Lecture notes Flashcards

1
Q

Widely used material for aircraft construction

A

Alominium alloy, duralumin

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2
Q

What type of wing does a cessna have

A

High wing with strut

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3
Q

Aluminium alloys have

A
  • High thermal and electrical conducitivity
  • Good corrosion resistance
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4
Q

Titanium

A

Lightweight, high strength, corrosion and tmp resistant. But very expensive

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5
Q

Two types of wing support

A

Braced
Cantilever

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6
Q

Which aircraft has braced support wing?

A

Cessna

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7
Q

Cantilever is

A

Self-supporting wing

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8
Q

Wings structure is made of

A

Ribs and spars

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9
Q

Wing torque box

A

Carries all the aircraft loads on the fueslage, in the center between the wings

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10
Q

Flutter

A

Self-exciting vibration under interaciton of aerodynamic force.

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11
Q

How can flutter be avoided

A

By a proper mass and balance of the CONTROL SURFACE by moving CG onto or ahead of the hinge line

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12
Q

MZFW

A

Maximum Zero fuel weight. The maximum aircraft weight with fuel allowed

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13
Q

Types of fuselage structures

A

Framework, Monocoque, Semi-Monocoque, reinforced steel

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14
Q

Framework (structure)

A

Small airplanes, the framework takes all the loads

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15
Q

Monocoque

A

External skin takes the load, made of framers (formers) to give its shape. Is heavy.

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16
Q

Semi-monocoque

A

Skin takes majority of load by framers, longerons and stringers reinforce the skin and prevent deformation

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17
Q

Reinforced steel

A

Comes from semi-monococuue, additional metal placed around apertures to provide more xsterngth.

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18
Q

Honeycomb structure

A

Two layers of metal in between which a honeycomb shaped. Increase strength

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19
Q

Flight windows are made of

A

Laminated glass or acrylic

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20
Q

Active hyraulic system

A

System pressuizerd by a pressure pump (engine driven or air driven)

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21
Q

Passive hydralulic system

A

Not pressurized by a pressure pump (hand or foot operated pumps used)

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22
Q

If an hydraulic fuel is leaking internally,

A

Temparature of the fluid will rise

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23
Q

Types of wheel connections

A

Cantilever, Fork, half fork, dual wheels

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24
Q

Advantages of oleo leg/shock strut

A
  • Sustain long periods in static load condition (parked)
  • Absorb impact of landing
  • Control the recoil of the landing
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25
Shock absorbers can be: 3
Oleo pneumatic Oil compression Spring suspension (C172)
26
Torque link use
Prevent inner and outer cylinder from rotating on each other
27
Brakes convert ____ energy into ____ energy
Kinetic, heat
28
Types of brakes
Drum, single disc, multiple disc
29
Single disc brake
Disc is driven by the wheel and has two stationary brake pads on each side. Two hyd. pistons squeeze the disc when brakes are applied
30
Multiple disc brake
Same as single disc, but multiple discs. Used on large aircrafts
31
Tyre main componenst
Tread, belt, sidewall, bead
32
The tyre tread provides us indication of
wear and grip
33
Tyre wear, under-inflation leads to wear at the
shoulders
34
Over-inflation leads to wear in
crown
35
Hydroplaning
Where tyre loses contact with surface and slides on water
36
Tyre creep
Tendency for the tire to slip about wheel. An example of no creep
37
The primary flight controls are controlled by
direct mechanical linkage
38
Icing can be prevented / eliminiating using 3
Pneumatic pressure, Electrical heat Fluid (alcohol spray)
39
Fuel tanks types may be
-Flexible(bag) -Rigid (aluminion aloy or plastic) -Intergal (spars, ribs) used on large aircraft
40
Fuel tanks must:
- Have sufficient space to allow contents to expand when heated - Baffles placed around so that fuel moves around the tank at manouvers
41
Venting the fuel tanks helping
Adjust the pressure inside the tanks to the outside pressure
42
Two ways of feeding the engine with fuel
Gravity-fed system Fuel pumps
43
Coulombs
Electric charge 1A flow per second is 1C passing a point a second
44
Electricity flows with the flow of electrons from ____ to ____
Negative to positive
45
When a battery is almost fully discharged, there is a tendency for the voltage to
decrease
46
For a rotating armature, to create DC we need a
comutator instead of slip rings
47
Inverter is
a unit to conver DC to AC
48
"Hot bus" or "direct bus" is a definition for a bus that is
directly connected to the battery
49
Shock cooling
50
An increase in RPM will _____ the AoA of the propellor
Incraese
51
An increase in TAS will _____ the AoA of the propller
Decrease
52
Supercharger and magneto to recap
53
Supercharger
Engine driven air-pump which increases manifold pressure and forces fuel/air mixture into cylinders. The higher the manfiolrd pressure, the more dense the fuel/air and more power the engine will produce
54
Brake horsepower
Actual amount of power delivered to the propeller shaft
55
3 types of pressure gauges mechanisms
Aneroid (low pressure) Bellows (Intermediate) Bourdon tube (high)
56
Turbocharger
Same as supercharger but used air from the exhaust
57
True altitude
Actual height of an object ABOVE MEAN SEA LEVEL (not HEIGHT!!!)
58
Denity altitude
Pressure altitude corrected for non-standart temp.
59
TAS formula
1.75% CAS per 1000 of altitude
60
ANDS (compass errors)
Accelerate North, Decelrate South
61
An acceleration will show an apparent turn to the
north
62
A deceleration will how an apparent turn to the south