Onkar_Joshi - Hyperloop.pptx
- 1. Made By :- ONKAR R JOSHI Roll No. :- T121220161 (TE Mechanical)
- 2. • CONTENTS • INTRODUCTION • WHAT IS HYPERLOOP • KANTROWITZ LIMIT • MAIN PARTS • AIR LOCKING SYSTEM • ADVANTAGES AND DISADVANTAGES • CONCLUSION
- 3. • INTRODUCTION • A FUTURISTIC MODE OF TRASPORATATION INTRODUCED BY ELON MUSK . • HIGHLY EFFICIENT THAN TRADITIONAL MODES WITH INCREASED SPEED. • CAN COVER DISTANCES ABOVE 1000 KILOMETERS IN UNDER AN HOUR.
- 4. • WHAT IS HYPERLOOP ??? IT CONSISTS OF A LOW PRESSURE TUBE WITH CAPSULES THAT ARE TRANSPORTED AT BOTH LOW AND HIGH SPEEDS THROUGHOUT THE LENGTH OF THE TUBE. THE CAPSULES ARE SUPPORTED ON CUSHION OF AIR. THE PROPAGATION OF CAPSULES TAKES PLACE DUE TO ELECTROMAGNETIC MOTORS.
- 5. • MAIN PARTS OF HYPERLOOP 1. CAPSULES 2. LOW PRESSURE TUBE 3. COMPRESSOR FAN 4. SUSPENSION 5. STATOR AND ROTOR
- 6. • CAPSULE • THE CAPSULE WILL BE STREAMLINED AND HAS A COMPRESSOR FAN MOUTED ON IT. • DIMESNSIONS :- WIDTH OF 1.35 METERS HEIGHT OF 1.10 METERS FRONT AREA OF 1.14 SQUARE METERS (ROUNDED CORNERS) • WEIGHS AROUND 3,100 KILOGRAMS (INCLUDING LUGGAGE) • COST ABOUT $245,000 OR INR 1,61,70,000.
- 7. • LOW PRESSURE TUBE • A PARTIALLY EVACUATED TUBE WITH ABOUT 100 PASCALS OF PRESSURE. • PYLONS WILL BE CONSTRUCTED AT EVERY 30 METERS TO SUPPORT THE TUBE • SOLAR PANELS WOULD BE FITTED ON THE ROOF OF THE TUBE FOR GENERTION OF THE POWER REQUIRED FOR RUNNING THE SYSTEM. • DIMENSIONS:- CROSS SECTIONAL AREA OF 3.91 SQUARE METERS. • INNER TUBE DIAMETER WILL BE EQUAL TO 2.23 METERS • COST ABOUT $ 650 MILLIONS OR INR 4920 CRORES FOR DISTANCE OF ABOUT A LTTLE MORE THAN 500 KILOMETERS.
- 8. • KANTROWITZ LIMIT IT A THEORETICAL CONCEPT OF CHOKING OF FLUIDS AT SUPERSONIC VELCITIES. HYPERLOOP OVERCOMES IT BY USE OF AN COMPRESSOR FAN AT THE FRONT OF THE CAPSULE.
- 9. • COMPRESSOR FAN • THE COMPRESSOR SERVES TWO PURPOSES 1. ALLOWS TH CAPSULE TO MOVE THOUGH THE NORROW TUBE WITHOUT ANY CHOCKING BY COMPRESSING THE AIR AND BY-PASSIG IT THROUGH THE CAPSULE. 2. SUPPLIES AIR TO THE AIR SUSPENSION THROUGHOUT THE JOURNEY
- 10. • SUSPENSION • USE OF AN AIR BEARING SUSPENSION INSTEAD OF CONVENTIONAL SUSPENSION WILL OFFER MORE STABILITY AND LOW DRAG AT A FEASIBLE COST. • THE FIELD IN THE GAP PUSHES THE SKI AWAY FROM THE WALL , THUS HELPS MAINTAINING THE NOMINAL RIDE HEIGHT. • IT A PAIRED WITH A MECHANICAL SUSPENSION FOR MORE COMFORT OF PEOPLE ON BOARD • IT IS EXACTLY SIMILAR TO THE AIR HOCKEY TABLE.
- 11. • STATOR AND ROTOR • THE HYPERLOOP USES A LINEAR INDUCTION MOTOR TO ACCELERATE AND DECELERATE THE CAPSULES. • ROTOR IS MOUNTED ON THE CAPSULE. • STATOR IS MOUNTED ON THE TUBE.
- 12. • AIR LOCKING SYSTEM AS THE STATIONS FOR HALTING OF CAPSULE ARE NEEDED TO BE MAINTAINED AT A LOWER PRESSURE AIR LOCKS WOULD BE NEEDED TO PREVENT THE RISE IN PRESSURE. VIDEO
- 13. • ADVANTAGES FASTER LESS EXPENSIVE POLLUTION FREE IMMUNE TO ALL WEATHER SELF POWERING SAFER
- 14. • DISADVANTAGES TUBE PRESSURISATION TURNING WOULD REQUIRE A VERY LARGE RADIUS MOVING SPACE FOR PASSSENGER IS INSUFFICIENT
- 15. • CONCLUSION AS IT HAS A NUMBER OF ADVANTAGES IT’LL BE VERY HELPFUL MODE OF TRANSPORTATION. FASTER SPEED MORE ECONOMICAL DESIGN MAKES IT A HANDY COSTUMER TO BE THE FIFTH MODE OF TRANSPORTATION.
- 16. • REFERENCES • Musk, Elon (August 12, 2013). "Hyperloop Alpha"(PDF). SpaceX. Retrieved August 13, 2013. • Garber, Megan (July 13, 2012). "The Real iPod: Elon Musk's Wild Idea for a 'Jetson Tunnel' from S.F. to L.A.". • Chin, Jeffrey C.; Gray, Justin S.; Jones, Scott M.; Breton, Jeffrey J. (January 2015). Open-Source Conceptual Sizing Models for the Hyperloop Passenger Pod (PDF). 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. January 5–9, 2015.Kissimmee, Florida. • IJSART (March 2013) “Construction Details and Safety Features of Fastest Mode of Transportation ‘Hyperloop’” . • Official_Crowd_Storm_Documentation:“Hyperloop_Transporation_Technolo gies.pdf”.