A group study of aircraft seating as a circular product-service system. My work focused on material choices, manufacturing routes and assembly of the primary structure, secondary systems and accessories.
PROJECTSustainable Aircraft Seat
MY ROLEMaterials, manufacturing and assembly within a group design
CONTEXTGroup project Team project
Inspect full-size image ↗FIG. 01Modular aircraft-seat concept developed from teardown and circularity research.
01 / OVERVIEW
The project in a minute.
THE OUTCOME
Contributed the materials, manufacturing and assembly proposal to a group seat concept, alongside shared lifecycle and circularity studies.
Improve the material use, serviceability and end-of-life route of an aircraft seat, while separating long-life structure from parts that wear out sooner.
My contribution
Materials, manufacturing and assembly within a group design. The final report explicitly credits my work on materials, manufacturing and structural assembly; whole-product CAD and lifecycle calculations have separate team credits.
Read this in context
Group concept study. Whole-product CAD and lifecycle calculations are team outputs. Mass estimates differ across report submissions, so no single final reduction percentage is presented.
Group concept study. Whole-product CAD and lifecycle calculations are team outputs. Mass estimates differ across report submissions, so no single final reduction percentage is presented.
Materials
My documented contribution
Material, manufacturing and assembly work, explicitly credited in the final contribution statement.
Modular
Group system concept
Replace worn parts without replacing the entire seat; connect maintenance to material recovery.
Concept
Evaluation status
Lifecycle and mass estimates belong to specific design iterations, not a certified production seat.
Source notes & scope 2
Sustainable Aircraft Seat Designpp. 20–24
Final system proposal and individual contribution statement on p. 24.
Sustainable Aircraft Seat Designpp. 12–18
Earlier submission; its weight estimates are not interchangeable with the final system.
↗FIG. 02The teardown exposed service, joining and material-separation constraints.↗FIG. 03Material decisions were assessed with life-cycle and circularity reasoning.
Built and tested a physical prototype, identifying fit, wiring, power and control issues. The production-oriented CAD proposes injection-moulded parts and modular assembly; it is not evidence of mass production.
My partPrototype testing, wiring, assembly, soldering and power calculations
Hands-on experience connecting physical robots, perception, control and services through task demonstrations, teleoperation, navigation experiments and hardware work.
My partTechnical Support Engineer Intern · robot applications and testing