Largest Non-captive Aerospace Resource Pool

Subsystem and Component MRO

Airbus Authorized Signatories

Passenger to Frieght Conversion

Electrical Wiring Harness

Primary & Secondary Structures

Interiors

Bombardier Diamond Supplier

Next-Gen In-Flight Entertainment

Objective

  • Build to Spec Next-Gen In-Flight Entertainment

Approach

  • Compact capacitive multi‑touch display
  • Linux firmware development and Android integration on ARM-based SoCs
  • Independent V&V for Linux and Android
  • Android CTS‑based product validation
  • Certified for commercial aviation standards
  • Awarded the best technical innovation at the Aviation industry conclave

Fuselage

Objective

  • Design, Development and Optimization of Composite Fuselage Structure

Approach

  • Concept design, feasibility studies, Detail Design, DFM, DFA, which includes Complete definition dossier, Preliminary sizing, stress analysis including F&DT ​
  • Certification of all the primary structural parts as per EASA requirements​
  • Non conformity/ concessions – both design and stress assessment ​
  • Components: Skin, Stringer, Frames, Clips, System cutouts and Section Assembly

Electrical Wiring & Interconnection Systems

Objective

  • Design & Development of Aircraft Electrical Wiring & Interconnection Systems

Approach

  • Aircraft Electrical Harness Concept & Detail Design ​
  • 3D Harness Routing
  • Primary Support Bracket Design and Installation​
  • Create Clash Report and Deviation report​
  • Segregation and Separation compliance​
  • Grounding and Bonding compliance​
  • Harness Release Process in Enovia/PLM​
  • Engineering Change Management​

Control Surface

Objective

  • Design to Manufacturing Support of Composite HT & VT

Approach

  • Design of Horizontal Tail, Vertical Tail & Rudder​
  • Improvement of Structural Efficiency​
  • Design Specifications to meet FAR25 standards​
  • Optimization using Carbon Fibre Composites​
  • Bird strike requirements​
  • Aero Elasticity Analysis​ and F&DT​
  • Study of Kinematics of Rudder & Horizontal Tail​

Doors: Pax & Cargo

Objective

  • Complete design and stress solutions for Cargo Door Surround (CDS) structure of S13/14.​

Approach

  • Sizing of the CDS primary composite and metallic components as per OEM requirements​
  • Providing design solution which meet the manufacturing and assembly requirements.​
  • Providing stress justification report for all primary and secondary structures.​
  • DFM drawings and CATIA models in VPM

Wings & Empennage

Objective

  • Wing modification to enable the addition of winglet.

Approach

  • Re-designing and strength check analysis
  • Design modifications & detailed stress analysis
  • Design & analysis of upper & lower skin
  • Preparation of detailed certification report

Interior

Objective

  • Design & Development of Galley Configurations​

Approach

  • Design and Manufacturing support for MF2 Galley Configurations and a predefined set for an American aerospace OEM’s commercial aircraft​
  • Type of Galleys involved:​ G1 Short & G1 Long​, G2 Galley​, G4B Galley​
  • Design enhancement of Galley structures, and ​equipment installation in Galleys​
  • Design Tubing and Electrical harness for Galleys​

Engines

Objective

  • BliskRepair process development​

Approach

  • Design and development of advanced gas heating system for post weld repair treatment of Blisk(Ti64- super alloy)​
  • Multi-jet Nozzle design & development​
  • Advanced insulation development for achieving effective heat transfer​
  • Material testing to understand effective residual stress reduction​
  • System design certified by TUV ​