Applications of Pneumatic Systems in Aircraft

PNEUMATIC SYSTEMS

Introduction

When talking about pneumatic system, we need to talk about where the pneumatic system comes from and it comes from a power system, there are three different types of power systems,

• Hydraulic system
• Pneumatic system
• Electrical system

Pneumatic systems in Aircrafts

Pneumatic systems they are also known as vacuum or pressure systems, the power many functions which are important to the aircraft. Power instrument landing gear, flaps, windows, air conditioning, doors and auto pilot devises are some of many operations powered by pneumatic system. Pneumatic and hydraulic systems are similar and use compressed fluids. Fluid property could be liquids as water, oil, or something that flows. And both liquids and gases flow, since they are considered as fluids; however, there is a great deal of difference in the characteristics of the two.

Get Help With Your Essay

If you need assistance with writing your essay, our professional essay writing service is here to help!
Find out more about our Essay Writing Service

Liquids cannot be compressible; a quart of water still occupies about a quart of space regardless of how hard it is compressed. But gases can be compressed, a quart of air can be compressed into a thimbleful of space. Considering this differences gases and liquids are fluids and can be made to transmit power. The type of unit used to provide pressurized air for pneumatic systems is determined by the system’s air pressure requirements.

Components in Pneumatic System

Hydraulic systems are sometimes compared to, pneumatic systems but some similarities can only be true in general terms. Such as

Pneumatic systems do not

• utilize reservoirs
• hand pumps
• accumulators
• regulators
• building normal pressure from engine or electrically driven power pumps

But similarities do exist in some components.

Air Compressors

Simply an air compressor is a Pump that compresses air, its job is raising air pressure to above established pressure for use in pneumatic systems on some aircraft, air compressors have permanently installed and added to recharge air bottles when pressure is used to operate a unit. Several types of compressors that are used for this purpose. Some have three stages of compression, while the others have two, depending on the desired operating pressure.

Relief Valves

Relief valves are used to prevent damage. They act as a pressure limiting units and prevent bursting lines and blowing out seals from excessive pressures.

Control Valves

Control valves are also a necessary part of a typical pneumatic system. It is used to control conditions such aspressure, flow,temperature, andliquidlevel by fully or gradually opening or closing. Control Valve is also called a Final Control Element.

Check Valves

Check valves are used in both hydraulic and pneumatic systems. Check valve is also called a one way valve which allows pressurized air to enter the system, but it prevents backflow of air toward the Compressor when Compressor system is stopped which prevent loss of pressure in the system.

Restrictors

Restrictor is type of control valve used in pneumatic system. Figure below 1llustrates an orifice type restrictor which has a large inlet port and a small outlet port. The rate of the airflow and the speed of operation of the actuating unit will be reduce by the small outlet port.

Variable Restrictor

The variable restrictor is a type of speed regulating unit it contains an adjustable needle valve, therefore has threads around top and the lower end. Depending on the direction turned and the needle valve turns the sharp point either into or out the small opening to decrease or to increase the size of the opening. Since air entering the inlet port must be able to pass through this opening before reaching the outlet port adjustment determines the rate of airflow through the restrictor.

PRESSURE REGULATOR

The pressure regulator is to control the maximum pressure in the system and to off-load the compressor when the system is idle.

Oil and Water Trap regulator

The oil and water trap is designed to remove any water or oil which may be suspended in the air delivered by the compressor.

Air Filters

Air filters purpose is to prevent oil vapor, dirt or moisture from passing into the various services. It is installed vertically with the drain plug at the bottom.

Some advantages are

• Prevent system contamination
• Remove air particulates
• Clean air is essential to good operation

Figure 1. View of Cutaway air filter. Air entering the top of section first flows through the element to remove solid particles. Then flows in a circular motion, where centrifugal force separates water from the air stream, andthen the water falls to the filters sump.

Storage Bottles

Storage bottles act as a reservoir of compressed air which operates all services to pneumatic system. Compressors main use is to build up system pressure when it falls below normal pressure level. The size of the bottles are taken from the volume of actuators and pipelines determines required for the normal and emergency pneumatic services.

Storage bottles are generally made of steel, and may use a wire wound construction for maximum strength. Light ally or fiberglass materials may be other typs of material wich will be used.

Air Pump

Heart of pneumatic system is pressure or vacuum air pump. Which is usually engine driven)

There are two basic types: •Wet air pumps which use engine oil to lubricate pump internally

•Dry air pumps which is more common more common have graphite vanes inside pump casing self-lubricate as pump rotates

High pressure systems

High pressure system is driven by an engine driven compressor feeds air from an unloading valve through the system keeping the pressure. The pressure around this system is 3000 psi but this will vary from manufacturer to another. There will usually also be a ground valve on the aircraft system to enable to pressurize when the main engines are not running. In high pressure systems air is normally stored in a metal bottles at pressures from 1000-3000 psi, depending on the particular aircraft system.

Some high pressure systems are

• Oxygen lines
• Flaps
• Breaks
• Landing gear

Low pressure systems

Low pressure systems are pressurized up to 1000 psi and uses an engine driven vane type pump. They are may be used to drive

• Air cons
• door seals
• de-ice boots
• small low power applications

Medium-Pressure Systems

A medium-pressure pneumatic system usually does not include an air bottle. Instead, it draws air from the compressor section of a turbine engine. Which is generally around 50 to 150 psi This is often called bleed air process and is used to provide pneumatic power for engine starts, engine deicing, wing deicing, and in some cases, it provides hydraulic power to the aircraft systems but only if the hydraulic system is equipped with an air-driven hydraulic pump. Engine bleed air is also used to pressurize the reservoirs of the hydraulic system.

Emergency Backup Systems

Many aircraft use a high pressure pneumatic back up system source to extend the landing gear or actuate the brakes. And if main hydraulic braking system fails. Nitrogen gas is not directly used to actuate the landing gear or brake system units but applies the pressurized nitrogen to move hydraulic fluid to the actuator. This process is called pneudraulics.

Nitrogen Bottles

There are two bottles of nitrogen stored for emergency use, mostly bottles located on each side of nose wheel well. Actuation of an outlet valve released by Nitrogen from the bottles. Once depleted, maintenance personnel must recharge the bottles. Fully serviced pressure will be approximately 3,100 psi at 70 °F/21 °C, which is only enough for one extension of the landing gear.

PNEUMATIC SYSTEM

The illustrator below is a typical full pneumatic system as is used on a twin engine commuter transport aircraft.

Each procedure is shown below in dot points

• Each of the two compressors is a four stage piston type pump, driven from the accessory gearbox of the two turboprop engines.
• Air is taken into the first stage through an air duct.
• It is compressed, then passes to the other three stages.
• From the fourth stage the discharge air is routed through an intercooler and a bleed valve to the unloading valve.
• The bleed valve is kept closed by engine oil pressure and in an event of a loss of an engine lubricating oil, the valve will open and relieve the pump of any load.
• The unloading valve maintains pressure between 2,900 and 3,300 psi in the system.
• When the pressure rises to 3,300 psi a check valve traps it and dumps the output of the pump air overboard.
• The pump is directed back into the system when the system pressure drops to 2,900 psi.
• The shuttle valve which is between the compressor and the main system makes it possible to charge the system from a ground source.
• When the pressure from the external source is higher than the external source of the compressor, when the engine is not running, the shuttle slides over and freezers the compressor.
• Compressed air system have moisture and this will condense and freeze when the pressure of the air is dropped for actuation because of this every bit of water must be removed from the air.
• Then a separator collects the water that is in the air on a baffle and holds it until the system is shut down.
• When the separator’s pressure drops below 450 psi, a drain valve operates and all of the accumulated water is blown overboard.
• Then an electric heater prevents the water collected in the separator from freezing.
• After the air leaves the moisture separator, about 98% of its water removed, it passes through a desiccant, or chemical drier, to remove the last traces of moisture.
• Before the air enters the actual operating system it is filtered through a 10 micron sintered metal filter.
• In the right engine nacelle a back pressure valve is installed.
• This is essentially a pressure relief valve in the supply line that does not open until the pressure from the compressor or ground charging system is above 1700 psi and this make sure that the moisture separator will operate most efficiently.
• The left side where there is no back pressure valve can be connected if it is required to operate the system from an external source of less than 1700 psi.
• There are three air storage bottles in this type of aircraft system,

• A 750 cu. Inch bottle for the main system
• A 180 cu. Inch bottle for normal brake operation
• A 180 cu. Inch bottle for emergency operation of the landing gear and brakes.

• Then come the mutually operated isolation valve which allows a technician to close off the air supply so that the system can be serviced without having to discharge the storage bottle.

• Most of the components in this system operate with pressure of 1000 psi so a pressure reducing valve is installed between the isolation valve and the supply manifold for normal operation of the

  • landing gear
  • passenger door
  • drag brake
  • propeller brake
  • nose wheel steering

• Since this valve reduces the pressure to 1000 psi it also serves as a backup pressure relief valve.

• The emergency system stores compressed air under the full system pressure of 3,300 psi and supplies it for landing gear emergency extension.

EMERGENCY BRAKE SYSTEM

In a failure of the hydraulic system, the pilot of a large aircraft can operate a pneumatic valve on the instrument panel and direct compressed air or nitrogen into the brake system. When the pilot turns the handle, a regulator is adjusted that controls the air pressure to the brakes. When sufficient pressure reaches the brake line, the piston moves up against the force of the control spring and shuts off the inlet valve. The compression of the spring determines the amount of pressure supplied to the brake. When the brake handle is rotated in the direction to release the brakes, the air is exhausted overboard.

Then rather than allowing compressed air to enter the wheel cylinder, which would require the entire brake system to be bled of air, the emergency air may be directed into a transfer tube. The air forces hydraulic fluid from the tube into the brake system.

Emergency operation of the brakes is also achieved in many aircraft by the use of compressed air. When the pilot is sure that there is no hydraulic pressure to the brakes, the pneumatic brake handle, located on the left instrument panel, can be rotated. Clockwise rotation of this handle increases the brake pressure. Nitrogen pressure released by this control handle forces hydraulic fluid in the transfer tube into the main wheel brakes through shuttle valves. When the brake handle is rotated counterclockwise pressure is released and the nitrogen is exhausted overboard.

http://www.engineerstudent.co.uk/uni_directional_flow_control_valve_symbols.html

http://navyaviation.tpub.com/14018/css/14018_285.htm

http://en.wikipedia.org/wiki/Relief_valve

http://mech-engineer.blogspot.com.au/2009/05/drawworks-brake-system-training-course.html

http://www.aliexpress.com/airbrush-compressor-regulator_reviews.html

http://www.airid.com/high-volume-drain-valve.html

http://basicaerospace.blogspot.com.au/2013/01/aircraft-pneumatic-system-for-beginners.html