Monday, 17 August 2015

Night Shift Material

The Link - https://drive.google.com/file/d/0B4VLfbiiR_kbU1JvLWFaOUZENFE/view?usp=sharing

http://www.livemint.com/Home-Page/lD9Q8oKr2cSGWtLrynE0YI/India-should-look-at-efficient-lowcost-airports-IndiGos.html

https://onedrive.live.com/?cid=a0bc7de4467a7edc&id=a0bc7de4467a7edc%21833&ithint=folder,&authkey=!AMcfXYz48t_Zcak

https://onedrive.live.com/?cid=F333375EC88B32B8&id=F333375EC88B32B8%21104&authkey=%21AA_Xf4E3roWC-tI

Chapter 1 – Basic Radio
The word 'radio' means the radiation of electromagnetic waves conveying
information, and detection of such waves. Within this meaning, such applications
as telegraphy, telephony, television and a host of navigation aids are all classified
as radio. This volume is primarily concerned with the air navigation aids
commonly used worldwide.

Hertz not only verified Maxwell's prediction but also established
the speed of the radio waves and other properties. He showed that they can
propagate in a vacuum, and that they are stopped by a metallic screen (the
foundation of our present day radar). He calculated wavelengths for various
frequencies and determined the relationship between the two.
Propagation of radio waves
If a source of alternating voltage is connected to a wire (i.e. an aerial) an
oscillating current will be set up in the wire, the electrons of which move about a
mean position. The electric field present in the wire is accompanied by a magnetic
field and at a suitable frequency (in relation to the length of the aerial) both fields
radiate efficiently outward from the wire in the form of electromagnetic or radio
waves. In the earth environment these disturbances travel approximately at the
speed of light, that is,
186000 statute miles per second or
162000 nautical miles per second or
300000000 metres per second or
300000 kilometres per second.
As the waves are alternating fields, the terminology involved with alternating
currents will be looked into first, extending this to radio terminology. An a.c.
voltage in a wire reverses its direction a number of times every second.
Consequently, if a graph of the current in the wire is plotted against time, it will be
found that it is a sine curve


Cycle. A cycle is one complete series of values, or one complete process.

Hertz. One hertz is one cycle per second. The number of cycles per second is
expressed in hertz. (This term is a relatively recent adoption in honour of the
above-mentioned eminent scientist).

Amplitude. Amplitude of a wave is the maximum displacement, or the
maximum value it attains from its mean position during a cycle. It is both positive
and negative. (That part of the curve in Fig. 1.1. above the mean or time axis is
called positive and that part which is below the line is negative.)

Frequency (f). Frequency of an alternating current or a radio wave is the
number of cycles occurring in one second, expressed in hertz (Hz). For example,
500 Hz means 500 cycles per second. Since the number of cycles per second of
normal radio waves is very high it is usual to refer to them in terms of kilohertz,
megahertz and giga-hertz as follows:

1 cycle per second = 1 Hz
1000 Hz = 1 kHz (kilohertz)
1000 kHz = 1 MHz (megahertz)
1000 MHz = 1 GHz (giga hertz)

Wavelength (l). This is the physical distance travelled by the radio wave
during one complete cycle of transmission. It is defined as the distance between
successive crests or the distance between two consecutive points at which the
moving particles of the medium have the same displacement from the mean value
and are moving in the same direction.


Chapter 2 Radio Wave


Propagation

Simple Transmitter

The basic components of a simple radio transmitter are shown in Fig. 2.1.
Oscillator. The purpose of an oscillator is to provide a radio carrier wave. At
very high frequencies a unit called a magnetron may be used to produce the
oscillations.

RF Amplifier. The signals produced by the oscillator are too weak for
transmission and they must be amplified. This amplification is done at the RF
amplifier, which is coupled, to the oscillator, and the outgoing amplified signals
are fed to the modulator.

Microphone and AF Amplifier. Similarly, a microphone produces weak
audio signals, which are amplified by the AF amplifier unit. The amplified signals
are then fed to the modulator.

Modulator. In this unit the audio signals modulate the carrier waves by
varying the amplitude (amplitude modulation) or the frequency (frequency
modulation); the resultant modulated signals are fed for further amplification to
the power amplifier.

Power Amplifier. Modulated signals arriving at this unit (not shown in Fig.
2.1) are finally amplified (by stages if necessary) to the transmission level.
Aerial. Modulated and amplified signals are fed to the aerial by the power
amplifier and the electromagnetic radiation takes place.

General Properties of Radio Waves
1) In a given medium, radio waves travel at a constant speed.
2) When passing from one medium to another of different refractive index, the
velocity of the waves changes. The waves are also deflected towards the
medium of higher refractive index, that is, they change their direction.
3) Radio waves are reflected by objects commensurate with their wavelengths

Radio Spectrum

The electromagnetic spectrum starts at the lower end of the radio frequencies,
that is 30 Hz, and stretches to over ten million, million giga hertz where the
radiation takes the form of gamma radiation. In this vast spectrum, radio
frequencies occupy only a very small part. Different frequencies are found to have
different characteristics and in order to identify frequencies having similar
characteristics the full range of the radio spectrum is divided into various groups
called frequency bands. The frequency bands shown in Table 2.1 are
internationally recognised.
Table 2.1

Frequency band   Abbreviation    Frequencies     Wavelength
extremely low frequency ELF 30-300 Hz 10000-1000 km
voice frequency VF 300-3000 Hz 1000-100 km
very low frequency VLF 3-30 kHz 100-10 km
low frequency LF 30-300 kHz 10000-1000 m
medium frequency MF 300-3000 kHz 1000-100m
high frequency HF 3-30 MHz 100-10m
very high frequency VHF 30-300 MHz 10-1 m
ultra high frequency UHF 300-3000 MHz 100-10 cm
super high frequency SHF 3000-30000 MHz 10-1 cm
extremely high frequency EHF 30000- 300 000 MHz 1-0.1 cm

Radar L band 1000-2000 MHz
Radar S band. 2000-4000 MHz
Radar C band 4000-8000 MHz
Radar X band 8000-12500 MHz

It will, however, be appreciated that these divisions are not 'watertight'
divisions and the characteristics of a particular band may overlap above and below
the demarcation frequency limit in the table.

The earth and its surround

Before we set out to discuss the type of propagation, the properties and the
ranges available in the above frequency bands, let us take a quick look at the
physical elements present on and around the earth.

First of all, the shape of the earth: it is approximately a sphere. This means
that the horizon curves away with distance from the transmission point, and if the
radio waves travelled only in straight lines (as they would, by their basic property)
the reception ranges would be limited to 'optical' distance only. This distance is
given by the formula D = 1.0 SVH, where D is the range in nautical miles and H is
the height in it. Fortunately, we will soon see that radio waves do curve to a
greater or lesser extent with the surface of the earth and in the atmosphere, which
means that the above formula is seldom used.

The conductivity of the earth's surface itself varies: seawater provides a
medium of high conductivity whereas the conductivity of the land surface depends
on its composition. It is fairly high where the soil is rich loam, and very poor in
the sands of a desert or the polar ice caps. The terrain itself varies from flat plains
to tall mountains, from deserts to dense jungles.

Surrounding the earth, our atmosphere is rich in water vapour right up to the
height of the tropopause. Water vapour is the major cause of the weather and the
weather means precipitation, thunderstorms, lightning and so forth. Electrical
activity may be expected in any of these attributes of the weather. The other
characteristics of the atmosphere, pressure, density, temperature, all vary
continually, both horizontally along the surface and with height.
And finally, well above the earth's surface we have electrically conducting
belts of ionised layers caused by the ultraviolet rays of the sun.
Radio waves travel best in the free space. On and around the surface of the
earth they are influenced to a varying degree by the factors discussed in the
preceding paragraphs. We will now study these influences in detail.

Propagation: Surface Waves



When electromagnetic waves are radiated from an omni directional aerial,
some of the energy will travel along the surface of the earth. These waves, gliding
along the surface are called surface waves or ground waves. As we learnt earlier,
it is the nature of radio waves to travel in a straight line. However, in appropriate
conditions they tend to follow the earth's surface giving us increased ranges. But,
what causes them to curve with the surface?

Primarily there are two factors. One, the phenomenon of diffraction and
scattering causes the radio waves to bend and go over and around any obstacles in
their path (see Fig. 2.2). As the earth's surface is full of large and small obstacles,
the waveform is assisted almost continually to curve round the surface. The extent
of diffraction depends on the radio wave's frequency (see Fig. 2.3). The diffraction
is maximum at the lowest end of the spectrum and it decreases as the frequency is
increased. At centimetric wavelengths (SHF) an upstanding obstacle stops the
wave front, causing a shadow behind it. It is because of this effect that LF
broadcasts give good field strength behind a range of hills but there is no reception
on your car radio when going under a railway bridge.

This bending downward is further assisted (the other factor) by the fact that as
a part of the wave-form comes in contact with the surface it induces currents in it,
thereby losing some of its energy and slowing down. This is called surface
attenuation. This slowing down of the bottom gives the wave forms a forward and
downward tilt encouraging it to follow the earth's curvature (see Fig. 2.4).
Thus, bending due to diffraction and tilting due to attenuation (imperfect
conductivity of the surface) cause the waves to curve with the surface. Waves
continue until they are finally attenuated, that is, become undetectable.

Attenuation, in its turn, depends on three factors:

1) The type of the surface. As mentioned earlier, different surfaces have different
conductivities. For a given transmission power a radio wave will travel a longer
distance over the sea than over dry soil. For example an MF transmitter's range
over the sea is nearly double that over the land.
2) Frequency in use. The higher the frequency, the greater the attenuation (see Fig.
2.5).

3) Polarisation of radio waves. Vertically polarised waves are normally used with
minimum attenuation.
In combating attenuation, we have no control over the surface over which the
propagation is to be made. The primary consideration therefore, is the choice of
frequency. We are now ready to summarise the ground ranges expected from
frequencies in various frequency bands.

VLF. Attenuation is least, maximum bending is due to diffraction. Given
sufficient power, ranges of several thousand miles may be obtained.

LF. Attenuation is less and the signals will bend with the earth's surface;
ranges to a distance of 1500 nm may be expected.

MF. Attenuation is now increasing, signals still bend with the surface and the
ranges are approximately 300 to 500 nm, maximum is 1000 nm over the sea.

HF. Severe attenuation, bending is least. The maximum range obtainable is
around 70 to 100 nm.

VHF and above. The signals do not bend and the radio waves travel in a
straight line, giving line-of-sight ranges.

Disadvantages at low frequencies.

Although low frequencies produce very long ranges there are considerable
drawbacks, which prohibit their inconsiderate employment.

1) Low efficiency aerials. Ideally the length of the transmitter and receiver aerials
should each be equal to the wavelength. An aerial approximately half the size of
the wavelength is also considered to be suitable for satisfactory operation. Any
further reduction in the aerial size would result in a loss of efficiency. The
largest aerials are found in the lowest frequency band -VLF.

2) Static is severe at lower frequencies and additional power must be supplied to
combat its effect. The effect of static decreases as the frequency is increased:
VHF is considered to be practically free from static.

3) Installation and power. The cost of initial installation is high and subsequent
power requirement to maintain the desired range giving satisfactory reception is
very large.

It should be noted that the range of a surface wave varies as the square root of
its power which may be written in the form of the equation:
Range (nm) = 3 ×√Power (watts)
Sky Waves

We have seen how surface waves may be transmitted to varying distances in
VLF to HF bands. In these bands, signals may also be received having first been
reflected from a huge reflecting layer surrounding the earth known as the
ionosphere. These reflected signals are referred to as sky waves and they form the
principal mechanism for long range communication.

The Ionosphere

The ionosphere is an electrically conducting sphere, completely surrounding
the earth. The ultra-violet rays from the sun impinging upon the upper atmosphere
cause electrons to be emitted from gas molecules. These free electrons are
believed to form a reflecting layer (positive ions would be too heavy to influence
electromagnetic waves). Because the absorption of the solar radiation is uneven at
different levels in the upper atmosphere, several distinct and separate layers, rather
than one continuous zone, are formed. They are given code names D, E and F (see

Fig. 2.6). During the period 1901-1930, the E layer was more commonly known as
the Kennelly-Heaviside layer, named after its discoverers. The presence of the F
layer was established simultaneously by E. V. Appleton in England and A. F.
Barnett in the USA and direct measurements were made in 1925, when the name F
layer was coined. At present, these belts may be identified either by the code letter
or the layer names. Average heights of these layers are as follows, and there are
diurnal and seasonal variations.

D layer: 50-100 km, average 75 km
E layer:100-150 km, average 125 km
F layer:150-350km, average 225km.

Friday, 29 August 2014

study material while working time


Convesely, if the blade angle increases, the required torque increases. Then the engine and the propeller will tend to slow down.










What Does "Constant Speed Propeller" Mean?

It means a constant RPM (revolution per minute) system that permits the pilot to select the propeller -- and engine -- speed the pilot wants for any situation, and then automatically maintain that RPM under varying conditions of airspeed and power.

How Is the RPM Controled?

It is done by varying the pitch of the propeller blades. The pitch is the the angle of the blades with relation to the plane of rotation. As the blade angle is reduced, the torque required to spin the propeller is reduced and the airspeed and RPM of the engine will tend to increase for any given power setting.

Thus, we can control the RPM by varying the blade angle or pitch of the propeller.

Does It Mean That the Propeller Operates at the Same Speed All the Time?

No. The system allows the pilot to select the RPM he/she wants. The pilot has a control in the cockpit for this. When the pilot wants maximum power at low airspeed such as for takeoff, the pilot pushes this control full forward. This gives low pitch and maximum RPM with full throttle. This is great for getting off the ground, but it is normally not desirable for cruising at high airspeeds. So the pilot can ease back on the throttle and the propeller control for cruising. This increases the pitch and the speed settles into the desired RPM for cruise conditions. The RPM automatically stays set until the pilot moves the control.

How Is the Pitch of the Blades Changed?

It is changed hydraulically in a single acting system using engine oil from the propeller governor to increase the pitch of the propeller blades.

Oil pressure acting on the piston in the propeller produces a force that is opposed by the natural centrifugal twisting moment of the blades and a spring. This moves the piston back. Motion of the piston is transmitted to the blades through the actuating links and pins, moving the blades toward high pitch.
When the opposing forces are equal, oil flow to the propeller stops and the piston will also stop. The piston will remain in this position holding the pitch of the blades constant until oil flow to or from the propeller is established by the governor. Pitch is decreased by allowing oil to flow out of the propeller to be returned to the engine sump. When the governor initiates this procedure, hydraulic pressure is decreased and the piston moves forward, which moves the blades toward low pitch. The piston will continue to move forward until the opposing forces are again equal.

What Is "Manifold Pressure"?

Manifold Pressure is the pressure of the fuel/air mixture induced into the engine cylinders. Manifold pressure is measured downstream of the throttle valve. When the throttle is closed, air outside the engine (under higher atmospheric pressure) can't flow into the induction system, despite the vacuum on the engine side of the throttle valve.



When the throttle is fully open, the pressure downstream of the throttle valve approaches that of the atmosphere. In other words, the air is forced into the induction system at the maximum pressure the atmosphere is capable of pushing.

Consequently, manifold pressure gives an approximate measure of engine power.

What Is Governor?

The propeller governor is an RPM sensing device which operates by means of the centrifugal force working on flyweights. The governor responds to a change in system RPM by directing engine oil to or releasing engine oil from the propeller to change the blade angle and return the system RPM to the original value. The governor may be set up for a specific RPM by the cockpit propeller control.
The propeller governor uses the same principle of Flyball Governor invented by James Watt in the 18th century! A look at the governor and total system will help to explain how it works.

The governor mounts on and is geared to the engine. This drives governor gear pump and the flyweight. The booster gear pump boosts engine oil pressure to provide quick and positive response by the propeller. The rotational speed of the flyweight varies directly with engine speed and controls the position of the pilot valve. Depending on its position, the pilot valve with direct oil flow to the propeller allow oil to flow back from the propeller, or forward to the propeller.

How Does the Governor Control RPM?

Please refer to the pictures in the "What Is Governor" section as well as the figures in this section for understanding how the governor controls engine RPM.
The flyweights (5) are installed with their lower legs projecting under a bearing on the pilot valve (10). When the pitch of the propeller blades is too low to absorb engine power, the engine RPM increases and it becomes higher than the propeller control setting. This is called overspeed condition. In the overspeed condition, the flyweights are open since the centrifugal force against the flyweights is high. Hence, the upward force by the flyweight becomes greater than the downward force by the speeder spring. As the result, the pilot valve is forced up and oil from the booster pump flows into the propeller.



This increases the pitch of the blades. Engine speed then slows down to maintain the original RPM setting.

On the contrary, in the underspeed condition (the engine RPM is lower than the propeller control setting), the flyweights are closed since the centrifugal force against the flyweights is small. Hence, the upward force by the flyweight becomes less than the downward force by the speeder spring (3). As the result, the pilot valve is forced down and the oil flows from the propeller.

This reduces the pitch of the blades. Engine speed then increases to maintain the former RPM setting.


CMV converted met visibility
Factor to be used for cmv
Ils categories - cat 1, 2, 3
Dh or da for cat 1 - ans is da
Dh for cat 2 and cat 3
Whats is thrust reduction altitude and, accelerated altitude.
Difference between precesion and non precesion approaches.
Vor ndb loc rnav - what type of approaches are these ( ans is non precision) 
Wake turbulence separation while on runway and while flying (approx 80 miles while flying) 
2 aircrafts one heavy and the other light when should they plan their descend. (heavy-early) 
Type of engine in a cessna 152
Difference between horizontally opposed and radial engines.
What happens when we give in the full power.
What is carburettor.
Any problems faced by using carburettor. 
Use of carb heat and indications.
What is compression ratio.
What is top dead centre.
When does ignition occur?
Why is ignition at a point before the piston is at top dead centre. 
Why do we do a mach drop check.
Enroute charts, date on an approach chart is which day, y? Waypoint names, wht it common between them? Deicing nd methods used, anti-icing, rvsm, flat rated and derated, compression ratio in piston engine
Carborator. Cost index fuel injection. Critical engine. Optimum altitude. Table top runway Da 42 engine. Detonation. Fuel used in my aircraft 100ll. What is ll What is rate of decent controller expecting you to do What's satus guys started aft session
Creep on tyre Fuse breaker Wd originate effects Indian climate Ils categories Airbus fly by wire, will Airbus stall Rvsm, contingencies Lots of hr but related to Cass I guess
They asked about qualification school college family sibling, how did u get into flying, why do u wana fly, y would u chose indigo, these r general qs that they'll ask everybody...N then there will be few counter qs