modification in chopper for unified uses-capstone project-ii

7/30/2019 Modification in Chopper for Unified Uses-capstone Project-II

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Transforming Education Transforming India

CAPSTONE PROJECT-II

MODIFICATION IN CHOPPER FOR UNIFIED USES

SUBMITTED TO: SUBMITTED BY:

MR. SUDARSHI RAKESH (MENTOR) OMKAR KUMAR JHA - 10902923

DEPT. OF MECHANICAL ENGINEERING (M3904) SHEKHAR PATAKU - 10902017

Sig: PRANAV KUMAR - 10903323

..

LOVELY PROFESSIONAL UNIVERSITY

PHAGWARA (PB)


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CERTIFICATE

This is to certify that.................................... Bearing Registration no. ......................

Has completed capstone project titled,

............................................................................................ Under my guidance and

supervision. To the best of my knowledge, the present work is the result of their

original investigation and study. No part of the dissertation has ever been

submitted for any other degree at any University.

The dissertation is fit for submission and the partial fulfillment of the conditions

for the award of partial degree

Signature and Name of the Research Supervisor

Designation

School

Lovely Professional University

Phagwara, Punjab.

Date:


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DECLARATION

We hereby declare that each contents of this project report are our own. Anythinghere mentioned is for educational purpose; hence some contents are beingtaken/analyzed from data from internet, Tata steel, books etc. So, there for, it issolely dedicated to the project guide, student and Lovely Professional University,

under department of mechanical engineering (M3904) for capstone projectpurpose.

- OMKAR KUMAR JHA- PRANAV KUMAR- SHEKHAR PATAKU


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ACKNOWLEDGEMENT

First of all, On behalf of the Department of Mechanical Engineering (M3904), wewish to extend our heartfelt gratitude to LOVELY PROFESSIONALUNIVERSITY, PHAGWARA (PB) for giving the opportunity to get familiar withand conduct project work. We took this opportunity to convey our sincere thanksto Mr. Aditya Veer Gautam (COD) for providing guidance, moral support, andmodalities to conduct this project.

We would like to thank our Mentor Mr. Sudarshi Rakesh for coordinating andhelping us during the project. We also extend our sincere thanks to all otherofficials of LPU for providing valuable information and their inputs for the studyover project to us. We would like to express our thanks to all the people at LPUand MECHANICAL SCHOOL as well who made our project duration verypleasant and comfortable and for all their hospitality extended to us.

We sincerely thank to all the people who have given a lot of effort by guiding theproject for so many days.

-Thanks and Regards


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TABLE OF CONTENTS

1. INTRODUCTION062. TYPES..073. FLIGHT MECHANISM/WORKING..084. THE PROJECT....135. CHOPPER ANATOMY...156. THE MODIFICATIONS..167. MODIFICATION DETAILS...178. FINAL WORK DESCRIPTION .21


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INTRODUCTION

In general aeroplane is abbreviated by the words aero means air and plane means

which can float over it.

In early of 1700 , the invention take place by wright brothers based on the

imagination over the great poet, scientist, musician, artist, and a multitalented

people named leo-nardo-da-vinchi.(name may pronounced differently). He (leo)

imagined that like an bird human can also fly or float on air. He also designed a

gladiator type equipment which cause some of the human life in danger .further in

late 19th

century Wright Brother completed the successful experiment to fly its

machine in the sky for some hours. That was the best milestone of the world

science.

Our project is mainly based over the different types of chopper, its specifications,

working, special aspects, and study of possible modification in it to ease human

beings.

Technically there is no any full stop in the invention into the science. If there is one

science or equipment is under working then there will be more and more introduce

in the new technology further days continuously.

In this project we have studied the all components working and tried to modify it

according to our project requirements that are solely based upon certain criteria

discussed further in detail section.


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WORKING

Aircraft/chopper can be sub-divided according to the means of propulsion they

use.

(i)UnpoweredAircraft that primarily intended for unpowered flight include gliders (sometimes

called sailplanes), hang gliders, and para gliders. These are mainly used for

recreation. After launch, further energy is obtained through the skillful exploitation

ofrising air in the atmosphere. Gliders that are used for the sport ofgliding have

high aerodynamic efficiency. The highest lift-to-drag ratio is 70:1, though 50:1 is

more common. Glider flights of thousands of kilometres at average speeds over

200 km/h have been achieved. The glider is most commonly launched by a tow-

plane or by a winch. Some gliders, called motor gliders, are equipped with engines

(often retractable) and some are capable of self-launching. The most numerous

unpowered aircraft are hang gliders and paragliders. These are foot-launched and

are generally slower, smaller and less expensive than sailplanes. Hang gliders most

often have flexible wings which are given shape by a frame, though some have

rigid wings. This is in contrast to paragliders which have no frames in their wings.

Military gliders have been used in war to deliver assault troops, and specialised

gliders have been used in atmospheric and aerodynamic research. Experimental

aircraft and winged spacecraft have also made unpowered landings.

(ii)PropellerSmaller and older propeller aircraft make use of reciprocating internal combustion

engines that turns a propeller to create thrust. They are quieter than jet aircraft, but

they fly at lower speeds, and have lower load capacity compared to similar sized
http://en.wikipedia.org/wiki/Glider_%28sailplane%29http://en.wikipedia.org/wiki/Hang_gliderhttp://en.wikipedia.org/wiki/Paragliderhttp://en.wikipedia.org/wiki/Lift_%28soaring%29http://en.wikipedia.org/wiki/Atmospherehttp://en.wikipedia.org/wiki/Glidinghttp://en.wikipedia.org/wiki/Lift-to-drag_ratiohttp://en.wikipedia.org/wiki/Motor_gliderhttp://en.wikipedia.org/wiki/Military_gliderhttp://en.wikipedia.org/wiki/Aerodynamicshttp://en.wikipedia.org/wiki/Experimental_aircrafthttp://en.wikipedia.org/wiki/Experimental_aircrafthttp://en.wikipedia.org/wiki/Spacecrafthttp://en.wikipedia.org/wiki/Internal_combustion_enginehttp://en.wikipedia.org/wiki/Internal_combustion_enginehttp://en.wikipedia.org/wiki/Propeller_%28aircraft%29http://en.wikipedia.org/wiki/Thrusthttp://en.wikipedia.org/wiki/Thrusthttp://en.wikipedia.org/wiki/Propeller_%28aircraft%29http://en.wikipedia.org/wiki/Internal_combustion_enginehttp://en.wikipedia.org/wiki/Internal_combustion_enginehttp://en.wikipedia.org/wiki/Internal_combustion_enginehttp://en.wikipedia.org/wiki/Spacecrafthttp://en.wikipedia.org/wiki/Experimental_aircrafthttp://en.wikipedia.org/wiki/Experimental_aircrafthttp://en.wikipedia.org/wiki/Experimental_aircrafthttp://en.wikipedia.org/wiki/Aerodynamicshttp://en.wikipedia.org/wiki/Military_gliderhttp://en.wikipedia.org/wiki/Motor_gliderhttp://en.wikipedia.org/wiki/Lift-to-drag_ratiohttp://en.wikipedia.org/wiki/Glidinghttp://en.wikipedia.org/wiki/Atmospherehttp://en.wikipedia.org/wiki/Lift_%28soaring%29http://en.wikipedia.org/wiki/Paragliderhttp://en.wikipedia.org/wiki/Hang_gliderhttp://en.wikipedia.org/wiki/Glider_%28sailplane%29


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jet powered aircraft. However, they are significantly cheaper and much more

economical than jets, and are generally the best option for people who need to

transport a few passengers and/or small amounts of cargo. They are also the

aircraft of choice for pilots who wish to own an aircraft.

Turboprop aircraft are a halfway point between propeller and jet: they use a turbine

engine similar to a jet to turn propellers. These aircraft are popular with commuter

and regional airlines, as they tend to be more economical on shorter journeys.

(iii) JetA Ukrainian An-225 Mriya is the world's largest fixed-wing aircraft.

Jet aircraft make use ofturbines for the creation of thrust. These engines are much

more powerful than a reciprocating engine. As a consequence, they have greater

weight capacity and fly faster than propeller driven aircraft. One drawback,

however, is that they are noisy; this makes jet aircraft a source ofnoise pollution.

However, turbofanjet engines are quieter, and they have seen widespread usage

partly for that reason.

The jet aircraft was developed in Germany in 1931. The first jet was the Heinkel

He 178, which was tested at Germany's Marienehe Airfield in 1939. In 1943 the

Messerschmitt Me 262, the first jet fighter aircraft, went into service in the German

Luftwaffe. In the early 1950s, only a few years after the first jet was produced in

large numbers, the De Havilland Comet became the world's first jet airliner.

However, the early Comets were beset by structural problems discovered after

numerous pressurisation and depressurisation cycles, leading to extensive

redesigns.
http://en.wikipedia.org/wiki/Turboprophttp://en.wikipedia.org/wiki/Turbinehttp://en.wikipedia.org/wiki/An-225_Mriyahttp://en.wikipedia.org/wiki/Turbinehttp://en.wikipedia.org/wiki/Noise_pollutionhttp://en.wikipedia.org/wiki/Turbofanhttp://en.wikipedia.org/wiki/Heinkel_He_178http://en.wikipedia.org/wiki/Heinkel_He_178http://en.wikipedia.org/wiki/Messerschmitt_Me_262http://en.wikipedia.org/wiki/Luftwaffehttp://en.wikipedia.org/wiki/De_Havilland_Comethttp://en.wikipedia.org/wiki/De_Havilland_Comethttp://en.wikipedia.org/wiki/Luftwaffehttp://en.wikipedia.org/wiki/Messerschmitt_Me_262http://en.wikipedia.org/wiki/Heinkel_He_178http://en.wikipedia.org/wiki/Heinkel_He_178http://en.wikipedia.org/wiki/Heinkel_He_178http://en.wikipedia.org/wiki/Turbofanhttp://en.wikipedia.org/wiki/Noise_pollutionhttp://en.wikipedia.org/wiki/Turbinehttp://en.wikipedia.org/wiki/An-225_Mriyahttp://en.wikipedia.org/wiki/Turbinehttp://en.wikipedia.org/wiki/Turboprop


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Most wide-body aircraft can carry hundreds of passengers and several tons of

cargo, and are able to travel for distances up to 17,000 km. Aircraft in this category

are the Boeing 747, Boeing 767, Boeing 777, Boeing 787 and Airbus A350, Airbus

A300/A310, Airbus A330, Airbus A340, Airbus A380, Lockheed L-1011 TriStar,

McDonnell Douglas DC-10, McDonnell Douglas MD-11, Ilyushin Il-86 and

Ilyushin Il-96.

Jet aircraft possess high cruising speeds (700 to 900 km/h, or 400 to 550 mph) and

high speeds for take-offand landing (150 to 250 km/h). Due to the speed needed

for takeoff and landing, jet aircraft make use offlaps and leading edge devices for

the control of lift and speed, as well as thrust reversers to direct the airflow

forward, slowing down the aircraft upon landing.

(iv)Supersonic jetSupersonic aircraft, such as military fighters and bombers, Concorde, and others,

make use of turbines (often utilising afterburners), that generate the huge amounts

of power for flight faster than the speed of the sound. Flight at supersonic speed

creates more noise than flight at subsonic speeds, due to the phenomenon ofsonic

booms. This limits supersonic flights to areas of low population density or open

ocean. When approaching an area of heavier population density, supersonic aircraft

are obliged to fly at subsonic speed.

Due to the high costs, limited areas of use and low demand there are no longer any

supersonic aircraft in use by any major airline. The last Concorde flight was on 26

November 2003.
http://en.wikipedia.org/wiki/Tonhttp://en.wikipedia.org/wiki/Boeing_747http://en.wikipedia.org/wiki/Boeing_767http://en.wikipedia.org/wiki/Boeing_777http://en.wikipedia.org/wiki/Boeing_787http://en.wikipedia.org/wiki/Airbus_A350http://en.wikipedia.org/wiki/Airbus_A300http://en.wikipedia.org/wiki/Airbus_A300http://en.wikipedia.org/wiki/Airbus_A310http://en.wikipedia.org/wiki/Airbus_A330http://en.wikipedia.org/wiki/Airbus_A340http://en.wikipedia.org/wiki/Airbus_A380http://en.wikipedia.org/wiki/Lockheed_L-1011_TriStarhttp://en.wikipedia.org/wiki/McDonnell_Douglas_DC-10http://en.wikipedia.org/wiki/McDonnell_Douglas_MD-11http://en.wikipedia.org/wiki/Ilyushin_Il-86http://en.wikipedia.org/wiki/Ilyushin_Il-96http://en.wikipedia.org/wiki/Take-offhttp://en.wikipedia.org/wiki/Landinghttp://en.wikipedia.org/wiki/Flap_%28aircraft%29http://en.wikipedia.org/wiki/Leading_edge_slatshttp://en.wikipedia.org/wiki/Thrust_reverserhttp://en.wikipedia.org/wiki/Supersonichttp://en.wikipedia.org/wiki/Bomberhttp://en.wikipedia.org/wiki/Concordehttp://en.wikipedia.org/wiki/Afterburnerhttp://en.wikipedia.org/wiki/Sonic_boomhttp://en.wikipedia.org/wiki/Sonic_boomhttp://en.wikipedia.org/wiki/Population_densityhttp://en.wikipedia.org/wiki/Population_densityhttp://en.wikipedia.org/wiki/Sonic_boomhttp://en.wikipedia.org/wiki/Sonic_boomhttp://en.wikipedia.org/wiki/Sonic_boomhttp://en.wikipedia.org/wiki/Afterburnerhttp://en.wikipedia.org/wiki/Concordehttp://en.wikipedia.org/wiki/Bomberhttp://en.wikipedia.org/wiki/Supersonichttp://en.wikipedia.org/wiki/Thrust_reverserhttp://en.wikipedia.org/wiki/Leading_edge_slatshttp://en.wikipedia.org/wiki/Flap_%28aircraft%29http://en.wikipedia.org/wiki/Landinghttp://en.wikipedia.org/wiki/Take-offhttp://en.wikipedia.org/wiki/Ilyushin_Il-96http://en.wikipedia.org/wiki/Ilyushin_Il-86http://en.wikipedia.org/wiki/McDonnell_Douglas_MD-11http://en.wikipedia.org/wiki/McDonnell_Douglas_DC-10http://en.wikipedia.org/wiki/Lockheed_L-1011_TriStarhttp://en.wikipedia.org/wiki/Airbus_A380http://en.wikipedia.org/wiki/Airbus_A340http://en.wikipedia.org/wiki/Airbus_A330http://en.wikipedia.org/wiki/Airbus_A310http://en.wikipedia.org/wiki/Airbus_A300http://en.wikipedia.org/wiki/Airbus_A300http://en.wikipedia.org/wiki/Airbus_A300http://en.wikipedia.org/wiki/Airbus_A350http://en.wikipedia.org/wiki/Boeing_787http://en.wikipedia.org/wiki/Boeing_777http://en.wikipedia.org/wiki/Boeing_767http://en.wikipedia.org/wiki/Boeing_747http://en.wikipedia.org/wiki/Ton


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(v)Solar-poweredA solar-powered aircraft generates the needed energy by means ofsolar cells. On

8 July 2010 the manned Solar Impulse became the first solar-powered aeroplane to

fly through an entire night.

(vi) UnmannedAn aircraft is said to be 'unmanned' when there is no person aboard the aircraft and

control is achieved remotely or via other means such as gyroscopes or other forms

of autonomous control. The aircraft is controlled only by remote controls or other

electronic devices.

(vii) Rocket-poweredExperimental rocket powered aircraft were developed by the Germans as early as

World War II , and about 29 were manufactured and deployed. The first fixed wing

aircraft to break the sound barrier in level flight was a rocket planethe Bell X-1.

The later North American X-15 was another important rocket plane that broke

many speed and altitude records and laid much of the groundwork for later aircraft

and spacecraft design. Rocket aircraft are not in common usage today, although

rocket-assisted takeoffs are used for some military aircraft. SpaceShipOne is a well

known current rocket aircraft; it is the prototype for development of a commercial

sub-orbital passenger service. Another rocket plane is the XCOR EZ-Rocket.

The construction of the aircraft is basically based over the frame body and use as

well.
http://en.wikipedia.org/wiki/Solar_cellhttp://en.wikipedia.org/wiki/Solar_Impulsehttp://en.wikipedia.org/wiki/World_War_IIhttp://en.wikipedia.org/wiki/Sound_barrierhttp://en.wikipedia.org/wiki/Bell_X-1http://en.wikipedia.org/wiki/North_American_X-15http://en.wikipedia.org/wiki/Flight_altitude_recordhttp://en.wikipedia.org/wiki/Spacecrafthttp://en.wikipedia.org/wiki/Assisted_takeoffhttp://en.wikipedia.org/wiki/Scaled_Composites_SpaceShipOnehttp://en.wikipedia.org/wiki/Sub-orbital_spaceflighthttp://en.wikipedia.org/wiki/XCOR_EZ-Rockethttp://en.wikipedia.org/wiki/XCOR_EZ-Rockethttp://en.wikipedia.org/wiki/Sub-orbital_spaceflighthttp://en.wikipedia.org/wiki/Scaled_Composites_SpaceShipOnehttp://en.wikipedia.org/wiki/Assisted_takeoffhttp://en.wikipedia.org/wiki/Spacecrafthttp://en.wikipedia.org/wiki/Flight_altitude_recordhttp://en.wikipedia.org/wiki/North_American_X-15http://en.wikipedia.org/wiki/Bell_X-1http://en.wikipedia.org/wiki/Sound_barrierhttp://en.wikipedia.org/wiki/World_War_IIhttp://en.wikipedia.org/wiki/Solar_Impulsehttp://en.wikipedia.org/wiki/Solar_cell


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If the craft is going to use for navigation only it will have different characteristics

regarding the weight and frame with respect to drag force over it.

So for the different purpose the craft is crafted under crucial conditions which are

highly precise in nature and the construction needed 100% accuracy as well. Main

consideration is the weight of the craft as well as the speed gain by its engine, its

height of fly and the propulsion system.

The above figure is the ray diagram of the jet having different views. During the

construction various forces are also comes into consideration. Mainly some forces

are essential that are drag, air pressure over plane,exhaust pressure and lift

pressure. so over all the main thing that Is taken in mind that the body of the craft

is made so much light weight that less power should be consumed and greater

efficiency can be obtained within the limit. Further the safety cant be ignored. So

proper insulation and the body under atmospheric pressure condition should be

maintained within the craft for public safety.

There for the optimum light weight and good quality product and technology is

used which have 99.99% of accuracy to every component either it is a single screw

or a rotor or engine.


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WORKING OF JET ENGINES

Generally the jet engines were traditionally made but further in the era the new

invention comes into science and they replaced some components but over all

process is remain constant yet.

Here in the diagram:

This diagram shows that air comes to inlet where it is already compressed to 40

times its volume and the mixture is rich enough as 1:20(fuel: air).the mixing is

takes place into the fuel injection area before the converging section of the engine.

After then the combustion occurs and the heavy blast caused the axial thrust over

the back section of the plane or called supersonic exhaust in the exhaust area which

gives the engine a boost to move forward.


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Further the new invention came which is introduced into the mainframe of the craft

engine technology.

Here from the picture it will be well noticed:

In fig (c) the converging section is as it was in the past. But in fig (b) there is the

two sections extra which provides more compression and the combustion of the

fuel. And so the greater efficiency can be obtained. Further in fig (a) the

compression area is again shifted in long section but it consist more advanced

technology and hence used some compressors which give more and more efficient

compression of the air more than 40 % to the conventional technique. And so the

combustion area is with the exhaust


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THE PROJECT

CHOPPER

(CONSTRUCTION AND COMPONENT WORKING)

Lets start with the

FUSELAGE: - it is the main front of the craft which is used to cut the air pressure

and safety of the body when the turning and bending occurs

CABIN DOORS: - the doors which are totally air locked and pressure controlled,

used to in and out of the pilot and the passengers.

ENGINE MOUNT: - the space which is used to mounting the heavy engine

assembly where it can be well function able and is situated at the center of the

body because the craft having weight is concentrated over the mid point where if

the extra load is applied further then the controlling is very well easy due to

normalization of all the force component working during flight

TRANSMISSION: -the assembly of the gears and the shaft

MAST: -the shaft which is used to transfer the torque to the blades to rotate.

CRAWLING: - It is the cover which saves the engine from dust, water and other

partials.

SWASH PLATE: - the two or more rode which is installed to keep the blades

stationary to its axis during rotation and due to centrifugal force.

STABLIZER BAR: -the bar or locker which is used to fasten the blade over the mast

so that due to force (centrifugal and weight) acting downward over the craft can be

prevented to unbolted or breakdown.


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ROTOR: - the blades which rotate and lift the craft upward by creating the air

density difference to upside down having 1500 rpm at final.

TAIL ROTOR DRIVE SHAFT: - a shaft which is used to transmit the power to the

rear blades which help to steer the craft in the air.

SYNCHRONISED ELEVATOR: - the elevator which can control the movement of

the craft by reducing or increasing the air pressure over the craft.


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CHOPPER ANATOMY


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THE MODIFICATIONS

(i) ROTOR BLADES(ii) POWER AND TRANSMISSION(iii) COMPONENT SYNCHRONISATION(iv) REMOTE CONTROL(v) GEAR BOX REPLACEMENT(vi) MULTI USE HOUSING(vii) SURVILIANCE MONITOR/SPY CAM(viii) INSECTISIDE SPRAY COMPONENTS(ix) HIGH ALTITUDE AND CONTOLE FUNCTION


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MODIFICATION DETAILS:-

ROTOR BLADES:-

Spec:- Shape: Symmetrical wing Length:500mm Width:13mm Shaft Diameter:70mm Weight:40.3g/set


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It helps the chopper to cut the upper side air to reduce the density of air on upper

section which helps it to drift upward.

The selection of special rotor was totally under consideration of actual use as the

project is based trails so the prototype was available for low altitude thus afterreplacing high capacity carbon fiber blades that reduces the weight as well as less

friction to air resulting in more power over less RPM.

POWER AND TRANSMISSION:-According to our design requirements it was necessary to fly at least 100-150 feet

During project checkup so that its efficiency for long time fly may increased.

COMPONENT SYNCHRONISATION

As per high speed requirement and for obtaining high altitude it is

necessary to modify the power transmitting shaft to enable high power

transmission with less friction and other losses.


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As per requirement of the present project the circuit also gets replaced by higher

degree of specification like:-Manufacturer: - align corp.

Type: - Starter STQ 100

Voltage 20-30 volts

Rpm regulation -1700-3600

Receiver- 500 feet (L and H)


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Four stroke 1 hp gasoline engineDisplacement: 37.7cc

Bore*Stroke: 39*30mm

Rated Power: 4kw/7000r/min

Max Power: 5.8-.9kw/7000r/min

Start Type: Recoil starter

Fuel Volume (L): 4lit.

Fuel Consumption: 400-480/Kw h.

Cooling System: Forced air

Ignition system: TCI

Size (L*W*H): 204*234*230


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US $ 90 - 120 / Set

This proposed engine is basic requirement for the power generation. This engine is

capable of lifting ~11-12 kg for 2.5 max hours. With this specified engine apropeller can rotate with such thrust that multi operation can be done.

Sprinkler

Automated sprinkler irrigation achieved by automatically rotating the sprinkler

pipe or boom, supplying water to the sprinkler heads or nozzles, as a radius from

the center of the field to be irrigated. Water is delivered to the center or pivot point

of the system. The pipe is supported above the crop by towers at fixed spacing and

propelled by pneumatic, mechanical, hydraulic, or electric power on wheels orskids in fixed circular paths at uniform angular speeds. Water is applied at a

uniform rate by progressive increase of nozzle size from the pivot to the end of the

line. The depth of water applied is determined by the rate of travel of the system.

Single units are ordinarily about 1,250 to 1,300 feet long and irrigate about a 130-

acre circular area.

Bill of extra material are as follows:-

EQUIPMENT RATING QUANTITYStorage cylinder 8-10 kg (l/B acc. To size) 1

Connecting pipes 10-12 mm dia. and 1 mlong

1

Connecting gear set 10:1 ratio to driver 2

Connecting shaft(gear) a/c to gear hub 2

Sprinkler cup 60-70 mm dia. 2

Rotating impeller - 2

Base rods a/c to initial design 2

Electrical Wire -do- 1 mSoldering rod and heater -d0- 1

Body sheet Aluminum ( sheet work) a/c to design

Welding system Initial Initial


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STORAGE CYLINDER

SOLENIOD

VALVE

DRIVER GEAR

DRIVEN GEAR 2DRIVEN GEAR 1

SPRINKLER

CUP 2

SPRINKLER

CUP 1

Sprinkler

nozzle


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FINAL WORK DESCRIPTION:

1. SO FINALLY WE HAVE CAME TO THE CONCLUSION THAT INCASE OF FARMERS IN INDIA, HAVING PROBLEM IN

CULTIVATING THEIR CROPS WITH MODERN TECHNLOGY.OUR

PROJECT IS BASED ON THE INVENSION AND INTRODUCING OUR

PROJECT INTO FARMERS LIFE. OUR PROJECT MAY HELP THEM

TO SPRAY INSECTICIDES IN THE CROPS AND CAN PREVENTS

FLIES TO SET THEIR HOME IN CROP AS THE CHOPPER APPLIES

GREAT THRUST IN DOWNWARD DIRECTION .DUE TO HEAVY

FLOW OF AIR THE CROPS GOT SAPERATED.AND HENCE PROPER

MIXING IS POSSIBLE.2. FURTHER PROPOSED MODIFICATIONS ARE UPON THE SECURITY

MATTER AS WE ARE UPTO ATTACHING A WIRELESS,

NIGHTVISION, ULTRA POWERD CAMS THAT CAN SEND THE

REMOTE VIDEO ONLINE TO OUR CONTROL STATION. WITH THE

HELP OF ONLINE STREAMING/TRANSMISSION SECURITY AND

SURVILIANCE WILL BE EASE FOR PERSONAL AND INDUSTRIAL

OR OTHERS. WITH THE HELP OF CAM THE TRAFFIC

INFORMATION CAN ALSO BE OBTAINED WHICH HELPS THERIDERS. FIRE FIGHTING CAN ALSO BE EASE IN CASE OF

EMERGANCY AND IF THE MACHINE IS PROPERLY INSULATED

AND MODIFIED THEN IT CAN SPRAY THE CO2 REMOTELY IN

FIRE ZONE

3. OTHER PROPOSAL IS BASED UPON INTEGRATION OF ENERGYEFFICIENT METHOD SUCH AS SOLAR ENERGY.WE HAVE

DECIDED TO COVER UP THE WHOLE SURFACE BY THIN SOLAR

PANNEL/PLATES SO THAT IN DAY HOURS THE BATTERY POWERCAN BE SAVED AND HENCE IT GOT CHARGED REGULARLY

WITH FLYING.DUE TO SOLAR POWER THE BATTERY WILL BE

AUTOMETICALLY CHARGED AND REST ENERGY MAY UTILISE

TO FLY OF THE CHOPPER AND HENCE THE MACHINE CAN BE


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STABLE FOR LONG TIME IN AIR.HENCE INCREASE IN EFFICIENY

WITH CONSERVATION ON ENERGY.

4. AS IT CAN FLY IN AIR, IT CAN ALSO RUN IN WATER ALSO BYSOME BASIC MODIFICATION IN BASE WITH ATTACHMENT OF

COMPONENT IN BASE OF CHOPPER..

Due to money problem the actual machine is not feasible to construct/assemble on

this stage because it costs total of 20-25k Rs. But this project is very good and

innovative for farmer to spray their crops without entering into field. Entering into

field cost more money and time with destroy some crop plants. Due to chopper

mechanism and its high density of air flow to downward direction the medicine can

uniformly sprayed without any loss.

SO HERE IT IS CONCLUDED THAT AFTER SOME MODIFICATION A

SIMPLE CHOPPER CAN UTILZE IN MULTIPLE WAYS...

IF YOU HAVE ANY NEW IDEAS OR RECOMANDATION, IT WILL BE AN

HONOUR TO US TO IMPLIMENT ON IT.

THANKS..


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REFRENCES

http://yaymicro.com/stock-image/crop-field-sprinkler/1260080 www.kifco.com www.waterreels.com/SportsFields.ivnu www.ul.com Building Materials Sprinklers en.wikipedia.org/wiki/Engine www.alibaba.com/showroom/1-hp-gasoline-engine.html www.nextag.com/motor-1-hp/stores-html en.wikipedia.org/wiki/Chopper_(electronics) www.edaboard.com/thread241672.htm

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modification in chopper for unified uses-capstone project-ii

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