Space Frame Suspension Connection for Haul Trucks

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Solution Overview

Problem

Conventional space frame structures for haul trucks face challenges in dynamic applications due to loads, bending, and flexing, requiring carefully designed high-strength castings and fabrications to maintain stiffness and flexibility while ensuring proper load transfer from the dump body to the wheels, which is difficult to achieve with traditional nodal connections.

Innovation Solution

The design of a front upper suspension connection for haul trucks includes a bottom surface for welding to a front lower suspension connection, a top rear mounting surface for welding to a front upper frame connection, and a front strut attachment point that pivots to attach a front strut, with coaxial holes for a pin to pass through, providing a lightweight and durable configuration for load distribution.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If conventional welded steel frames are used, then strength and load-bearing capacity are improved, but weight increases significantly and manufacturing complexity increases

Engineering Contradiction:
Improveload-bearing capacityVSAvoidframe weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The frame is divided into multiple tubular members connected by nodal connections, creating a space frame structure that distributes loads efficiently across segments rather than requiring a solid welded steel frame

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The nodal connections integrate multiple materials and connection methods (welding, mechanical fastening) to create a composite structure that achieves high strength-to-weight ratio by combining the advantages of different connection techniques

Inventive Principle:
Principle #40Composite materials

2Strength

If conventional welded steel frames are used, then strength is improved, but manufacturing complexity and time increase

Engineering Contradiction:
Improveframe strengthVSAvoidmanufacturing complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The frame structure is segmented into modular components (tubular members and nodal connections) that can be manufactured separately and assembled, reducing overall manufacturing complexity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Nodal connections are designed to be pre-assembled with tubular members using standardized procedures, allowing for preliminary preparation and reduction of on-site welding complexity

Inventive Principle:
Principle #10Preliminary action

3Weight of moving object

If fabricated nodal connections are used in space frames, then weight is reduced, but reliability under dynamic loads deteriorates

Engineering Contradiction:
Improveframe weightVSAvoidreliability under dynamic loads
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The nodal connections feature curved transition regions and rounded geometries that distribute stress more evenly under dynamic loading conditions, improving reliability while maintaining the lightweight space frame structure

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The nodal connections are designed with optimized geometric parameters and material properties to withstand dynamic loads, including carefully designed curvature radii and wall thickness variations that enhance structural integrity

Inventive Principle:
Principle #35Parameter changes

4Stability of the object's composition

If high-strength castings and fabrications are used, then stiffness and flexibility characteristics are improved, but manufacturing complexity increases

Engineering Contradiction:
Improvestiffness and flexibility characteristicsVSAvoidmanufacturing complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The structure is segmented into standardized nodal connections and tubular members with consistent design parameters, allowing for simplified manufacturing processes while achieving the required stiffness and flexibility characteristics through the overall space frame configuration

Inventive Principle:
Principle #1Segmentation

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 ensures reliable load transfer and distribution between the dump body and the space frame, accommodating dimensional variations and component deflection, while maintaining structural integrity and flexibility under dynamic conditions.

Implementation Method 1

a bottom surface configured to weldably attach to a front lower suspension connection fabrication

Methodology Applied
Scientific EffectWelding: Welding

Implementation Method 2

a top rear mounting surface configured to weldably attach to a front upper frame connection fabrication

Methodology Applied
Scientific EffectWelding: Welding

Implementation Method 3

a front strut attachment point located below the top rear mounting surface and the top front mounting surface configured to pivotably attach a front strut of a front suspension system

Methodology Applied
Scientific EffectPivoting: Hinge

Implementation Method 4

The front strut attachment point can include a hole passing through the top rear mounting surface, a coaxial hole passing through the top front mounting surface, and a front strut attachment pin configured to pass through the top rear mounting surface, the top front mounting surface, and a top mounting hole integral to the front strut

Methodology Applied
Scientific EffectMechanical Fastening: Mechanical Fastener

Data Source

PatentUS11292311B2Space frame front upper suspension connection
Publication Date: 2022.04.05 CATERPILLAR INC
  • US11292311B2 patent drawing
  • US11292311B2 patent drawing
  • US11292311B2 patent drawing

AI summary

A front upper suspension connection for a space frame comprises a bottom surface fixedly attachable to a front lower suspension connection; a top rear mounting surface fixedly attachable to a front upper frame connection; a top front mounting surface fixedly attachable to a first elongate support member; a front strut attachment point located below the top rear mounting surface and the top front mounting surface to pivotably attach a front strut; and a lower rear mounting surface located below the top rear mounting surface fixedly attachable to a second elongate support member. The front strut attachment point can include a hole passing through the top rear mounting surface, a coaxial hole passing through the top front mounting surface, and a front strut attachment pin configured to pass through the top rear mounting surface, the top front mounting surface, and a top mounting hole integral to the front strut.