Ask for a detailed explanation of the principle of each component of the aircraft

Big brother. Do you know how many years of hard work it takes to research, design, and manufacture a component of an aircraft?

Knowing the principle of a component in detail is a lifelong experience. You even say "parts".

If all that knowledge were printed, it would be a national library.

That being said, I will give you a general description below. Hopefully, you'll be able to read it all. Thank you.

Most aircraft consist of five main parts: wings, fuselage, tail, landing gear, and power plant.

Wing: The main function is to provide lift for the aircraft to support the aircraft to fly in the air; It also plays a certain role in stabilizing and manipulating.

Engines, landing gear, and fuel tanks are mounted on the wings, among other things. (Power).

Ailerons and flaps are generally installed on the wings. (It can control the aircraft to turn and reverse, etc.).

Fuselage: The main function is to load passengers, passengers, cargo and various equipment; Other parts of the aircraft such as the tail, wings and engines can also be connected into a single unit.

Tail: The main function is to control the pitch and deflection of the aircraft, as well as to ensure that the aircraft can fly smoothly.

It includes a horizontal tail (flat tail) and a vertical tail (vertical tail).

The horizontal tail consists of a fixed water level stabilizer and a movable elevator.

The vertical tail consists of a fixed vertical stabilizer and movable rudders.

Landing gear: Also known as landing gear, it is used to support the aircraft and enable it to take off, land and park on the ground and other horizontal surfaces.

It is used to support aircraft during take-off and landing runs, ground taxiing, and parking.

Powerplant: It is mainly used to generate pull or thrust to move the aircraft forward. Secondly, it also provides power for the electrical equipment on board.

The power plant of modern aircraft mainly includes turbine engines and piston engines.

There are four types of power units that are widely used:

aviation piston engine plus propeller thruster;

turbojet engines;

turboprop engines;

Turbofan engine.

With the development of aviation technology, rocket engines and atomic energy aircraft engines may also be gradually adopted.

In addition to the engine, the power unit also includes a series of systems to ensure the normal operation of the engine, such as fuel ** system.

In addition to the above five main parts, the aircraft is also equipped with various instruments, communication equipment, pilotage equipment, safety equipment and other equipment.

Hope it helps.

There are a lot of aspects involved in the content of your question, which is not easy to find, so I recommend a good book to you, and you don't have to ask for anything to see the structural problems.

The book is called "Fundamentals of Aircraft Construction", the author Song Jingbo, published by Aviation Industry Press, ** and Mao is very rich in content, and there is a very detailed introduction to each part of the aircraft, which is also the best book I have ever bought about aircraft construction knowledge.

The main components of conventional aircraft are the fuselage, wings, tail, landing gear, power system, flight control system, avionics system and airborne equipment.

1.The wing is the main component that generates lift. Ailerons for lateral maneuvering and flaps for increased lift are also mounted on the wings.

2.The powertrain includes the engine and some ancillary systems such as fuel, lubrication, heat dissipation, intake and exhaust, etc., which provide the thrust (or pull) force that enables the aircraft to overcome the drag experienced while flying.

3.The tail of an aircraft usually includes a horizontal tail and a vertical tail, and its main function is to ensure the balance of the aircraft and control the aircraft.

4.The landing gear is used for take-off, landing, and ground parking of aircraft.

5.The main function of the fuselage is to load equipment, crew and cargo.

6.The control system is used to transmit control instructions and control the flight attitude of the aircraft.

7.Airborne equipment includes flight instruments, communications, navigation, environmental control, life support, energy supply and other equipment, as well as some airborne equipment related to aircraft use, such as fighter aircraft and fire control system, passenger aircraft cabin life service facilities, etc.

The most basic is ; Hydrodynamics.

When the wing is moving at high speed, the pressure difference between the gas flowing above the wing and the gas below the wing is greater than the weight of the airframe, and the aircraft will rise; Otherwise, it will decline.

The engine is the power that brings the aircraft forward to create a pressure difference.

Other safety measures are designed with Tianhou in mind.

Ride is the design of each company.

Wings? Or turbines? Or the landing gear? Or is it the part of the wing that is removed?

In the case of the wing, it is not only the principle of the reaction of the air flow to the object, but also the principle of pressure and the flow velocity, and if you have used a hair dryer, you will understand it.

The landing gear is hydraulic pressure, and hydraulic shock absorbers as well as lever principle, etc.

The principle of the reaction of air currents on an object.