System Controller Connector/Harness/Baseplate Redesign Feasibility Study

Electronic assemblies are used to control various systems in an aircraft. Under normal operating conditions, these assemblies undergo vibration, and therefore have an expected life span. Different designs are analyzed to reduce production cost, and these designs have to ensure that the electronic components contained within the hardware can tolerate the same operating conditions without failure. With time continuous research projects are being conducted to produce products with the same quality and lower costs, and this is one of them.

Faculty Supervisor:

Kamran Behdinan

Student:

Mahmoud Embabi

Partner:

Honeywell Aerospace

Discipline:

Engineering - mechanical

Sector:

Aerospace and defense

University:

Program:

Accelerate

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