AIRCRAFTS HYDRAULIC SYSTEM JANHARLAL.E.M. S-7 ME. NO.65.

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AIRCRAFTS HYDRAULIC SYSTEM JANHARLAL.E.M. S-7 ME. NO.65

Transcript of AIRCRAFTS HYDRAULIC SYSTEM JANHARLAL.E.M. S-7 ME. NO.65.

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AIRCRAFTS HYDRAULIC SYSTEM

JANHARLAL.E.M.S-7 ME.

NO.65

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B737 Hydraulic System

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INTRODUCTION Hydraulics is based on the fact that

liquids are incompressible Hydraulic system is a system where

liquid under pressure is used to transmit energy

In it a hydraulic pump converts mechanical power to hydraulic power

An actuating cylinder converts hydraulic power to mechanical power.

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A SIMPLE HYDRAULIC SYSTEM

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DEVICES USING HYDRAULIC SYSTEMS IN AIRCRAFTS

Gun turrets Auto pilot Shock absorption systems Dive, landing, speed and flap brakes Bomb bay doors Doors and hatchways Landing gears, wing flaps, etc…

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PRINCIPLES OF OPERATION Governed by Pascal’s law The oil is in contact with

both sides of the piston head but at different pressures.  High pressure oil may be pumped into either side of the piston head.

The selector valve determines to which side of the actuating cylinder the high pressure oil (red colored side) is sent.

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PARTS OF THE POWER SYSTEM

RESERVOIR ACCUMULATOR FILTER POWER PUMP SYSTEM RELIEF VALVE PRESSURE REGULATOR

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POWER SYSTEM

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RESERVOIR

FUNCTIONS Holds reserve supply oil to account for

normal leakage, emergency supply of oil, volume changes, thermal contraction of oil,

Provides pressure head on the pump, a place to remove air or foam from liquid, air space for expansion of the oil due to temperature changes

etc

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RESERVOIR

CONSTRUCTION Material: 5052 aluminium Size: takes into account all oil

volumes in operational requirements, thermal expansion, leakage, etc.

Shape: domed cylindrical shape, due to ease of construction & mounting

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ACCUMULATORS

PRINCIPLE Gas valve lets in

compressed gas at ½ system pressure

Diaphragm pops up & oil is sent through system

When system pressure>accumulator pressure, diaphragm deploys

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ACCUMULATORS

USES Absorbs the shocks due to rapid pressure

variations in a hydraulic system Helps maintain a constant pressure within

the hydraulic system Helps the hydraulic pump under peak

pressure loads It is an emergency source of power Spherical shape is preferred for

accumulators

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POWER PUMPS

FUNCTION Is to change mechanical horsepower to

hydraulic horsepower TYPES Gear pumps: move fluid based upon the

number of gear teeth and the volume spacing between gear teeth.

Piston pumps: move fluid by pushing it through the motion of the pistons within the pump

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POWER PUMPS

PRINCIPLES OF GEAR PUMPS

The liquid from the reservoir is pushed between the gear teeth.

The oil is moved around to the other side by the action of the drive gear itself and sent through the pressure line.

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POWER PUMPS

PRINCIPLES OF RECIPROCATING PISTON PUMP As the cylinder block rotates, space between the

block and the pistons increase, letting in more oil. As the block rotates from bottom dead center, the

reverse occurs and the pistons push oil out through the outlet

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SYSTEM RELIEF VALVE

PRINCIPLE The adjustment screw is set for a

certain pressure value P2. When the pressure increases, the

poppet will move up, forcing the excess liquid in

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Douglass Pressure Regulator

High pressure oil from the power pump opens valve C and also act on piston A

Piston A pushes Ball B off seat D, the oil goes through passage D into the center chamber back to the reservoir.

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HAND PUMPS

Single Action Single Impulse

Used for testing on ground and for Emergency

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Selector Valves Position (1) is the position of the selector valve,

for example, upon the extension of the landing gear or the lowering of flaps.

Position (2) is the position of the selector valve upon retraction of the landing gear or the raising of the flaps

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ACTUATION CYLINDER

The function is to take the pressure & hydraulic fluid flow & change them into linear or rotary motion.

Single piston double rod is an equal displacement cylinder used in aileron system or automatic guidance system

Double piston-double rod actuating cylinder used in bomb bay doors

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ADVANTAGES It is lighter in weight than alternate existing

systems. It is dead beat, that is, there is an absence of

sloppiness in its response to demands placed on the system.

It is reliable; either it works or doesn't. It can be easily maintained. It is not a shock hazard; it is not much of a fire

hazard. It can develop practically unlimited force or

torque.

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CONCLUSION

Hydraulic systems determine flight worthiness, usability and reliability.