surface is replaced with a textured surface featuring turbulators. These turbulators create controlled turbulence in the water boundary layer, reducing suction effects during takeoff. The substitution maintains manufacturing feasibility while dramatically improving takeoff performance from calm water surfaces.

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

Solution Approach 2:

The surface characteristics of the float are changed from smooth to textured with specific turbulator patterns. This parameter change in surface roughness and geometry creates beneficial flow patterns that reduce adhesion to calm water, improving ease of operation during takeoff without significantly complicating manufacturing.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If heavy landing gears are integrated into the floats, then the ability to land on paved runways is improved, but the aircraft weight increases, reducing maximum takeoff weight and fuel economy

Engineering Contradiction:
Improvelanding capabilityVSAvoidaircraft weight
Core Design Contradiction:
Adaptability or versatilityVSWeight of moving object

Solution Approach 1:

The float structure incorporates a thin skin with attached foam core that provides structural support for landing gear integration without requiring excessive weight. The foam core acts as a lightweight structural element that can support landing gear loads, enabling paved runway capability while minimizing weight penalty compared to traditional heavy float skin designs.

Inventive Principle:
Principle #30Flexible shells and thin films

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 level and safer takeoffs from calm water, increases payload capacity, and improves impact energy absorption during landings, reducing the risk of damage to the aircraft and passengers.

Implementation Method 1

a plurality of turbulators located at a water contacting surface of the float body. The turbulators create turbulence in the water

Methodology Applied
Scientific EffectTurbulence: Turbulence

Implementation Method 2

This resistance is due to a suction-type effect of the water on the aircraft float which is caused by the surface tension of the water acting on the float

Methodology Applied
Scientific EffectSurface tension: Surface Tension

Data Source

PatentUS11104433B2Aircraft float
Publication Date: 2021.08.31 BANGLE DAVID
  • US11104433B2 patent drawing
  • US11104433B2 patent drawing
  • US11104433B2 patent drawing

AI summary

An aircraft float includes a float body configured to provide buoyancy to an aircraft, and a lower portion of the float body is configured to contact water. The lower portion of the float body includes a turbulator.