Landing Gear Flashcards

1
Q

L/G UNDERCARRIAGES
And oleo (oil and air) strut is a pneumatic hydraulic shock absorber

Sustain long periods in a static load condition (parked)
Absorb impact of landing and related drag and side load (landing load condition)
Control the recoil of the landing

A

Strut dikme demek
Oleo (ail&air)

Bogie: iki teker arası yatay eleman. Dönüşleri uzun alıyoruz ki bogie’lere çok fazla yük binmesin.

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2
Q

The oil supplies damping
Nitrogen supplies spring function

A

Nitrojenin olma nedeni korozyon oksidasyon olmaması.

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3
Q

Torque links

Landing gear torque links are used to prevent rotation of the landing gear piston in the oleo strut

A
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4
Q

Safety pins*
Aircraft downlock pins are used to lock the landing gear in place

In some aircraft, there is protection device to avoid the landing gear being inadvertently retracted on the ground. It consist of: A latch located in the landing gear lever.

The pilot may be prevented from retracting the landing gear whilst the aircraft is on the ground by: THE ELECTRICAL CONTROL SYSTEM BEING ROUTED THROUGH THE WEIGHT ON WHEELS SWITCH

A

Latch: kilit.
Ağırlık swichleri sayesinde

Pilot landing gearları yerdeyken geri toplamasını engellemesi için uçağın ağırlık swichleri engel olur.

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5
Q

Emergency gear extension can be performed

With compressed nitrogen
By mechanical manual means
By freefall
By hydraulic system

A
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6
Q

Overcentre

A

Iniş takımlarının kilitlenmesi için kullanılan prensip

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7
Q

Tubeless Tyres:
Only nitrogen inside
No internal friction
Lower risk of bursting
Less weight than tube tyre

Ply rating- index of tyre strength

A
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8
Q

Tyre treads - provide indication of wear, grip, and means of displacing water

A

Yağmurlu havalarda sert iniş - positive landing
Çok sert - hard landing

Aquaplaning - hydroplaning

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9
Q

Thermal plug - if the wheel becomes excessibely hot the fusible material melts, releasing the air pressure and tyre deflate - wheel rims

The reason for fitting thermal plugs to aeroplane wheels is that they prevent tyre burst after excessive brake application.

A

Isınan havayı dışarı deşarj ediyor. Fazla basıncı bu şekilde tahliye eder.

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10
Q

Tyre creep - tendency for the tyre to slip (rotate) about wheel

(Circumferential movement of the tyre in relation to the wheel flange)

A
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11
Q

Tyre wear
- it is very important that inflation pressures are kept at the correct level

Under inflation leads to wear at the SHOULDERS
Over inflation leads to wear at the CROWN
Tyre treads may be repaired several times however damage to sidewalls and plies is not acceptable.

A

Çok şişkin olduğunda göbekten eriyor, az basınçta kenarları eriyor.

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12
Q

Shimmy Damper

shimmy - oscillation of the nose wheel from side to side on the ground (has potential to cause damage)

Nose wheel shimmy may be described as a possibly damaging vibration of the nose wheel when moving on the ground

Shimmy occurs on the nose wheel landing gear during taxiing when the wheels tend to describe a sinusodial motion on the ground

This effect is overcome by means of an accumulator associated with the steering wheel cylinder

A

Ön tekerin sağ sol titremesi, Vto’nun altında lövyeyi kaldırıp biraz basıncı düşürebiliriz.

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13
Q

Hydroplaning
Occurs when tyre loses contact with surface and slides on a thin film of water

If depth of water is greater than 3 mm possibility of hydroplaning is high
Hydroplaning speed (kt) = 9 √(tyrepressure psi)

During hydroplaning, the friction coefficient between tyre and rwy surface is approximately 0

1 bar = 14.5 psi

A
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14
Q

Operational Considerations

Ground maneuvring - imposes greates stress on wheel assembly, so taxi slowly. Use minimal breaking and largest turn radius possible

Wheel fires: can occur if brakes are very hot and oil or grease is present.

Use dry powder to extinguish
Only appr wheel from front or rear. Not the side in case sidewall blows out.

A
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15
Q

Types of wheel brakes

Mechanical drum brakes - very old ac and cars
Hydraulic expander brakes - old ac
Pneumatic bag brakes - old ac
Single disc - light ac
Multi disk - airliners

A

Multiple disc brakes are manufactured from steel or carbon fiber

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16
Q

Brake operating systems

The function of an accumulator in a hydraulic brake system is to supply a limited amount of brake energy in the event of a failure of the hydraulic system normally supplying the brakes.

A
17
Q

Anti skid systems are designed to minimise aquaplaning and the potential tyre damage which can occur when a wheel is locked or rotating at a s peed which does not correspond to the speed of the aircraft. Anti skid removes the possibility of reverted rubber skids caused by locked wheels

THE WORKING PRINCIPLE OF THE ANTI SKID SYSTEM IS REDUCTION OF THE BRAKE PRESSURE AT THE SLOWER TURNING WHEELS

A

Hız düştükçe fren sertliği otomatik azaltılarak centerline takip edilmesini koolaylaştırır. Bir teker dönerken diğeri durursa yoldan çıkma ihtimali var.

18
Q

AUTO BRAKE SYSTEM reduce pilot workload during landing, by automatically applying smooth, even braking pressure to maintain a programmed deceleration value. They also reduce workload in a RTO scenario, helping to bring the ac to a halt as rapidly as possible.

The ABS autobrake system is being disconnected after landing by pilot action

A

TAT: Total air temperature (ram air temp)
SAT: Static air temparature (outside, ambient air temperature)

19
Q

How landing gear be extended if there is a complete hydraulic system failure

A

Mechanically

20
Q

Shuttle valves will automatically

A

Switch hydraucilally to more suitable

21
Q

Landing gear torque links

A

Rotation u önleyecke

22
Q

Low pressure switch of a hydraulic circuit sets off an alarm if:

A

Pump output pressure is insufficient.

23
Q

Hydraulic fluid özellikleri

A

Sondaki highlar yok ;)

24
Q

In hydraulic system, a shuttle valve:

A

Allows two possible sources of pressure to operate one unit.

25
Q

Landing gear wheel is hydroplaning: the friction factor is equal to:

A

O

26
Q

On large aeroplanes equipped with power brakes, the main* source of power is derived from :

A

The aeroplane’s hydraulic system

27
Q

The damping element in a landing gear shock absorber used on large aircraft

A

Oil

Spring deseydik Nitrogen

28
Q

A pressure regulator is used in a hydraulic system

A

constant delivery of pump

29
Q

The viscosity of a hydraulic fluid should be:

A

The lowest to minimize power consumption and resistance to flow

30
Q

Assuming an accumulator is precharged with air to 1000 psi and the hydraulic system is pressured to 1500 psi, the accumulator gauge will read:

A

1500 psi

31
Q

Emergency extension of landing system may comprise:

A

Nitrojen - free fall - aux hydraulic sys
245

32
Q

In a commercial transport aeroplane the landing gear normal operating system is usually

A

Hydralicully driven

33
Q

VLE & VLO

A

VLE - landing gear extend maximum speed

VLO - landing gear maximum operating speed (Pegasus’un izin verdiği max iniş takımı indirme hızı)