Lesson Notes By Weeks and Term v4 - SHS 2

Aircraft Structures and Control

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Subject: Aviation And Aerospace Engineering

Class: SHS 2

Term: 2nd Term

Week: 5

Grade code: 3.1.3.LI.4

Strand code: 1

Sub-strand code: 3

Content standard code: 3.1.3.CS.2

Indicator code: 3.1.3.LI.4

Theme: Core Concepts in Aerospace Engineering

Subtheme: Aircraft Structures and Control

Lesson Video

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Performance objectives

Lesson summary

Welcome, future engineers and pilots! Today, we explore one of the most fundamental questions in aviation: How does a pilot actually control a massive machine like an aeroplane, weighing hundreds of tonnes, as it flies through the sky? The answer lies in the aircraft's control systems, which act as the "nervous system" connecting the pilot's brain and hands to the aircraft's moving parts. In Ghana, as Kotoka International Airport grows as a major West African hub, understanding the technology inside the aircraft we see every day is crucial. From the smaller PassionAir planes flying to Kumasi to the giant Emirates A380s flying to Dubai, different technologies are at work.

Lesson notes

This lesson focuses on the three primary methods used to translate a pilot's commands into aircraft movement. First, let's remember the primary flight controls: Ailerons (on the wings) control roll. Elevator (on the tail) controls pitch (nose up/down). Rudder (on the tail) controls yaw (nose left/right).

The question is: how does the pilot's yoke (steering wheel) or sidestick move these surfaces? Mechanical Control Systems

This is the oldest and most direct method of controlling an aircraft. Core Concept: A direct, physical connection exists between the pilot's controls and the flight control surfaces. How it Works: Think of the brake system on a simple bicycle. When you squeeze the brake lever, a steel cable is pulled, which in turn pulls the brake pads against the wheel. Mechanical flight controls work the same way. The pilot moves the control yoke or rudder pedals. This movement pulls on a network of steel cables, push-pull rods, pulleys, and bell cranks. This physical network directly moves the ailerons, elevator, or rudder. Analogy: A puppeteer controlling a marionette with strings. The puppeteer's hand movements are directly and physically connected to the puppet's limbs. Key Features: Simplicity: Relatively easy to design, build, and maintain. Reliability: Not dependent on electrical power or hydraulic fluid. The physical connection is robust. Feedback: The pilot can "feel" the aerodynamic forces on the control surfaces through the yoke. This is called control feedback. Limitation (Pilot Effort): On large or fast aircraft, the air pressure on the control surfaces is immense. It would require superhuman strength for a pilot to move them with cables alone. Weight: The long runs of heavy steel cables and rods add significant weight to the aircraft. Example Aircraft in Ghana: Small training aircraft used at flight schools, such as the Cessna 172. Hydraulic Control Systems (Hydro-mechanical)

As aircraft got bigger and faster, a solution was needed for the "pilot effort" problem. Hydraulics provided the muscle. Core Concept: Uses the power of pressurized fluid to move the control surfaces, significantly reducing the pilot's physical effort. How it Works: Think of a hydraulic car jack. A small push on a lever can lift a heavy car. The system multiplies force. The pilot moves the control yoke, which is still connected to cables and rods (like a mechanical system). However, instead of pulling the control surface directly, these cables move a small hydraulic valve. Opening the valve allows high-pressure hydraulic fluid (a special type of oil) to flow into an actuator (a piston in a cylinder). The immense pressure of the fluid pushes the piston, which is connected to and moves the large control surface. Analogy: Power steering in a car. You turn the steering wheel with little effort, and the hydraulic system provides the force to turn the heavy wheels. Key Features: Force Multiplication: Allows pilots to control huge surfaces on large jets with ease. Smoothness: Control inputs are smoother and less jerky. Complexity: More complex than mechanical systems. It requires engine-driven pumps, reservoirs for fluid, filters, and a network of high-pressure pipes. Dependency: Relies on the hydraulic system functioning. A loss of hydraulic pressure can lead to a loss of control, so multiple redundant systems are built in. Example Aircraft in Ghana: Many regional jets and older generation airliners like the Boeing 737, and the Dash 8 aircraft flown by Africa World Airlines (AWA) and PassionAir. Fly-By-Wire (FBW) Control Systems

Evaluation guide