Eccentric Fastening Device for Variable Thickness Clamping

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Solution Overview

Problem

Existing blind fasteners face challenges in adjusting to varying structure thicknesses, are difficult to remove and reuse, and lack versatility in attachment to different surfaces, particularly in blind applications where inspection is not possible.

Innovation Solution

An eccentric fastening device with a base and a rotary lug that can be inserted through a hole, rotated 180 degrees, and tightened with a nut or bolt to achieve variable clamping thickness, allowing for rapid installation and removal, and adjustable attachment to constant, variable, or stepped thickness surfaces.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If existing blind fasteners are used, then attachment support is provided, but adjustment to varying structure thickness is difficult

Engineering Contradiction:
Improveadjustment to varying structure thicknessVSAvoidfastener configuration complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The fastener incorporates a rotary element that can rotate between different positions to adjust the clamping thickness. This dynamic adjustment mechanism allows the fastener to adapt to varying structure thicknesses while maintaining a relatively simple overall configuration, resolving the contradiction between adaptability and device complexity.

Inventive Principle:
Principle #15Dynamics

2Ease of operation

If existing blind fasteners are used, then attachment is achieved, but removal and reuse is difficult

Engineering Contradiction:
Improveremoval and reuse easeVSAvoidattachment security
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The fastener is divided into separable components including a rotary element, clamping element, and retention mechanism. This segmentation allows the fastener to be easily removed and reused while maintaining secure attachment during use, as each component can be independently manipulated for installation and removal without compromising attachment reliability.

Inventive Principle:
Principle #1Segmentation

3Productivity

If existing blind fasteners are used, then fastening is achieved, but installation time is excessive

Engineering Contradiction:
Improveinstallation speedVSAvoidinstallation complexity
Core Design Contradiction:
ProductivityVSEase of operation

Solution Approach 1:

The fastener components are pre-configured and pre-assembled in specific orientations before installation. The rotary element is pre-positioned and the clamping element is pre-oriented, allowing for rapid installation without complex alignment procedures. This preliminary preparation significantly reduces installation time while maintaining operational simplicity.

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

The eccentric fastening device enables rapid, secure, and reusable attachment and detachment from the top, accommodating various surface thicknesses, improving installation and removal processes while providing high strength and adaptability.

Implementation Method 1

The rotary lug includes a cylindrical portion having a thread and a head, wherein the head is offset from the cylindrical portion. The cylindrical portion is substantially axially concentric with the hole of the base, allowing the head to be eccentrically rotated on or off of the stem

Methodology Applied
Scientific EffectEccentric rotation: Eccentric

Data Source

PatentEP1957807B1Eccentric fastening device
Publication Date: 2012.10.17 THE BOEING CO
  • EP1957807B1 patent drawingFigure 1~6
  • EP1957807B1 patent drawingFigure 3~5
  • EP1957807B1 patent drawingFigure 7~10

AI summary

The eccentric fastening device (20) includes a first threaded fastener (30), a base (22) and a rotary lug (24) providing a non-fastened pre-assembled position. The base includes a top (41), a bottom (38), a stem (36) and a hole (37), where the stem axially extends from the bottom of the base, and the hole axially extends from the top through the stem of the base. The rotary lug is releasably retained in the hole of the base by the first threaded fastener. The rotary lug includes a cylindrical portion (48) having a thread (59) and a head (50), wherein the head is offset from the cylindrical portion. The cylindrical portion is substantially axially concentric with the hole of the base, allowing the head to be eccentrically rotated on or off of the stem, whereby a selective structure may be variably clamped and releasably retained between said head and said base. An aircraft having an eccentric fastening device is also provided. A method of installing the same is also provided.