Martin P. Profile

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(1 review)

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$20 USD / hour

brno,

czech republic

$20 USD / hour

It's currently 7:03 AM here

Joined April 24, 2014

0 Recommendations

Martin P.

@dhv4brre

5.0

(1 review)

2.6

50%

$20 USD / hour

brno,

czech republic

$20 USD / hour

100%

Jobs Completed

100%

On Budget

100%

On Time

N/A

Repeat Hire Rate

FEM & CAD specialist Aircraft design and certification

FEM & CAD specialist for 20 years Aircraft design and certification for 15+ years. I am ready to start work on your 3D design jobs. I hold the related experience necessary and also have an excellent capability to handle this skillful job. In my time I have worked as a 3D design Designer and as a FEM specialist in the areas of Aircraft design and certification and have also worked as a Solidworks and Inventor Designer. I have the experience and skills required for your projects and am ready to be hired by you.

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Contact Martin P. about your job

Portfolio

$Pratt & Whitney Canada \"PT6A-42\" Turboprop engine mounting analysis Dynamic analysis of engine mounting Non-linear static analysis of engine mounting according to the requirements of FAR23 regulation Optimization of the structure and recommendations for modification - CAD remodeling FEA - NASTRAN CAD - SolidWorks Rendering - KeyShot$

PT6A-42 Engine Mounting - Analysis, Optimization, Remodeling

3D Modeling - Solidworks
Rendering - KeyShot

Instruments:
Garmin - GCU275, GDU1200W, GTC570, GMC710
SwissChrono - CM30
L-3 Communications Avionics Systems - ESI2000

3D Modeling & Rendering - Aircraft Dashboard

3D Modeling & Rendering - Avionics

Stackable pallets for products storage & APS pallets (Automatic car Park System)
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3D Modeling - SolidWorks

Rendering - KeyShot

FEA Analysis & Optimization - NASTRAN

3D Modeling, Rendering, FEA - Stackable Pallets & APS

$CAD-Automated Parking System (APS)\n\n90 pieces of pallet manufactured and installed in a multi-storey car park house here in Brno (Czech Republic) on the Kopecna street.\n\n45 pieces of modified pallets was manufactured and installed in a multi-storey car park house in Warsaw (Poland) on the Mokotowska Street$

CAD - Automated Parking System (APS) - real story

$90 pieces of pallet manufactured and installed in a multi-storey car park house here in Brno (Czech Republic) on the Kopecna street.\n\n45 pieces of modified pallets was manufactured and installed in a multi-storey car park house in Warsaw (Poland) on the Mokotowska Street$

FEM - Automated Parking System (APS) - real story

PT6A-42 Engine Mounting - Analysis, Optimization, Remodeling

3D Modeling & Rendering - Aircraft Dashboard

3D Modeling & Rendering - Avionics

3D Modeling, Rendering, FEA - Stackable Pallets & APS

CAD - Automated Parking System (APS) - real story

FEM - Automated Parking System (APS) - real story

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5.0

$277.00 CAD

Platonic Solids

Martin is great to work with. Highly recommended.

3D Rendering

3D Modelling

3D Animation

Peter N.

@PeterNosalik

•

9 years ago

Experience

Institute of Aerospace Engineering, Brno University of Technology

Jun 2000 - Dec 2012 (12 years, 6 months)

Aerospace Research Centre - Research worker

consortium DLR, AIRBUS-DEUTSCHLAND, EADS CCR, EADS GMBH, ATECA, ALMA Consulting, University of Liverpool, University of Oxford, University of Patras, University of Aachen, ENS de Cachan, University of Stuttgart, Brno University of Technology

Jan 2006 - Dec 2009 (3 years, 11 months)

co-worker of the grant of 6FP EU - „CELPACT – Cellular Structures for Impact Performance“, FP6-031038, consortium DLR, AIRBUS-DEUTSCHLAND, EADS CCR, EADS GMBH, ATECA, ALMA Consulting, University of Liverpool, University of Oxford, University of Patras, University of Aachen, ENS de Cachan, University of Stuttgart, Brno University of Technology. http://www.easn.net/supported-projects/celpact/celpact.htm

MORAVAN – AEROPLANES a.s.

Jan 1998 - Jun 2000 (2 years, 5 months)

Independent research worker, Strength analyses

Education

Ph.D.

Brno University of Technology,

Czech Republic

1997 - 2004

(7 years)

Ing.

Brno University of Technology,

Czech Republic

1992 - 1997

(5 years)

Qualifications

CAA CZ - Czech Civil Aviation Authority

2008

Certification and airworthiness - Certificate of completion of specialized course

Brno University of Technology

2004

the State examination certificate

Brno University of Technology

1997

the State examination certificate

Publications

Static Analysis of Main and Nose-wheel Landing Gear of the Ae270HP Airplane

Technical Report

2002 - Static Analysis of Main and Nose-wheel Landing Gear of the Ae270HP Airplane

Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear

Seminar ARC (Aerospace Research Centre)

2003 - Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear

2010-2012 SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY

RESEARCH BULLETIN Vol.2012

SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY. RESEARCH BULLETIN, Vol.2012, (2012), No.22, pp.1-8, ISSN 1425-2104

Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities

RRDPAE ‘98 Conference

1998 - Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities

Static strength analysis of the Ae270 Nose-wheel and Main Landing Gear

Technical Report

1999 - Static strength analysis of the Ae270 Nose-wheel and Main Landing Gear

Static strength analysis of the Ae270 Main Landing Gear

Technical Report

1999 - Static strength analysis of the Ae270 Main Landing Gear

Static strength analysis of the Ae270 Nose-wheel Landing Gear

Technical Report

1999 - Static strength analysis of the Ae270 Nose-wheel Landing Gear

Static strength analysis of the Aero Ae270 Nose-wheel and Main Landing Gear

FS100 VUT Brno

2000 - Article for the 100 years University jubilee: Static strength analysis of the Aero Ae270 Nose-wheel and Main Landing Gear

Comparison of the Results of FEM Analysis and Results of Tension Measurements

RRDPAE 2000 Conference

2000 - Comparison of the Results of FEM Analysis and Results of Tension Measurements

Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities

Journal for Czech Aerospace Research, Development and Innovations

2000 - Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities

Experience with application of the MSC.NASTRAN software in strength analyses of airplane landing gears

MSC.Software User conference

2000 - Experience with application of the MSC.NASTRAN software in strength analyses of airplane landing gears

Package of Aeroelastic analyses of the EV-97 VLA Airplane Wing

Technical Report

2000 - Package of Aeroelastic analyses of the EV-97 VLA Airplane Wing

Static strength analyses of the Ae270 landing gears

Seminar

2001 - Static strength analyses of the Ae270 landing gears

Strength adjudication of the dynamograph's bolted join

Technical Report

2001 - Strength adjudication of the dynamograph's bolted join

The influence of material and geometric non-linearity to accuracy FEM stress analysis of landing gear

WORLDWIDE AEROSPACE CONFERENCE and TECHNOLOGY SHOWCASE 2002, MSC.Software 2002

2002 - The influence of material and geometric non-linearity to accuracy FEM stress analysis of landing gear

Comparison of the Results of FEM Analysis and Results of Tension Measurements

ICAS 2002

2002 - International Congress of the Aeronautical Science. Comparison of the Results of FEM Analysis and Results of Tension Measurements

Aeroelasticity Airworthiness

Journal for Czech Aerospace Research, Development and Innovations

2002 - Aeroelasticity Airworthiness

Static strength analysis of the Ae270HP Main Landing Gear

Technical Report

2002 - Static strength analysis of the Ae270HP Main Landing Gear

Static strength analysis of the Ae270 and Ae270HP Nose-wheel Landing Gear

Technical Report

2002 - Static strength analysis of the Ae270 and Ae270HP Nose-wheel Landing Gear

Static strength analysis of the Ae270HP Nose-wheel Landing Gear

Technical Report

2002 - Static strength analysis of the Ae270HP Nose-wheel Landing Gear

Application of the MSC.MVISION material database in association with the MSC.Nastran and MSC.Dytran solvers

Technical Report

2003 - Application of the MSC.MVISION material database in association with the MSC.Nastran and MSC.Dytran solvers

Static analysis of VUT 100 Aircraft Main and Nose-wheel Landing Gear

Journal for Czech Aerospace Research, Development and Innovations 3/2003

2004 - Static analysis of VUT 100 Aircraft Main and Nose-wheel Landing Gear

Preliminary static strength analysis of the VUT100 Nose-wheel Landing Gear

Technical Report

2004 - Preliminary static strength analysis of the VUT100 Nose-wheel Landing Gear

Preliminary static strength analysis of the VUT100 Main Landing Gear

Technical Report

2004 - Preliminary static strength analysis of the VUT100 Main Landing Gear

The Influence of Material and Geometric Non-Linearities to Accuracy FEM Stress Analysis of Landing Gear

ICAS 2004 Conference

2004 , International Congress of the Aeronautical Science - The Influence of Material and Geometric Non-Linearities to Accuracy FEM Stress Analysis of Landing Gear

Vibration analysis of the wind power plant's blade made of carbon-glass composite

Technical Report

2004 - Vibration analysis of the wind power plant's blade made of carbon-glass composite

Nonlinear stress-strain analysis of the wind power plant's blade made of carbon-glass composite

Technical Report

2004 - Nonlinear stress-strain analysis of the wind power plant's blade made of carbon-glass composite

Static strength analysis of the Ae270 Nose-wheel Landing Gear (TOW 4000kg)

Technical Report

2004 - Static strength analysis of the Ae270 Nose-wheel Landing Gear (TOW 4000kg)

Static strength analysis of the Ae270 Main Landing Gear (TOW 4000kg)

Technical Report

2004 - Static strength analysis of the Ae270 Main Landing Gear (TOW 4000kg)

Adjudication of manufacturing defect of the Main Landing Gear of the L159-ALCA Aircraft with respect to the static strength

Technical Report

2004 - Adjudication of manufacturing defect of the Main Landing Gear of the L-159 ALCA Aircraft with respect to the static strength.

Preliminary static strength analysis of the Ae270 Nose-wheel Landing Gear (TOW 4000kg)

Technical Report

2004 - Preliminary static strength analysis of the Ae270 Nose-wheel Landing Gear (TOW 4000kg).

Preliminary static strength analysis of the Ae270 Main Landing Gear (TOW 4000kg)

Technical Report

2004 - Preliminary static strength analysis of the Ae270 Main Landing Gear (TOW 4000kg)

FEM Based Fatigue Life Analysis of Landing Gear

Journal for Czech Aerospace Research, Development and Innovations, Vol.2005

2005 - FEM Based Fatigue Life Analysis of Landing Gear, ISSN 1211-877X

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

Journal for Czech Aerospace Research, Development and Innovations, Vol.2006

2006 - Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear, ISSN 1211-877X

Crashworthiness of Aircraft Seat.

Optimage Ltd., Edinburgh, UK. 25th Congress of the International Council of the Aeronautical Sciences, Hamburg

2006 - Crashworthiness of Aircraft Seat. ISBN 0-9533991-7-6,

Preliminary strength analysis of the Main and Nose-wheel Landing Gear of the L-410 Aircraft.

Technical report

2012 - Technical report of the MOSTA project

Geometric optimisation of the fuselage main beam No.12

Technical report of the MOSTA project

2012 - Technical report of the MOSTA project

Geometric optimisation of the fuselage main beam No.14

Technical report

2012 - Technical report of the MOSTA project

Geometric optimisation of the frame segment No.12

Technical report

2012 - Technical report of the MOSTA project

Geometric optimisation of the frame segment No. 14.

Technical report

Technical report of the MOSTA project

Static strength analysis of the Ae270 Nose-wheel and Main Landing Gear

Technical Report

1999 - Static strength analysis of the Ae270 Nose-wheel and Main Landing Gear

Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities, RRDPAE ‘98

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Martin P.

Martin P.

@dhv4brre

FEM & CAD specialist Aircraft design and certification

Contact Martin P. about your job

Portfolio

Reviews

Experience

Research worker

co-worker of the grant of 6FP EU - CELPACT

Independent research worker

Education

Ph.D.

Ing.

Qualifications

Certificate of completion of specialized course

University Diploma

University Diploma

Publications

Static Analysis of Main and Nose-wheel Landing Gear of the Ae270HP Airplane

Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear

2010-2012 SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY

Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities

Static strength analysis of the Ae270 Nose-wheel and Main Landing Gear

Static strength analysis of the Ae270 Main Landing Gear

Static strength analysis of the Ae270 Nose-wheel Landing Gear

Static strength analysis of the Aero Ae270 Nose-wheel and Main Landing Gear

Comparison of the Results of FEM Analysis and Results of Tension Measurements

Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities

Experience with application of the MSC.NASTRAN software in strength analyses of airplane landing gears

Package of Aeroelastic analyses of the EV-97 VLA Airplane Wing

Static strength analyses of the Ae270 landing gears

Strength adjudication of the dynamograph's bolted join

The influence of material and geometric non-linearity to accuracy FEM stress analysis of landing gear

Comparison of the Results of FEM Analysis and Results of Tension Measurements

Aeroelasticity Airworthiness

Static strength analysis of the Ae270HP Main Landing Gear

Static strength analysis of the Ae270 and Ae270HP Nose-wheel Landing Gear

Static strength analysis of the Ae270HP Nose-wheel Landing Gear

Application of the MSC.MVISION material database in association with the MSC.Nastran and MSC.Dytran solvers

Static analysis of VUT 100 Aircraft Main and Nose-wheel Landing Gear

Preliminary static strength analysis of the VUT100 Nose-wheel Landing Gear

Preliminary static strength analysis of the VUT100 Main Landing Gear

The Influence of Material and Geometric Non-Linearities to Accuracy FEM Stress Analysis of Landing Gear

Vibration analysis of the wind power plant's blade made of carbon-glass composite

Nonlinear stress-strain analysis of the wind power plant's blade made of carbon-glass composite

Static strength analysis of the Ae270 Nose-wheel Landing Gear (TOW 4000kg)

Static strength analysis of the Ae270 Main Landing Gear (TOW 4000kg)

Adjudication of manufacturing defect of the Main Landing Gear of the L159-ALCA Aircraft with respect to the static strength

Preliminary static strength analysis of the Ae270 Nose-wheel Landing Gear (TOW 4000kg)

Preliminary static strength analysis of the Ae270 Main Landing Gear (TOW 4000kg)

FEM Based Fatigue Life Analysis of Landing Gear

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

Crashworthiness of Aircraft Seat.

Preliminary strength analysis of the Main and Nose-wheel Landing Gear of the L-410 Aircraft.

Geometric optimisation of the fuselage main beam No.12

Geometric optimisation of the fuselage main beam No.14

Geometric optimisation of the frame segment No.12

Geometric optimisation of the frame segment No. 14.

Static strength analysis of the Ae270 Nose-wheel and Main Landing Gear

Landing Gear FEM Analysis and Comparative Testing, Considering the Material and Geometric Non-Linearities, RRDPAE ‘98

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