The introduction of aircraft parts and the introduction of each aircraft model, the first is the foc

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 wing of an aircraft is an important part of the aircraft, and the design and control of its geometry parameters have a crucial impact on the performance, stability and maneuverability of the aircraft. Here are a few common wing geometry parameters. 1.

Wingspan: Refers to the distance between the two ends of an airplane's wings, a parameter that affects the lateral stability of the aircraft. Rent.

2.Wingspan ratio: This is the ratio of wingspan to wing chord length. The larger the wingspan ratio, the higher the lift-to-drag ratio of the aircraft, and the corresponding improvement in take-off, landing and gliding performance.

3.Airfoil: Includes airfoil cross-section and airfoil curvature. The airfoil section shape affects the lift and drag of the aircraft, while the airfoil curvature affects the lateral stability of the aircraft.

4.Chord length: This is the distance between the leading and trailing edges of the wing. The longer the chord length, the larger the wing area, and the higher the lift-to-drag ratio of the aircraft.

5.Sweep angle: that is, the angle between the trailing edge of the wing and the body of the aircraft. The larger the sweep angle, the better the aircraft's high-speed cruise performance, but low-speed performance suffers.

6.Wingspan sweep angle: Refers to the angle between the leading edge of the wing and the fuselage. This parameter has a significant impact on the stability and control performance of the aircraft.

7.Wing area: The area sandwiched between the lower and upper surfaces of the wing, which affects the lift and drag of the aircraft.

In conclusion, the design and control of wing geometry parameters is an important step in aircraft design, and multiple factors need to be considered to achieve the optimal design effect.

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

The main function of the wing is to provide lift for the aircraft to support the aircraft in the air, and also play a certain role in stabilization and maneuvering. Ailerons and flaps are generally installed on the wings. Manipulating the ailerons allows the aircraft to roll; Lowering the flaps increases the lift coefficient of the wing.

In addition, engines, landing gear, and fuel tanks can be installed on the wings. Wings come in a variety of shapes and in different numbers. In the early days when aviation technology was not developed, in order to provide greater lift, aircraft were mainly biplanes or even multiplanes, but modern aircraft are generally monoplanes.

The main function of the fuselage is to load crews, passengers, goods, and various equipment; Other parts of the aircraft such as the tail, wings and engines can also be connected into a single unit. But the flying wing is the fuselage that is hidden inside the wing.

Tail tails include horizontal tails (flat tail) and vertical tails (vertical tails). The horizontal tail consists of a fixed water level stabilizer and a movable elevator (some models of civil and military aircraft have movable control surfaces throughout the flat tail, and there is no special elevator). The vertical tail consists of a fixed vertical stabilizer and movable rudders.

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

Landing gear. Landing gear, also known as landing gear, is used to support an aircraft and enable it to take off, land, and park on the ground and other horizontal surfaces. The landing gear of land aircraft is generally composed of shock absorbing pillars and wheels, in addition to landing gear with pontoon devices and skid landing gear for snow take-off and landing. It is used to support aircraft during take-off and landing taxi, ground taxi, and parking.

Power plant. The power plant is mainly used to generate the pull or thrust force that moves the aircraft forward. Secondly, it can also provide electricity for the electrical equipment on the aircraft, and provide gas source for gas equipment such as air conditioning equipment.

The power plant of modern aircraft mainly includes turbine engine and piston engine, and there are four widely used power plants: aviation piston engine and propeller thruster; turbojet engines; turboprop engines; Turbofan engine. With the development of aviation technology, rocket engines, ramjet engines, and atomic aero engines are also likely to 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.

Friend, you are very professional in this question, what are the parts of the aircraft you are referring to?

The parts of the aircraft are calculated in millions, and the engine alone does not know that there are a lot, I can only tell you some key parts, you remember:

Nose, fuselage, wings, aviation instruments, engines, engine starters, doors, lighting systems, aviation cables, take-off and landing devices, aviation seats, turbine discs, blades, pumps, valves, bearings, bolts, nuts, rivets and other standard parts, aviation rubber parts, aviation glass, fuel tanks.

Titanium alloy, carbon fiber composite, hydraulic system.

The above things are currently more popular things, of course, more parts needless to say, China can only do screws, nuts, cabin doors These technical content is not very high, and the high-tech things are in Boeing, Airbus.

By the way, there are several regions in China that are currently better: Xi'an, Shenyang, Changchun, Guiyang, Anshun, Nanchang, Harbin, Shanghai, Hanzhong, Tianjin, Hunan, Chengdu (Anshun, Zhuzhou, Hanzhong).These are all aircraft parts, and the whole machine is mainly produced in the place.

You can take a look at their industrial base**.

There are also two large groups, the first and second airlines, and there are a lot of things that can be seen in them.

Chengfei, Shen Fei, Shangfei, and Xifei are all the main forces, you can enter their group** to see, I know so much, if you still need it, you can send me a message, happy to answer.

There are too many, it is better to buy a magazine, which is very detailed.

The main components of an aircraft, the organism, landing gear, power plant, flight control system, on-board equipment, and other systems. Combat aircraft also have airborne ** systems.

The airframe includes wings, fuselage, and tail.

The function of the wing is to generate lift when moving in the atmosphere, and it is also equipped with ailerons and spoilers; Aircraft without a tail are equipped with longitudinal control devices (lifting ailerons) on the wings, in addition, there are lifting devices on the wings.

The fuselage is used to house personnel, load equipment, cargo, **, power plant and fuel, etc. The wings and tail are fixed to the fuselage, and the landing gear struts of some aircraft are also fixed to the fuselage.

The tail is divided into a horizontal tail and a vertical tail. The horizontal tail is generally composed of a horizontal stabilizer and an elevator, and the vertical tail is composed of a vertical stabilizer and a rudder. Some aircraft make the horizontal tail into a whole, which can be manipulated and deflection, which is called a full-motion flat tail.

Some aircraft do not have a horizontal tail and are equipped with horizontal winglets in front of the wing, known as front wings or canards. The horizontal tail ensures the pitch stability, maneuverability and balance of the aircraft. The vertical tail ensures the directional stability and maneuverability of the aircraft, and together with the wings, ailerons or spoilers or differential flat tails, the lateral stability and maneuverability of the aircraft are guaranteed.

Landing gear, power plant, airframe, flight control system, on-board equipment, Other systems.

Airplanes are composed of "flying" and "airplane".