What is a fixed wing aircraft, and how many layouts do the flaps of a fixed wing aircraft have on th

Definition The so-called fixed-wing aircraft refers to the aircraft with fixed parameters such as wing position, sweep angle and so on; Compared with some modern supersonic aircraft, when flying at low speed, in order to get greater lift, the wing stretch is larger (the sweep angle is smaller), and the sweep angle can be changed and increased with the increase of the aircraft's speed in flight, which is no longer a fixed-wing aircraft, typical is ***, it is also called a gyroplane, without a fixed wing; In order to reduce the floor space when parked, the wings of the carrier-based aircraft are folded; However, if the wings cannot be folded or the angle is changed during flight, it is still a fixed-wing aircraft. At present, civil airliners are fixed-wing aircraft.

To put it bluntly, fixed-wing is an aircraft whose wings cannot change direction and cannot rotate and move, except for helicopters.

In addition to taking off by propeller, it includes fighters, bombers, and reconnaissance aircraft.

Other aircraft, including transport aircraft, are basically fixed-wing aircraft.

Aircraft (aircraft, plane, aeroplane, airplane, aeronef, aeroplane, flying machine), the professional term is fixed-wing aircraft (fixed-wing aircraft), which generally refers to an aircraft that is heavier than air, driven by a power plant, the wing is fixed to the fuselage and does not move relative to the fuselage, and the lift force is generated by the force of air on the wing. This definition is to distinguish it from gliders and gyroplanes. Fixed-wing aircraft are by far the most common type of aircraft.

Power** includes piston engines, turboprops, turbofan engines or rocket engines, among others. Fixed-wing aircraft refers to a heavier-than-air aircraft with wings and one or more engines that can fly in the atmosphere by its own power. Strictly speaking, an aircraft is an aircraft with fixed wings.

At the beginning of the 20th century, the Wright brothers of the United States made significant contributions to the history of aircraft development in the world. In 1903, the first manned flight under its own power, the Flyer 1, was built and successfully tested. They were awarded the U.S. Congressional Honor Award in 1909.

In the same year, they founded the "Wright Aircraft Company". Since the invention of the airplane, the airplane has increasingly become an indispensable means of delivery for modern civilization. It profoundly changes and impacts people's lives.

As the name suggests, the wing of the aircraft cannot change its up-down and front-to-back angles.

First of all, the position of the rear part of the wing end is to give the fuselage a greater turning moment, the aileron can be shaken up and down, and the aileron must be constantly used to make large-angle turns during the flight, and the fuselage will also tilt, and after the turn, it should be turned back to the center like a car turning; The flap is at the rear of the wing by the fuselage, and can also be on the front edge of the wing windward, and can only rotate downward, and the purpose is to increase the wing area and increase lift during takeoff; The angle of rotation is generally 20°. The purpose of landing is to increase drag and shorten the running distance, and the angle of rotation is generally 35°. A slight turn of the flaps during flight can reduce the turning radius.

<>1. Fixed-wing aircraft (fixed-wing plane) is referred to as aircraft (English: plane), which refers to a heavier-than-air aviation hail device that produces forward thrust or rushing pull force from the power unit and lift force generated by the fixed wing of the fuselage.

2. It is a type of fixed-wing aircraft, and it is also the most common one, and another type of fixed-wing aircraft is a glider. Aircraft can be divided into jet aircraft and propeller aircraft according to the type of sail motive they use.

Summary. Yes, holders of the Vertical Fixed-Wing Captain Certificate can fly multi-rotor. This is because VTOL fixed-wing aircraft and multi-rotor UAVs have some similarities in flight principles, such as aviation knowledge, flight rules, etc.

However, flying different types of aircraft requires specific training and qualifications, so holders of a vertical fixed-wing captain certificate must obtain additional training to fly multirotors and operate within the limits set by the relevant agencies or regulations.

Yes, holders of the Vertical Fixed-Wing Captain Certificate can fly multi-rotor. This is because VTOL fixed-wing aircraft and multi-rotor UAVs have some similarities in flight principles, such as aviation knowledge, flight rules, etc. However, flying different types of aircraft requires specific training and qualifications, so holders of a vertical fixed-wing captain must obtain additional training to fly multi-rotors and operate within the limits of the relevant grinding or regulations.

Fellow, I really didn't understand, I can be more specific.

Holders of the Vertical Fixed-Wing Captain Certificate can fly multi-rotors, but additional training and operation are required within the specified range.

Today's airplanes are mainly fixed-wing aircraft: the wings are flat on both sides of the fuselage, mainly generating lift, and the wings are relatively fixed.

There is another kind of variable-swept wing aircraft, that is, an aircraft whose wing sweep angle can be changed in flight, which also belongs to fixed-wing aircraft. Modern supersonic aircraft widely use small aspect ratio large swept wings, supersonic drag is less, but at low speed the aerodynamic efficiency is low, and the lift characteristics are not good. Using a large aspect ratio wing with a small sweep angle with good low-speed performance will also deteriorate supersonic performance.

Variable-swept wing aircraft can solve the contradiction between high and low speed performance requirements through the change of wing sweep angle. The aircraft uses a small sweep angle during take-off and landing and low-speed flight, which has the largest wingspan aspect ratio, so it has a higher low-speed cruise efficiency and a larger take-off and landing lift. When flying at supersonic speeds, the aspect ratio and relative thickness of the wing are reduced with a large sweep angle, which is very beneficial for reducing the drag of supersonic flight.

In addition, when supersonic bombers and strike aircraft fly at ultra-low altitude and high speed, in order to reduce the turbulence caused by unstable air currents, they also require a large wing sweep angle and a small aspect ratio. Modern variable-swept wing aircraft are often used in multi-role fighters, fighter-bombers and bombers, such as the Soviet Union's MiG-23, Western Europe's "Tornado" and the United States' F-14 and B-1 are all variable-swept wing aircraft.

Gyroplane: The common *** belongs to the rotary-wing aircraft.

It is like the wing of a civil aviation 3 fork machine, and what cannot be extended is a fixed wing.

Fixed-wing aircraft refers to aircraft with fixed parameters such as wing position and sweep angle; Compared with some modern supersonic aircraft, when flying at low speed, in order to get greater lift, the wing extension is larger (the sweep angle is smaller), and the sweep angle can be changed and increased with the increase of the aircraft's speed in flight, which is no longer a fixed-wing aircraft, typical is ***, and gyroplanes, without fixed wings; In order to reduce the floor space when parked, the wings of the carrier-based aircraft are folded; However, if the wings cannot be folded or the angle is changed during flight, it is still a fixed-wing aircraft.

Fixed-wing aircraft or fixed-wing aircraft, often referred to as airplanes, refer to heavier-than-air aircraft that are heavier than air flying in the atmosphere by the forward thrust or pull force generated by the power unit and lift generated by the fixed wings of the fuselage. Aircraft in today's world, mainly fixed-wing aircraft.

The plane turns through a vertical stabilizer in the air The function of the vertical stabilizer is a bit like the rudder of a ship How to turn has nothing to do with the engine, the engine just gives the plane a pull (propeller) or thrust (turbine), but in the case of a double engine, the turning rate can be adjusted by adjusting the pull (thrust) of the two engines when turning.

When taxiing on the ground, the turning is generally controlled by the foot pedal to control the deflection of the nose landing gear, and some mainframes may have handle control, and control the brakes of the left and right main landing gear at the same time to adjust the turning rate.

In the air, the attitude of the aircraft is mainly controlled by three main control surfaces, the outer trailing edge of the wings on both sides is the aileron, which controls the roll of the aircraft, the trailing edge of the vertical stabilizer plane of the tail is the vertical tail, which controls the deflection of the aircraft, and the trailing edge of the horizontal stabilizer plane is the horizontal tail, which controls the pitch of the aircraft; When turning, coordinate the network to turn the direction of the pressure plate, the rudder (foot pedal), so that the aircraft produces a slope to the direction of the turn (such as the uncoordinated rudder will produce side slip, resulting in a decline in flight performance), is the slope to reach the pre-selected slope of this turn, a few degrees in advance back to the disk, back to the rudder, is the rudder back to the previous level flight position, so that the aircraft is fixed in the attitude of turning. When the heading is about to reach the pre-selected course, a few degrees in advance (this degree is determined by the turning slope, generally one-half of the slope) reverse disc and rudder, change the turning attitude, reach a few degrees before the level flight attitude, return to the rudder, return to the level flight attitude, in addition, when turning the aircraft with a slope, the vertical component of lift will be reduced, when turning to properly bring a rod (pull the steering stick), increase the angle of attack, and improve the lift to maintain the height.

This can be done by the vertical tail flaps and the flaps on the wings on both sides, and the steering purpose is generally achieved by rolling over.