TWM580998U - Unmanned fixed-wing airplane for vertical take-off and landing - Google Patents

Abstract

A vertical take-off and landing unmanned fixed wing machine includes a fuselage; a pair of wings connected to the fuselage; a pair of propellers are disposed on both sides of the front end of the fuselage; a launching tube is disposed on the machine The center of the front end; a pair of vertical tails are disposed on both sides of the rear end of the fuselage, and the body can stand vertically; a propeller is disposed at the center of the rear end of the fuselage; through the pusher of the propeller and the propeller Rotate to allow the aircraft to take off and land vertically. At the same time, it can be automatically taken off to the user's preset position through the setting of the flight control computer installed in the fuselage, and then automatically return to the vertical landing.

Description

Unmanned aeroplane for vertical takeoff and landing

The invention relates to an unmanned aeroplane for vertical take-off and landing, in particular to an unmanned aeroplane with vertical take-off and vertical take-off and landing, which is light and portable and easy to transport.

When the conventional fixed-wing aircraft takes off, there must be a runway to provide a fixed-wing aircraft to take off and land. Therefore, if the length of the runway is insufficient, the fixed-wing aircraft cannot take off and land and become useless.

In order to solve the problem that the fixed-wing aircraft must have a runway, an aircraft with a vertical take-off and landing function (such as a rotorcraft) is developed. However, the vertical take-off and landing aircraft can freely take off and land without the need for a runway, but The payload is small, and usually the flight distance is short, so it is still insufficient in practicality and usability.

Therefore, how to combine the advantages of the fixed wing machine and the rotorcraft at the same time is an urgent problem to be overcome.

It can be seen that there are still many shortcomings in the above-mentioned conventional fixed-wing aircraft or rotorcraft, which is not a good designer, and needs to be improved.

In view of the shortcomings derived from the above-mentioned conventional fixed-wing aircraft or rotorcraft, the inventor of the present invention has improved and innovated, and after years of painstaking research, he finally succeeded in researching and developing the unmanned aeroplane of this vertical take-off and landing.

The purpose of this creation is to provide an unmanned aeroplane that can take off and land vertically.

In order to achieve the above object, the unmanned aeroplane for vertical take-off and landing of the present invention comprises: a fuselage having an accommodation space therein; a pair of wings respectively disposed on two sides of the fuselage; a pair of propellers, The system is disposed on both sides of the front end of the fuselage, and the propeller is driven to rotate by a motor; a launching tube can accommodate and emit an object, and is disposed at the center of the front end of the fuselage; It is disposed on both sides of the rear side of the fuselage, so that the fuselage can stand vertically; a propeller is disposed at the center of the rear end of the fuselage, and can generate a propulsive force.

The vertical take-off and landing unmanned aeroplane disclosed in the present case, wherein the wing system has low resistance and high lift characteristics.

The vertical takeoff and landing unmanned aeroplane disclosed in the present case, wherein the wing system is foldable relative to the fuselage.

The vertical take-off and landing unmanned aeroplane disclosed in the present case, wherein the launching object can be a rocket or a pesticide bomb.

The vertical take-off and landing unmanned aeroplane disclosed in the present invention, wherein a photographic device can be disposed on the body.

The unmanned aeroplane for vertical take-off and landing disclosed in the present invention, wherein the fuselage interior is provided with a flight control computer, an emission control module and a power supply unit.

The vertical take-off and landing unmanned aeroplane disclosed in the present case, wherein the flight control computer system is transparent Receive the message entered by the user by wire or wirelessly.

The vertical take-off and landing unmanned aeroplane disclosed in the present invention, wherein the shooting control module is used to control the launching tube to emit an emission object accommodated in the launching tube.

The vertical take-off and landing unmanned aeroplane disclosed in the present case, wherein the power supply unit provides the required power.

The vertical take-off and landing aircraft disclosed in the present case, wherein the wing and the fuselage are folded to each other, the size is about 50 x 50 x 15 cm.

The vertical take-off and landing unmanned aeroplane of the present invention, wherein the structure in which the wing and the fuselage are folded together may be a pivotal or disassembled assembly structure.

This case has at least the following advantages:

1. The unmanned aeroplane system for vertical take-off and landing in this case can take off and land vertically according to the position set by the user, and complete the second action set by the user (such as launching rocket, pesticide bomb, photography, etc.).

2. The unmanned aeroplane system for vertical take-off and landing of this case is equipped with a FOT firing control module. Therefore, it has the characteristics of being shot and ignored, and the target can be changed during navigation to ensure the target is hit.

The detailed description of the present invention and the accompanying drawings are intended to provide a further understanding of the present invention.

1‧‧‧ body

11‧‧‧ Flight Control Computer

12‧‧‧Shot Control Module

13‧‧‧Power supply unit

2‧‧‧ wing

3‧‧‧propeller

4‧‧‧ launch tube

5‧‧‧Vertical tail

6‧‧‧ propeller

7‧‧‧ Backpack

71‧‧‧Strap

A‧‧‧ vertical takeoff and landing aircraft

The first figure is a three-dimensional schematic diagram of an unmanned aeroplane with vertical takeoff and landing.

The second figure is a schematic diagram of another angle of the unmanned aeroplane with vertical takeoff and landing.

The third figure is a schematic diagram of another angle of the unmanned aeroplane for vertical take-off and landing.

The fourth figure is a schematic diagram of the planar structure of an unmanned aeroplane with vertical takeoff and landing.

The fifth figure is a schematic diagram of the unit structure of an unmanned aeroplane with vertical takeoff and landing.

The sixth figure is a schematic diagram of the implementation of a vertical take-off and landing unmanned aeroplane.

The seventh figure is a schematic diagram of the folding implementation of a vertical take-off and landing unmanned aeroplane.

The eighth figure is a schematic diagram of the implementation of a non-fixed-wing aircraft with vertical take-off and landing.

The above and other objects, features and advantages of the present invention will become more apparent and understood.

Referring to the first to fourth figures, the present invention provides an unmanned aeroplane for vertical take-off and landing, which comprises: a fuselage 1 having an accommodation space therein; a pair of wings 2, Separately disposed on the two sides of the fuselage 1, wherein the wing 2 is designed to have low resistance and high lift characteristics; a pair of propellers 3 are disposed on both sides of the front end of the fuselage 1, wherein the propeller 3 is transmitted through a The motor is driven to rotate (not shown); a launching tube 4 is disposed at the center of the front end of the fuselage 1, and the launching tube 4 is for accommodating an object, wherein the projectile can be a rocket or a pesticide. a pair of vertical tails 5 are disposed on both sides of the rear end of the fuselage 1 so that the fuselage 1 can stand vertically, the vertical tail 5 can be used to control the flight direction and angle; a propeller 6 is set In the center of the rear end of the fuselage 1, and can generate a propulsive force; The airframe 1 is provided with a flight control computer 11, an emission control module 12 and a power supply unit 13 (see FIG. 5); and the flight control computer 11 is received by wire or wirelessly. The information input by the user, and the flight control computer 11 can control the above components according to the message to control the flight direction, flight route and the like; the shooting control module 12 is used to control the launch tube 4 to enable the flight control module 12 to The transmitting object that is placed in the launch tube 4 is emitted; and the power supply unit 13 is used to provide the power required by the aircraft of the present invention.

When in use, the user can input the preset position into the flight control computer, and through the pushing of the propeller 6 and the rotation of the propeller 3, the aircraft can take off vertically, fly to the set position and complete the preset action. For example, launching rockets, pesticide bombs, etc., and then automatically returning to the vertical landing. In addition, a camera device (not shown) may be disposed on the body 1, and the purpose of flight photography may also be achieved.

Please refer to the sixth figure, which is a schematic diagram of the implementation of the vertical take-off and landing aircraft A of the present invention. If the user needs to use a large area or continuously, the user can respectively transfer the preset positions one by one to the vertical take-off and landing of the present invention. In the aircraft A, then it can automatically take off vertically to the set position, and after completing the task, it will automatically return to the take-off position without additional operation by the user, which greatly improves the application range and practicality as well as personnel safety.

Referring to the seventh and eighth figures, the wing 2 of the vertical take-off and landing aircraft A of the present invention can be folded relative to the body 1. After folding, the overall shape is slightly rectangular and can be placed in a backpack 7. The back strap 71 in front of the backpack 7 can provide the user with the piggyback carrying, so that it can be applied to a larger range and field. In this embodiment, the overall size of the vertical take-off and landing aircraft A after folding is about 50 x 50 x 15 cm. The folding manner between the wing 2 and the body 1 may be a pivoting or disassembling combination, but not limited to the above size or folding method.

The detailed description above is a detailed description of one of the possible embodiments of the present invention, but the embodiment is not intended to limit the scope of the patents, and the equivalent implementations or modifications that are not departing from the spirit of the present invention should be included in the present case. In the scope of patents. The scope of protection of this creation should be as described in the scope of the patent application described later.

Claims (7)

An unmanned aeroplane for vertical take-off and landing, comprising: a fuselage having an accommodation space therein; a pair of wings respectively disposed on two sides of the fuselage; a pair of propellers disposed on the body The two sides of the front end of the fuselage, and the propeller is driven to rotate by a motor; a launching tube can accommodate and emit an object of the launching body, and is disposed at the center of the front end of the fuselage; a pair of vertical tail fins are disposed on the machine The two sides of the rear side of the two sides make the fuselage stand vertically; a propeller is placed at the center of the rear end of the fuselage. An unmanned aeroplane for vertical take-off and landing according to claim 1, wherein the wing system is foldable relative to the fuselage. An unmanned aeroplane for vertical take-off and landing according to claim 2, wherein the structure in which the wing and the fuselage are folded together is a pivoting or disassembling assembly structure. An unmanned aeroplane for vertical take-off and landing according to claim 1, wherein the airframe system is provided with a flight control computer, an emission control module and a power supply unit. An unmanned aeroplane for vertical take-off and landing according to claim 4, wherein the flight control computer receives the information input by the user by wire or wirelessly. An unmanned aeroplane for vertical take-off and landing according to claim 4, wherein the emission control module is configured to control the launch tube to emit an emission object accommodated in the launch tube. An unmanned aeroplane for vertical take-off and landing as described in claim 4, The power supply unit provides the required power.