Showing posts with label aviation. Show all posts
Showing posts with label aviation. Show all posts

Monday, December 12, 2011

DC SOURCES OF ELECTRICITY

batteries is divided into two groups
  • primary cell ( dry cell / leclanche cell )
  • secondary cell
now we are going to discuss about secondary cell

SECONDARY CELL.
-known as storage cell.
-any kind of electrolytic cell in which the electrochemical reaction that releases energy is reversible.
-must be charged before used.
-examples of usages :
  • laptop
  • handphone cell
types of secondary cell
  • LEAD ACID CELLS
  • NICKEL CADMIUM CELL ( NiCAD )

LEAD ACID CELLS

purpose :
  • power supply to aircraft during emergency and starting.
construction:
  • +ve plate used lead peroxide fill with antimony
  • -ve plate used spongy lead and has extra plate than +ve plate
  • electrolye is dilute sulphuric acid with water 30% acid and 70% water
  • casing made up of high impact plastic
  • vent screw type which allow distilled water to adjust electrolyte level.
  • separator prevents +ve and -ve plate from touching but allow sulphuric acid to pass through.
  • 6 / 12 cells, each cell rate 2.1 volts.
indication of fully charged condition:

-terminal voltage
  • 2.7V/ cell on charged
  • 2.1 V/ cell off charged
  • 1.8 V/cell discharged
terminal voltage between 30.0 to 32.4 V ( on charge ), if terminal voltage below 28.5 V , it should be withdrawn from service.

voltage test :
  • specific gravity of electrolyte - 1.275 and 1.300 at 80. use hydrometer to check
  • gassing freely

fully discharge
  • sulphation occur and electrolyte become water.
  • S.G will be low (1.150) due to internal resistance becomes high.
  • both plate becomes white lead sulphate : act as high resistance
  • sulphation occurs when battery discharged
capacity
  • ability to produce a given amount of current for specific time e.g 1A for 1 Hour
  • more than 80% efficiency fit for aircraft use
efficiency (%) = output capacity / rated capacity X 100

factor affecting capacity of a battery :
  • num of plate
  • plate area
  • strength of electrolyte
  • temperature
proper servicing is required on this cell :
  • keep battery clean , all terminals tight and free of corrosions.
  • electrolyte level should 1/4 above the plates , if low add distilled water and not acid.
  • when mixing electrolyte always add ACID to WATER.
  • coat the battery terminals with petroleum jelly or general purpose grease in order to prevent corrosion or oxidization on the terminals.

two types charging :

- Constant current charging
  • most effective
  • charge battery by supplying current at a constant rate ( manually )
  • when charging more than one battery, it must be connected in series and battery voltage must not exceed the charging voltage.
  • several batteries in series , charge at the lowest battery capacity.
  • need monitoring during charging
  • temperature must not exceed 60 C as for the electrolyte it must be below 43C
  • when cells commence gassing, the voltage and relative density should be measured periodically.

-Constant voltage charging
  • when battery connected in an aircraft , car or a other vehicles
  • generating voltage system slightly higher than battery voltage
  • the amount of current flow into a battery is determined by the state charge of battery.
  • no need monitoring device

capacity test :
  • carried out after initial charge
  • carried out 3 monthly
  • at any time if capacity in doubt
  • acceptable capacity for use in aircraft is 80% and above

insulation test :
  • carried out at a periodic of time
  • at any time the electrolyte suspected leakage.
  • place a fully charged battery on metal plate , test between terminal and plate using 250 V insulation tester ( megger ), reading must not less than 1 Mili Ohms.

storage :
  • stored clean, dry, well ventilated area
  • always stored in fully charged condition this is to prevent sulphation to occur.
  • give re freshening charged every 2 to 4 weeks.

safety and precaution :
  • lead acid and Nicad cell must be stored in separate room.
  • do not wear rings, or metal strap.

to be continued......................


Monday, August 1, 2011

ferrous metal part 1

what is ferrous metal?
  • ferrous metal is metallic material that contains at least 50% iron
the simplest ferrous metal is
  • plain carbon steel- consisting of less than one percent carbon.
parts that are made from ferrous metal is
  • aircraft engines
  • engine mounting
  • hydraulic lines
  • control cables and etc
metals ---> ferrous metal ---> iron as the base metal ---> iron is the most common metals used---> iron Ore is mined producing IRON (Pig Iron)


GENERAL CHARACTERISTIC OF METAL
* the properties of a metal, which influence its suitability as a material for engineering use.

1. brittleness
  • the property of a metal to break when bent, defamed, or hammered.
  • it is the resistance to change in the relative position of the molecules within the material.
  • cast iron, cast aluminium and very hard steel are examples of brittle metals.
2. conductivity
  • the characteristic of a material , which makes it possible for it to transmit heat or electrical energy by conduction
3. ductility
  • the property , which allows metal to be drawn into thinner sections without breaking.
  • ductility allows materials like aluminium and copper to be drawn into very small wires.
4. elasticity
  • the capability of an object a material to be stretched and recover its size and shape after its deformation.
5. malleability
  • the characteristic of a material that allows it to be stretched and shaped by beating with a hammer or passing through rollers without breaking.
6. plasticity
  • the property of assuming a new shape when subjected to pressure
  • the new shape being retained after the pressure has been discontinued.
7. tenacity
  • this is the resistance a material offers against being pulled apart.
  • material which have good tenacity have a high tensile strength.
  • tensile strength of steel is high where as that of lead is low.


to be continued........

Tuesday, July 19, 2011

ATA CHAPTER

for my material and hardware subject, we were asked by our lecturer to do a little research before he explains the ATA CHAPTER. so this is the result of my research.

ATA CHAPTER NUMBER - provide a common referencing standard for all commercial aircraft documentation. this commonality permits greater ease of learning and understanding for pilots and engineers alike. the standard numbering system is controlled and published by the Air Transport Association.

ATA CHAPTERS

Aircraft General
ATA 05 - The limits/ Maintenance Checks
ATA 06- Dimensions and Areas
ATA 07- Lifting and Shoring
ATA 08- Leveling and weighing
ATA 09- Towing and taxiing
ATA 10- Parking, mooring, storage and return to service
ATA 11- placards and markings
ATA 12- Servicing - routine maintenance

Airframe Systems
ATA 20- standard practice
ATA 21- air conditioning
ATA 22- Auto flight
ATA 23- communications
ATA 24- Electrical powers
ATA 25- equipment/ furnishing
ATA 26- fire protection
ATA 27- flight controls
ATA 28- fuel
ATA 29- Hydraulic power
ATA 30- ice and rain protection
Ata 31- indicating/ recording systems
ATA 32- landing gear
ATA 33- lights
ATA 34- navigation
ATA 35- oxygen
ATA 36- pneumatic
ATA 37- vacuum
ATA 38- water/waste
ATA 45- central maintenance system
ATA 46- informations systems
ATA 47- nitrogen generation system
ATA 49- airborne auxiliary power
ATA 50- cargo and accessory compartment

Structure
ATA 51- standard practices and structures- general
ATA 52- doors
ATA 53- fuselage
ATA 54- nacelles/ pylons
ATA 55- Stabilizer
ATA 56- windows
ATA 57- wings

Power Plant
ATA 71- power plant- general
ATA 72- engine
ATA 73- engine - fuel and control
ATA 74- ignition
ATA 75- bleed air
ATA 76- Engine controls
ATA 77- engine indicating
ATA 78- exhaust
ATA 79- oil
ATA 80- starting

this is the list of ATA CHAPTER, that we, as the future aircraft engineers must memorise, and from what i see, there are many more ATA chapter that i missed here.

source of reference is here, so if there is any doubted or any mistakes that i have done, please do leave a comment.
p/s : don't comment on my grammar, i know my grammar suck -.-"