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$20 USD / giờ
Cờ của INDIA
udupi, india
$20 USD / giờ
Hiện ở đây đang là 11:36 CH
Đã tham gia vào tháng 8 17, 2018
0 Khuyến nghị

Shashank A.

@ShashankAmin478

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$20 USD / giờ
Cờ của INDIA
udupi, india
$20 USD / giờ
Không áp dụng
Công Việc Hoàn Thành
Không áp dụng
Đúng Ngân Sách
Không áp dụng
Đúng Thời Hạn
Không áp dụng
Tỉ Lệ Thuê Lại

Manufacturing Design and 3D visualization expert

Mechanical Engineer Specialize in Aerospace applications and thoroughly experienced in additive manufacturing(FDM 3D printing). Based in TU, Delft, Netherlands Software Expertise: Solidworks : (Certified Solidworks Design Associate) Solidworks Flow simulation Solidworks Ultimaker Cura Slic3r Simplify 3D CATIA Grasshopper
Freelancer Proofreaders India
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Liên hệ Shashank A. về công việc của bạn

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Portfolio

8812404
Topology Optimization for Drone Landing Gear
Topology Optimization for Drone Landing Gear
4468570
The TOEFL iBT conducted by ETS is an English proficiency test. It has 4 sections: Reading, Listening, Speaking and Writing. Each of the sections is out of 30 marks. Therefore the score received is out of 120 marks in total. I scored 112 out of 120.
TOEFL iBT English Proficiency Test
4463581
All Terrain Autonomous All Terrain Rover
All Terrain Low budget Rover
4463576
Servo Knife Thread cutting mechanism
Thread Cutting Mechanism
Servo Knife Thread cutting mechanism
Thread Cutting Mechanism
4463572
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
4463518
I designed and assembled the parts on Solidworks and Sliced the product on Ultimaker Cura to generate the G-Code to 3D print the part.
Double Herringbone Sun and Planet Gear Bearing in Action
8812404
Topology Optimization for Drone Landing Gear
Topology Optimization for Drone Landing Gear
4468570
The TOEFL iBT conducted by ETS is an English proficiency test. It has 4 sections: Reading, Listening, Speaking and Writing. Each of the sections is out of 30 marks. Therefore the score received is out of 120 marks in total. I scored 112 out of 120.
TOEFL iBT English Proficiency Test
4463581
All Terrain Autonomous All Terrain Rover
All Terrain Low budget Rover
4463576
Servo Knife Thread cutting mechanism
Thread Cutting Mechanism
Servo Knife Thread cutting mechanism
Thread Cutting Mechanism
4463572
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
I was in charge of designing & fabricating a light weight solar powered Mars glider, which had to to be able to fit into a Can with dimensional constraints of 12.5 cm diameter and 310 cm height. It had to glide in a helical path from a height of 400 meters after ejection from a sounding rocket. The wings were foldable and had thin aero-grade Power Film solar panels retrofitted on them. The glider had no active control surfaces as per the competition requirements. While descending the, the gliders on board electronics, that were safely hard mounted, had to record environmental data and transmit it to a ground station. They were powered by the solar panels.
Foldable and Deployable Solar powered glider
4463518
I designed and assembled the parts on Solidworks and Sliced the product on Ultimaker Cura to generate the G-Code to 3D print the part.
Double Herringbone Sun and Planet Gear Bearing in Action

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Kinh nghiệm

Project Intern

MX3D B.V
thg 10 2020 - thg 2 2021 (4 tháng, 1 ngày)
Worked as a structural optimization Intern at MX3D in Amsterdam. MX3D is a Metal 3D printing company that specializes in Wire and Arc Additive Manufacturing technology. I conducted experimental research at the company and also worked on the structural topology optimization of an aluminium ship rudder.

Học vấn

Master's in Aerospace Structures and Materials

Technische Universiteit Delft, Netherlands 2019 - 2021
(2 năm)

Bachelors in Mechanical Engineering

Vellore Institute of Technology, India 2015 - 2019
(4 năm)

Bằng cấp

TOEFL iBT

Educational Testing Service
2018
The TOEFL iBT conducted by ETS is an English proficiency test. It has 4 sections: Reading, Listening, Speaking and Writing. Each of the sections is out of 30 marks. Therefore the score received is out of 120 marks in total. I scored a 112 out of 120. Picture proof is in my portfolio.

Certified Solidworks Design Associate

Dassault Systemes SOLIDWORKS Corportaion
2018
This Certification is for Associate Expertise in Part Modeling and Assembly Generation. License C-NHV677TYKN

Nội dung đã đăng

Design, Analysis and Scaled 3D printing of the Rear Axle of a Single Axle Heavy Truck

International Journal of Production Engineering
I have designed the rear axle of a single axle heavy truck on CATIAV5. An engineering drawing of the exploded view is made on Solidworks. A Finite Element analysis of the axle is done on ANSYS to obtain the maximum deformation, stress and strain, the minimum factor of safety, the life cycle and fatigue sensitivity of the axle. Then it is sliced and 3D printed. Link: https://www.researchgate.net/publication/328341953_Design_Analysis_and_3D_Printing_of_the_Rear_Axle_of_a_Single-Axle_Heavy_Truck

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