WHAT WE CAN DO

    Provide information of completion (floor Plan)   Information on design process and customer specification  Demonstrate compliance with structural regulations or requirements Types of Materials used in Fabrication Types of hardware components used and vendors Cabinet assembly and installation Engineering standards and drawings

AIR CRAFT INTERIORS

General Floor plan of Business Air craft Process flow for aircraft interior installations

FOR INTERIORS

 Customer driven design and comfort  Aesthetically pleasing interior design with maximum storage capacity, passenger safety, weight reducing concepts, installation procedure, etc,.

 Meet the customer specification with quality and timely delivery till the last detail  Satisfy customer request also maintain compliance with the regulatory standards  Make best usage of materials, weight and space

General characteristics

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Crew:

2 (Pilot & Co-Pilot) •

Capacity:

14 passengers •

Length:

15.02 m (49.28 ft) •

Wingspan :

14.70 m (48.23 ft) •

Height:

5.20 m (17.06 ft) •

Useful load:

1,232 kg (2,710 lb) •

Max take off weight:

(15,653 lb) 7,100 kg

WORK FLOW FOR INTERIORS

CUSTOMER SPEC & DESIGN MARKETING DRAWING & MASTER OPTION LIST Interior Design Design review meeting, material selection &orders. Design modeled by existing data, standard models & marketing drawings.

2D & 3D working drawings created Weight Estimates & Reports Stress/Material Evaluations

Feasibility studies

Written specification Design Liaison New models identified

Corrections & improvements

Avionics Design Avionics Technical Support Avionics Mechanical Installations Systems Design Wire Routing Specification Liaison Configuration Management Program Management Management by Options CATIA Processes Standards Management Manufacturing process Complete work instruction CNC Machining router Inspection process Completion process

AIRCRAFT INTERIOR

The Main Cabin virtual image

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OUR WORK EXPERIENCE

Systems Engineering  We have a specialized team of engineers and designers that are tasked with utilizing the extensive 3D modeling capabilities of CATIA in Wiring Installation  Optimum routing and placement of wiring and work with avionics mechanical to adjust any equipment locations that will optimize wiring.

 They integrate systems into the aircraft such as lighting, telephone, video/audio, cabin integration, and galley accessories (i.e., ovens, coffeemakers, etc.).

OUR WORK EXPERIENCE

Systems Engineering  Engineers Assist for the installation of all the mechanical parts inside the aircraft, such as the brackets that pertain to avionics equipment and wire, bundles, and connectors that are part of wire installation.

 Exposure for cabin temperature controls and waste water systems.

They also assist in Air and plumbing to supply to the cabinets was tapped from basic aircraft air and water systems

OUR WORK EXPERIENCE

Design Engineering  We have a specialized team of engineers and designers that are tasked with 2D & 3D modeling capabilities of CATIA V4 & V5, creation of CNC programming  Create 2D drawings as per customer specification with reference to aircraft canter line drawings.

 Experience engineers working on PDM or VPM systems  Make best usage of materials, weight and space which are producible, repeatable, certifiable and maintainable.

 Utilize the most cost effective methods in selection including standardization or using pre existing designs and parts where possible.

OUR WORK EXPERIENCE

Design Engineering  Assist procurement of material which are suitable for the design they have specified.

 Strength, standard and application Information on installation components..

 General information metal joining, measurement systems, control systems, finishing and marking  Designing standards components and allowable, according assist to in manufacturing, installation and inspection team. Create part list (BOM)  Assist assemblies in testing components and

OUR WORK EXPERIENCE

Design Engineering information on Materials [Alloys, non metallic (plastics, thermoplastics, composites, leather, fork, felt, adhesive tapes, foams, elastomers, etc,)] and installation (Hinges, brackets, latches, screws, fasteners (blind, fluid tight, etc.), bolts, nuts, pins, screws, rivets, bearings, splines & keys, gears, seals, springs and miscellaneous) commonly used in interiors composites: for panels available in different thickness Ply Fiberglass skin / aluminum core Ply Fiberglass skin / aluminum core Carbon skin / aluminum core aluminum skin / aluminum core Acoustic panel paper skin/paper core/rubber layer

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OUR WORK EXPERIENCE

Design Engineering Valance panels extend the full length of the main cabin on the left and right sides and are installed between the headliner and window panels. These panels incorporate passenger service units (PSU) panels plus upper and lower utility shrouds often housing up/downwash lighting.

Thermoplastic resin reinforced laminates used in Manufacturing applications such as valance panels luggage bins, flooring and galley carts, cans, etc.

OUR WORK EXPERIENCE

Design Engineering Seats are purchased from different vendors based on the aesthetic the customer is requesting. Aircraft seats are very rigorously tested to gain approval an impact analysis criteria is established Engineering placement and securing of seats on the aircraft and instruction of how the passenger position in the seat while taxi, takeoff and landings are taken care Document specification of the seating is provided by the vendor Thermoplastic resin reinforced laminates, leather, foam and alloys used in assembly

Installation are purchased from different vendors based on the strength, application and standards and specification details Metallic alloys (aluminum, steel, titanium, etc.) also non metallic like (rubber, sealants, etc) used in products

screws seals Bearing brackets Nuts, bolts & pins hinges Iso mounts

OUR WORK EXPERIENCE

Weight Engineering     Enables in calculation of the entire weight which goes in Aircraft.

Work involves calculation of structural, non structural and miscellaneous weights Calculation of weight are linked to CATIA V5 also using Visual basic in excel for formulation of weight for different structures as individually.

Conversant with all measuring systems for temperature, pressure and position measurement.

Stress Engineering    Strength checking of the structural substation for certification.

Well versed with modeling procedures and analytical procedures for interiors Experts in commercial tools and implementing design process for interiors

Scope Static strength analysis substantiation of the Galley and Aft lavatory structure for acceleration loads using FEM methods inputs • CATIA V5 Model • Material properties • Equipment weights • Allowable for soft mount, rivets and nuts Approach Deliverables

• 2D quadrangle element used to model composite panels in PATRAN & HYPERMESH • Calculation of Entire mass of the structure M Galley = M miscellaneous + M panels Note :The mass of miscellaneous includes mass of inserts, potting, brackets, and screws as well as mass of laminate, and veneer.

• Equipment weights were modeled as concentrated mass • Static analysis done in NASTRAN 9G X-load, 7G Z-load and 3G Y-load.

• Analytical substantiation for soft mounts, screws, brackets and bolts.

Deliverables • Stress report for static strength of the structure with attachment reactions during the forward/aft, sideward and downward/upward load case as per certification standards.

Bulkhead and drawers

EXPERTISE

Seating systems F urniture's Bulkhead and drawers Lighting and cabin sound proof