/Secondary Systems
   /Brakes & Wheels

Aircraft BrakesWheel brake

Aircraft Brake Design

Wheel brakes are normally used to slow the aircraft down during landing roll on the runway and to aid in directional control during ground handling operations as taxiing, steering and parking.

In small GA aircraft the brakes are connected to the main landing gear only and are usually operated independently from each other, meaning a left and right foot pedal/ brake.

The brake systems are operated by hydraulic pressure and the rudder pedals have the brakes installed on top and are toe operated. Some aircraft use heel brakes or even with separate levers in the cockpit operated by hand (e.g. Pipistrel, DynAero MCR and Tecnam).

With larger aircraft the weight increases but the force pilots can apply will usually be about the same for every human being. It is therefore important that the pilot gets help in the form of brake boosters or power assisted brakes to handle the heavier aircraft.

Wheel brakes

Drum Brakes

The wheel brakes are usually made of the disc type, but on some exotic aircraft the drum type with two brake shoes inside is still being used. You will remember them from old ancient (sometimes called classic) cars too.

Drum type

With this model the two brake shoes are operated by either pneumatic (air) or hydraulic (oil) pressure or maybe even manually with a cable (very rare and usually these were used on the parking brakes). You will not see these on modern aircraft anymore. Inside there are a couple of springs attached to the shoes to make sure that the brake contacts the drum evenly as friction will try to move them slightly. The springs also make sure that the shoes retracts when brake pressure is released.

Disc brakes

Very popular as they are lightweight and the disc sits between the braking pads clamping them when brake pressure is applied. For heavier aircraft multiple brake calipers and or multiple discs can be used to increase braking power capacity.

The brake disc is made from steel and bolted onto the wheel and rotates with it. The clamping part, caliper, contains two brake pads and is self centering. When brakes are applied the oil pressure moves a piston cylinder arrangement inside the caliper and the pads will clamp the disc. Resulting in an even pressure on both sides.

Disc Brakes

Brake system

Most light aircraft have two independent brake systems on the upper part of the rudder pedal. This part is hinged and connected to a master cylinder. High pressure tubing is used to connect the master cylinder to the brake cylinder in the caliper. Special hydraulic fluid (DOT4, AeroShell Fluid 41) is used to transmit the brake pressure. Careful: this fluid will eat away paint so keep it well clear from other surfaces.

Do make sure, that at the start of the takeoff run you place your feet low enough as not to ride the brakes as this would result in a sluggish takeoff roll and very hot, even burnt brake pads.

As the aircraft has two separate brake systems the pilot can use differential braking to help steer the aircraft, some aircraft (Pelican PL, Cessna, Piper) have their nose wheel steering connected to the brake system where the first 10° left or right the nose wheel moves and with further rudder movement the main gear will help steer the aircraft, this is very helpful during taxi and parking.

Parking brake

Some aircraft have a sort of ratchet type system where they keep the brake pressure in the system, holding the aircraft in its place. Others use a hydraulic valve and after pressing the toe brakes (or manual) they close the parking valve, thereby locking the hydraulic pressure. Check the POH to see which type of system is installed in yours.

Power Assist

The simplest system is the boosted brake. In this systems main hydraulic pressure is used progressively through a valve to help the pilot applying the brakes.

With power assisted brakes, the brake system is fed by the main hydraulic system with a much higher pressure than the pilot can apply. Brake pressure regulates main hydraulic pressure to the wheel and caliper.

These power assisted brake systems usually have a backup in case the main hydraulic pressure fails so the aircraft can still be stopped by using the brakes and not run off the runway at the end.

Written by EAI.

Enjoyed our Website? 

If you enjoyed and found value in our site, consider becoming a member. With your help this website can keep growing as a source of information for all aviation enthusiasts!

Become our Patron