top of page
OUR PROJECTS
-
Design
-
Maintain maximum operational loading
-
Remove stress concentrations
-
Reduce overall material
-
Optimize for AM
-
-
Results
-
45% weight reduction (same material)
-
Eliminated failure in test
-
Reduced manufacturing costs
-
Streamlined testing and validation
-
Engine Module Project
-
Design
-
Preliminary & Detail Design of Power Turbine Module
-
Integration and Verification
-
Complete Tolerance Stack and Gap Analysis
-
Maintain BOM
-
-
-
Analysis
-
Analysis of all static and rotating hardware
-
Stress
-
Vibration
-
Thermal
-
-
-
Presented Design Reviews to customer CEs
-
$3 Million+ Program
Root Cause Analysis + Product Redesign
-
Process
-
Tasked to investigate multiple product failures
-
Reviewed engineering documentation, assembly procedures, and observed assembly process
-
Performed Root Cause Analysis
-
Verified all engineering requirements and performed tolerance analysis
-
Developed multiple new design concepts and analyzed the concepts
-
Presented findings to customer chief technologist
-
Supported project until EIS
-
-
Results
-
Advatech design patented by customer
-
Zero failures of new design
-
Winglet Design
-
Coordination
-
Customer
-
MFR/Suppliers
-
OEM
-
DERs
-
Tooling
-
Test
-
-
Furnished Data
-
Load
-
Master Dimension Datasheet
-
Process Specs
-
Procedures & Definitions
-
Sample Package
-
-
Design/Analysis
-
CATIA models/drawings
-
Static strength/damage tolerance reports
-
FEM documentation and model
-
Mass properties
-
-
Design Criteria per FAR, Part 25
-
Design of wing mods/attachment hardware
-
CATIA models/drawings
-
-
Static Test Plan & Support
-
Certification Plans/Documentation
-
FAA approved test plan
-
Instrumentation Design
-
Test Fixture Design
-
FAA approved test reports
-
-
Continued Airworthiness Documents Support
-
Maintenance Planning Document
-
Aircraft Maintenance Manual
-
Structural Repair Manual
-
Supplemental Inspection
-
bottom of page