A/C system Recit Flashcards

1
Q

Hydraulic system

A

it uses a pressurized fluid to transmit power and create force, motion, or control through a network of interconnected components

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2
Q

Pascal’s Law

A

Pressure applied to a liquid spreads equally in all directions.

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3
Q

Users of Hydraulic System in Airbus

A

Flight controls
Landing gear
Brakes
Nose wheel steering
Cargo doors
Thrust reverser
Ram Air Turbine (RAT)

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4
Q

Advantages of using Hydraulic System

A
  • Lightweight
  • Easy to install
  • Easy to Inspect
  • Low Maintenance requirements
  • Incompressible, nagtratravel liquid without loss of time and motion
  • They provide good lubrication of components.
  • Low viscosity
  • They prevent internal corrosion in the system.
  • They have a wide operating-temperature range.
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5
Q

Hydraulic Fluid

A

used primarily to transmit and distribute forces to various units to be actuated

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6
Q

Viscosity

A

a liquids ability to resist flow

as temperature decrease, viscosity increases

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7
Q

Chemical Stability

A

the liquid’s ability to resist oxidation and
deterioration for long periods.

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8
Q

Viscosimeter

A

measure the viscosity of a liquid

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9
Q

Sludge

A

Dirt or thick build-up that forms if the fluid breaks down.

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10
Q

Flash Point

A

the temperature at which a liquid
gives off vapor in sufficient quantity to ignite momentarily or flash when a flame is applied

The lowest temperature where the fluid can catch fire briefly.

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11
Q

Fire Point

A

the temperature at which a
substance gives off vapor in sufficient quantity to ignite and continue to burn when exposed to a spark or flame

The temperature where the fluid keeps burning once it starts.

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11
Q

Mineral-based hydraulic fluid (MIL–H-5606)

A

Red color
Good in cold weather
Flammable
MIL-H-6083 is a version with rust protection

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12
Q

MIL-H-6083

A

is a version with rust protection of mineral based hydraulic fluid

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13
Q

POLYALPHAOLEFIN-BASED
FLUID

A

Fire-resistant
Can self-extinguish
Works in very high temperatures
Good against rust

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14
Q

Phosphate Ester-Based Fluid

A

used in most commercial aircraft
not fireproof
Sensitive to water contamination

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15
Q

GIVE 2 BRANDS OF PHOSPHATE ESTER-BASED HYD. FLUID AND THEIR COLORS

A

Skydrol - Purple
Hyjet - Purple Blue

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15
Q

CHARACTERISTICS OF A PHOSPHATE ESTER BASED HYDRAULIC FLUID

A

Good fire safety
Protects against rust
Works well in heat and cold
Lightweight

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16
Q

HYDRAULIC RESERVOIR

A

is a tank in which supply of hydraulic fluid for
the system is stored.

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17
Q

HYDRAULIC PUMP

A

is responsible in
delivering hydraulic power into
the users of hydraulic system.

Hydraulic power output 3000 psi.

input psi is 40-47

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18
Q

output pressure of hydraulic system

A

3000 psi

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19
Q

input pressure of hydraulic system

A

40-47 psi

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20
Q

Check Valve

A

Fluid can only flow one way

Stops backflow

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20
Q

HYDRAULIC FILTERS

A

is a screening or straining device used to clean the hydraulic fluid, preventing foreign particles and contaminating substances from remaining in the system.

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20
Q

micron element

A

is designed to prevent the passage
of solids greater than 10 microns

21
Q

Shutoff Valve

A

are used to shut off the flow of fluid to a
particular system or component

Stops fluid flow during problems or emergencies

21
Q

PRESSURE RELIEF VALVE

A

Releases extra pressure if it gets too high

also called Safety Valve

can not be used as pressure regulator

22
Q

Pressure Regulator

A

Controls system pressure

Keeps the pump running safely without wasting energy

is to manage the output of
the pump to maintain system operating.

23
Q

SELECTOR VALVE

A

allows the changing of
direction of the flow of pressurized
hydraulic fluid

24
Q

HYDRAULIC ACTUATOR

A

converts hydraulic power to
mechanical action

25
Q

ACCUMULATOR

A

is a steel sphere divided into
two chambers by a synthetic rubber
diaphragm.

The upper chamber contains fluid at
system pressure

the lower chamber is
charged with nitrogen or air.

STORES HYDRAULIC PRESSURE

26
Q

FUNCTIONS OF ACCUMULATOR

A

Absorbs sudden pressure changes (to prevent damage)

Provides extra power when many parts work at the same time

Stores power for emergency use if the pump stops

Maintains pressure to cover small leaks and prevent the system from turning on and off repeatedly

27
Q

Hydraulic System Safety Procedures

A

Wear coveralls

Use nitrile or polymer gloves
Use safety goggles

Fluids like Skydrol can dry or irritate your skin

Prevent leaks and handle with care

28
Q

Pneumatic system

A

utilized the use of compressed air for the operation and use of the air conditioning and pressurization system,
anti- icing, engine starting, hydraulic reservoir and potable water
tank pressurization.

29
Q

Location of the controls of the hydraulic system

30
Q

Uses of pneumatic system

A

AIR CONDITIONING AND PRESSURIZATION

ANTI- ICING

HYDRAULIC RESERVOIR PRESSURIZATION AND
POTABLE W ATER PRESSURIZATION

31
Q

Air Bleed

A

Compressed air taken from the engine or APU (auxilliary power unit)

31
Q

compressed air

A

pneumatics, bleed air, or air bleed

32
Q

Fokker F-27 Turboprop Aircraft

A

first aircraft to use full pneumatics on
* Brakes
* Opening and closing doors
* Driving hydraulic pumps, alternators, starters, water
injection pumps.
* Operating emergency devices

33
Q

Disadvantages of pneumatic system

A

*Loss of precision due to the high
compressibility of gas compared to liquid.
*Bleed Air does not respond immediately to
pressure differentials.

Short:
Not precise

Slow reaction compared to hydraulics

Compressible (hard to control accurately)

34
Q

Sources of pneumatics in wide bodied

A

Engines (8th and 13th compressor stage)

Auxiliary Power Unit (APU)

Pneumatic Cart / Ground Power Unit

35
Q

Auxiliary Power Unit

A

acts as a standby source of bleed air in case during flight

36
Q

OPERATING PRESSURE AND
TEMPERATURE OF PNEUMATICS

A

200-250 °C and 40 psi

37
Q

PRECOOLER

A

air-to-air heat exchanger located in the
pylons that cools and regulates the bleed air before it enters the distribution manifold

37
Q

Pressure Regulating Valve / Bleed Valve

A

Controls air pressure and temperature of bleed air prior to entering the system

Shuts off air during emergencies

38
Q

CROSSBLEED VALVE

A

Allows the connection of the
two sides of the Pneumatic system.

When both engines cannot supply bleed air during operation, this valve allows the APU to supply bleed air to the users of Pneumatic System.

38
Q

Check Valve

A

prevents the reverse
flow of bleed air

39
Q

BLEED AIR SUPPLY DUCT

A

Acts as supply line where the bleed air
travels to the distribution manifold

40
Q

HEPA Filter

A

HIGH EFFICIENCY PARTICULATE
ARRESTANCE FILTER

41
Q

bleed monitoring computer

A

control all the valves that
comprises the Pneumatic System and monitors the system as a
whole.

shuts off the valves when encountering emergencies.

42
Q

ECAM (Electronic Centralized Aircraft Monitor)

A

Monitors aircraft systems (like pneumatic and hydraulic)

43
Q

CFDIU (Centralized Fault Display Interface Unit)

A

Displays system faults or problems for the pilot

44
Q

LEAK DETECTOR CAMERA

A

quick leak detections in a safe environment

The camera uses 124 microphones to form a very precise acoustic image in
the desired direction.

45
Q

location of the controls of pneumatics

A

The controls of the pneumatic system are located in the cockpit.

The pilots control and monitor the system using buttons, switches, and screens.

It is part of the ECAM or monitoring system inside the cockpit.

46
Q

X bleed Valve

A

Same as cross-bleed valve, allows air sharing between engines or from APU

47
Q

OVER PRESSURE VALVE

A

Protects the pneumatic system by releasing extra pressure if it’s too high (same function as pressure relief valve in hydraulics)

56
Q

Users of pneumatic system

A

air conditioning

pressurization system

anti- icing

engine starting

hydraulic reservoir

potable water tank pressurization

57
Q

Sources of pneumatic in wide bodies

A

APU and bleed air

58
Q

Where to locate controls of pneumatic

A

Overhead control panel

59
Q

Important Properties of a hydraulic fluid that is use in aviation

A

viscosity

chemical stability

fire point

flash point