Rotary Joint with Compensation Gap for Torsional Load Management

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Solution Overview

Problem

Conventional framework construction methods fail to efficiently compensate for additional torsional moments introduced into joints, leading to increased weight and material usage due to the need for local strengthening, which nullifies weight advantages.

Innovation Solution

A rotary joint design featuring concentrically nested shells with a compensation gap, where strut holding fixtures with flange portions extend between the shells, allowing sliding members to shift and neutralize bending moments, and a framework construction kit using these joints with interconnection struts and snap-fit connectors for adjustable lengths.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If cutter milled struts are used between parallel longitudinal support bars to decrease beam weight, then weight is reduced, but additional torsional moments are introduced into the attachment joints requiring local strengthening

Engineering Contradiction:
Improvebeam weightVSAvoidjoint strength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The joint is segmented into an outer shell segment and an inner shell segment that are concentrically arranged and spaced apart by a compensation gap. This segmentation allows the joint to handle torsional moments through the compensation gap while maintaining lightweight strut connections.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The inner shell segment is nested concentrically within the outer shell segment, creating a compact joint structure. The strut holding fixtures are arranged in openings of the outer shell segment with flange portions extending into the compensation gap,实现ing efficient space utilization and moment compensation.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Strength

If local strengthening means are added to compensate for torsional moments in joints, then joint strength is improved, but weight advantages are nullified

Engineering Contradiction:
Improvejoint strengthVSAvoidoverall structure weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The joint incorporates a compensation gap between the outer and inner shell segments that allows dynamic adjustment and movement to accommodate torsional moments. This dynamic design eliminates the need for static local strengthening, maintaining the lightweight advantage while ensuring joint strength.

Inventive Principle:
Principle #15Dynamics

3Strength

If conventional rigid joints are used to ensure structural integrity, then strength is maintained, but flexibility and adaptability are reduced

Engineering Contradiction:
Improvestructural integrityVSAvoidframework flexibility
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The joint design changes the structural parameters by introducing a compensation gap and allowing rotational movement between the outer and inner shell segments. This enables the joint to adapt to different loading conditions and framework configurations while maintaining structural integrity through the distributed moment compensation mechanism.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentEP2921600B1Rotary joint, framework construction kit and method for constructing a framework
Publication Date: 2016.05.18 AIRBUS OPERATIONS GMBH
  • EP2921600B1 patent drawingFigure 1~6
  • EP2921600B1 patent drawingFigure 7~14
  • EP2921600B1 patent drawingFigure 15~16

AI summary

The present invention pertains to a rotary joint (10), comprising an outer shell segment (1) having the outer shape of a solid of revolution, the outer shell segment (1) having a plurality of openings (4) arranged in the outer surface; an inner shell segment (2) having the outer shape of the solid of revolution of the outer shell segment (1), the inner shell segment (2) being aligned concentrically with the outer shell segment (1) and spaced apart from the outer shell segment (1) by a compensation gap; and a plurality of strut holding fixtures (11), the strut holding fixtures (11) having a hollow interior (12) and a flange portion (13), wherein each of the strut holding fixtures (11) is arranged in one of the plurality of openings (4) and the flange portion (13) extends within the compensation gap between the inner shell segment (2) and the outer shell segment (1) in each case; a method for constructing a framework is also disclosed.