NANOROBOTICS RESPIROCYTES Smrithi Sasidharan (Btech 3rd Year‚ ECE) Varsha Vasudev(BTech 3rd Year‚ EB ) Amrita School of Engineering Bangalore‚ Model Engineering College‚ Kochi ABSTRACT Molecules are the universal basic building blocks of all the elements of nature‚ whether it be living or non-living. The complex human body with its interdependent physiological subsystems can be scaled down to a collection of various types of molecules. The accessibility to the molecular and atomic components
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reactive power with the grid. Running on different operating conditions‚ the rotor of DFIG has different energy flow directions. Although energy always flows from stator to grid‚ sub-synchronous operating state‚ the energy flows from the grid to the rotor; super-synchronous operating state‚ the energy flows in an opposite way. Therefore‚ in order to make the system run in a wide speed range‚ it has to ensure that the rotor energy can flow in double-way. This process is achieved with GSC by regulating
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DESIGN OF TESLA TURBINE Abstract:- The Tesla turbine is a bladeless centripetal flow turbine patented by Nikola Tesla in 1913. It is referred to as a bladeless turbine because it uses the boundary layer effect and not a fluid impinging upon the blades as in a conventional turbine. The Tesla turbine is also known as the boundary layer turbine‚ cohesion-type turbine‚ and Prandtl layer turbine (after Ludwig Prandtl). Bioengineering researchers have referred
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Nikola Tesla and Induction motor Name: Boris Halada Academic year: 2014/2015 Language supervisor: PaedDr. Dagmar Rusková‚ PhD. Nikola Tesla (10 July 1856 – 7 January 1943) was a Serbian American inventor‚ electrical engineer‚ mechanical engineer‚ and futurist best known for his contributions to the design of the modern alternating current (AC) electricity supply system Tesla gained experience in telephony and electrical engineering before immigrating to the United States in 1884 to work for Thomas
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uniform air gap is shown in Figure Q1(c). The mutual inductance between the rotor and the stator is given by Lsr = 0.5 cos θ Henries The windings are supplied with either of two sources: Source A: Source B: 3 A DC 6 A r.m.s f = 50 Hz The rotor is locked at θ = 50°. What is the torque developed for the following source connections: (i) (ii) Source A to both windings Source A to the rotor and source B to the stator. Rotor axis [6 marks] [7 marks] θ = 50° (locked) Stator axis Figure
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control systems‚ robotics‚ mecatronics‚ electric vehicles‚ high speed transportation etc. SYNCHRONOUS RELUCTANCE MOTORS * A reluctance motor is a type of synchronous electric motor which induces non-permanent magnetic poles on the ferromagnetic rotor. * Torque is generated through the phenomenon of magnetic reluctance. Operating principle * Whenever a piece of ferromagnetic material is located in a magnetic field a force is exerted upon the material tending to bring it
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be familiar with some of the terminology associated with it. The rotor is the spinning component that has wheels and blades attached to it. The blade is the component that extracts energy from the steam. There are two basic types of turbine designs. One is called the "impulse" design in which the rotor turns due to the force of steam on the blades. The other is called a "reaction" design‚ and it works on the principle that the rotor derives its rotational force from the steam as it leaves the blades
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corresponds to a physical position of the rotor. The frequency is exactly determined by the formula f = RPM x p / 120 where f is the frequency (Hz)‚ RPM is the rotor speed (revolutions per minute) and p is the number of poles formed by the stator windings. A synchronous generator is essentially the same machine as a synchronous motor. The magnetic field of the rotor is supplied by direct current or permanent
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with fuel and ignited by the ignition system. The combustion is a constant process that heats and expands the released gases before they reach the two-stage axial turbine. The gases clash on the turbine blades‚ which causes a rotation of the common rotor shaft. After the gases leave the turbines they flow into the APU exhaust and are released in the open
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"an artificial horizon". When in a left turn‚ the blue portion of the ball will have rolled to the right‚ as though you were looking at the horizon over the nose of the aircraft. In a right turn‚ the blue portion will have rolled to the left. The rotor‚ mounted in a sealed housing‚ spins in a horizontal plane about the vertical axis. The housing pivots about the lateral axis on a gimbal‚ which in turn is free to pivot about the longitudinal axis. The instrument case is the third gimbal necessary
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