Professional Engineering Analysis

Complex Assembly Analysis

Real-world engineering assemblies with detailed BOM, interference analysis, stress simulation, and manufacturability review.

Trent XWB Turbofan Engine

Aerospace Propulsion

Parts: 2487Mass: 7,277 kgSize: Ø3.0m × 4.7mExtreme

Explode:0%

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Assembly Description

High-bypass turbofan engine powering Airbus A350 XWB. Features 3-stage LP compressor, 8-stage IP compressor, 6-stage HP compressor, annular combustor, and single-stage HP/IP/LP turbines.

Assembly Metrics

Total Parts

2487

Total Mass

7,277 kg

Dimensions

Ø3.0m × 4.7m

Complexity

Extreme

Analysis Summary

InterferenceClear

Stress Safety1.8x

Max Temperature1,650°C

DFM Score92/100

Material Distribution

Ti-6Al-4V8%

Inconel 7181%

Ti-8Al-1Mo-1V59%

Waspaloy2%

Hastelloy X0%

CMSX-4 SC27%

M50 Steel2%

MRS Analysis Pipeline

From STEP import to comprehensive engineering review

Step 1

STEP Import

Parse geometry, hierarchy, and metadata from native CAD files

Step 2

Structure Analysis

Extract BOM, assembly tree, joints, and kinematic chains

Step 3

Engineering Review

Interference detection, DFM analysis, stress and thermal simulation

Step 4

Report Generation

PDF/HTML reports with traceable assumptions and confidence levels