Intervista per Business 24 – Sky Canale 821

Progetto FIRE

SEAGULL

We are engaged in the development and prototype manufacturing of
THE MARIN – AIR VEHICLE FOR THE MILLENNIAL GENERATION

Aeroelastic Analysis

More than 25 years of experience in the execution of Aeroelastic Analysis and support for Certification of Aircraft.

GVT – Ground Vibration Test

More than 25 years of experience in the execution of GVT Testing on complete aircrafts and structural components.

FEM ANALYSIS

Novotech provides Advanced FEM Analysis of Aircraft Structural Components.

AFP Machine – Robot 8-Fibre Placement Head

Novotech promotes the development of High Technological and Innovative Processes (AFP, RTM, VARTM, LRI, and PCM) for the Production of Composite Structural Components.

Partners

Latest Projects and Researches

The Company

NOVOTECH is a key partner for many industries working in the aerospace field and other advanced technology sectors. The Company was founded in 1992 as spin-off engineering consulting company from Department of Aerospace Engineering of the University of Naples “Federico II”. In order to keep high competitiveness on the market, NOVOTECH has developed well consolidated know-how on aircraft and aircraft components: design/certification; automated composite manufacturing processes; advanced FEA; static/dynamic experimental tests.

NOVOTECH has proven capability in design and manufacturing of composite structures, based on low cost and out-of-autoclave automated production processes (as AFP, PCM, RTM and LRI).

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Capabilities

ACOUSTIC AND VIBRATIONS

Experimental Modal Analysis
Real Life Monitoring
Active and Passive Vibration (Design and Testing)
Production of Noise and Vibrations Control System
Statistical Energy Analysis (SEA)
Noise Certification (FAR 36 and ICAO Annex 16)
Material Testing

ADVANCED COMPOSITE MANUFACTURING

Process:
AFP (Automatic Fiber Placement);
RFI (Resin Fiber Infusion);
RTM (Resin Transfer Moulding) and others with Thermoset,Thermoplastic and Dry Fibers

AEROELASTICITY

GVT-Ground Vibration Testing
Aerolastic Certification with FAA, EASA
Gust Load Calculations

AERONAUTIC ENGINE STRUCTURE

Static and Dynamic Finite Element Calculations
Fatigue and Creep Analysis

DESIGN, TESTING and CERTIFICATION of GENERAL AVIATION AICRAFT

Preliminary Design and Sizing
Wind Tunnel Testing
Detailed Design and Structural Calculation by Classical Methods and FEM Analysis
Static Testing of Main Components
Certification with FAA and EASA rules

(LSA, VLA, FAR 23 -CS 23, Far 25-CS 25)

INTERIORS

Design
Structural Analysis
Structural Fatigue Analysis
Finite Element Analysis

MAIN AEROSPACE STRUCTURAL COMPONENT

Preliminary Sizing
Structural Stress Analysis
Structural Fatigue Analysis
Structural Components Design
Finite Element Analysis
Static and Dynamic Experimental Tests

SMART STRUCTURES

Actuation and Sensing trough.
Piezoelectric
Magnetostrictive
Shape Memory Alloy
Adaptive Structures and Morphing
Vibration Energy Harvesting

STRUCTURAL HEALTH MONITORING (SHM)

Vibration and Ultrasonic Based System with use of piezoelectric sensing and actuating patches

TEST RIG DESIGN

Preliminary Sizing
Design
Structural Analysis